A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf

Modern Power Plants training book in english khalid ayaz soomro

CENTRAL POWER GENERATION CO.
LTD GENCO-II
A BOOK ON
BASIC
CONCEPT OF
MODERN
POWER
PLANTS
BY
KHALID AYAZ SOOMRO
INSTRUCTOR OPERATION CLASSES AND
(INTERN SHIP ENGINEERS)
GENCO’S TRAINING CENTER CPGCL TPS,
GUDDU
Acknowledgement
All the praise and thanks to the
most Beneficent and Gracious the
greatest
Lord “Almighty Allah” who
blessed me with potential and
ability to contribute
a material to existing
knowledge.
I pay all my tributes to the Holy
Prophet Hazrat Mohammad
(S.A.W.W)
Who enlightened our conscious,
who is torch of guidance for all
humanity, who is the city of
knowledge, All and every
respect is for Hazrat Mohammad
(S.A.W.W) who enables us to
recognize our creator
(STAY BLESSED MY
AMI ,ABUAND MY
LOVELY FAMILY )
*EMERGENCY CAN
BE OCCURRED
AT ANY TIME AND
NEVER CAN BE
OCCURED
CONTENTS:
Fire
Safety
Health
Fist Aid
Introduction to Power plants
Basic concept of modern power plants
Conventional Power Plants
Non-conventional Power Plants
Combined cycle power plant
Combined Cycle Principles of Operation
Ccpp Advantages
Ccpp Abstract
Gas turbine for power Generation Introduction and Parts
Gas Turbine Performance
Gas Turbine Theory
Static Frequency Converter(SFC)
load-commutated- inverter (LCI)
Aerodynamic Torque Converter for Gas Turbines
Definition of torque converter
Advantages of gas turbine
Gas turbine cooling and sealing air
Gt blades material
Gas turbine starting procedure
Q and A /Efficiency
Compressor surge
Bryton Cycle
Gas turbine compressor washing
Turbine inlet air cooling system (types)
Mee Industries(Mee Fogg)
Gas Turbine Protections
Gas Turbine Fire Protection
What is normal air/fuel ratio?
Kinds of Gas Turbine Loading
HRSG (Heat Recovery Steam Generator)
HRSG circulations (types)
Supplementary firing (HRSG)
Parts of HRSG
Protections of HRSG
Types of HRSG
Typical Application of HRSG
HRSG star up pre checks
HRSG Startup Program
Boiler /Steam Generator
Types of boiler
Boiler Zones
Parts of Boiler
Types of Boiler System
Boiler system controls
Purging of Boiler
Boiler Fittings and Abbreviations
Boiler Excess Air Control
Energy
Types of Energy
Boiler Furnace
Types of Furnace s
Boiler Combustion system
Fuels and Combustion
Fossil Fuels
Fuel Gas
Fuel Oil(heavy Oil)
Fuel Coal
Gross calorific values of different fuels
Boiler system major components
Boiler Drum
Drum Internals
Stresses in Tubes and Drums
Super Heaters Design and Performance
Steam temperature control methods in supper heater
Attemperation / De super Heater
Economizer
Air Pre Heater
Stacks / Chimney
Types of draft.
Boiler Water Circulation Types
Safety Valves
Boiler Internal inspection
Ratio of heat absorbed by different compenents placed in the foue
gases path
De Aerator and Types
Economizer
Air Pre Heater
Boiler make-up water treatment plant and storage
Auxiliary steam distribution
Dew Point
Hydrostatic Test of Boiler
Boiler safety Interlocks
Creating Your Boiler Log
Pumps and its Types
Condensate System
Feed water Heaters
Condensate Polishing Systems
Desalination Plants
Applications
History
Experimental Techniques Other desalination techniques
Steam Traps
Essentials of steam power plant equipment
Steam Condensers and types
Vacuum loss conditions
Common condenser problems
Condenser terminal difference
Condenser circulation ratio
Corrosion
Protection from corrosion
Condensate Cycle
Feed Water Cycle
Main Steam Cycle
Boiler Water Carryover
Effects of Carryover
Causes of Carryover
INTRODUCTION of NPSH
NPSH-PROBLEMS
PUMP CAVITATION
Steam Turbine
Steam Turbine History
Types of Steam Turbine
Speed Regulation
Steam Turbine Classifications
The Curtis Stage
Types of blades and stage
Basic Parts of Steam Turbine
Parts and functions of steam turbine
Principal of operation and Design
Impulse turbines
Reaction turbines
Q and A
Thermodynamic cycles and Types
Methods to increase power
Methods to improve efficiency
Thermal power station
Introductory overview
Efficiency
Cost of electricity
Working principal of steam turbine
The four processes in the Rankine cycle
Principle of operation of steam turbine
Advantages of steam turbine over steam engine
Steam Turbine Governing
Heating of Steam Turbine
Steam Turbine Performance
Steam Turbine Testing
Steam Turbine Specifications
Classification of Steam Turbine
Turbine operation
Shutting the turbine down
Major components of a turbine
Governing or regulating valves
Control Monitoring & Operation Operator Responsibilities
Prime movers governing systems
The turbine supervisory system TSE
Introduction to Protection Measurement Types
Shaft Vibration (relative)
Shaft Vibration (absolute)
Bearing Vibration (also relates to prediction monitoring)
Position Measurement
Eccentricity
Phase (also relates to prediction monitoring)
Differential Expansion
Valve Position
Speed Measurement (acceleration, direction, and more)
Axial Position Protection
Process Variables
Steam turbines with modern control platforms
Noise Criterion
Proper Eccentricity probe location
Advanced Turbine Monitoring System by ITS
Turbine stress evaluator TSE
How steam turbine protection system works
Protection of Steam Turbine
POWER
BEARINGS
Turning Gear
Turbo Generator
History
Design
Generator heat dissipation
Generator high voltage system
Excitation of Synchronous Machine
Synchronous Alternator Construction
Excitation System
Types of Excitation System
Q and A
What are the types of generator
Basic working principal of generator
Generator Cooling System
Advantages of A.C Generator
Generator protections system
Generator protections Zones
Governor Droop system
Droop speed control
Q and A
Diesel Generator
Use Of Diesel Generator In Power Plants
Diesel Power Plant
Synchronization
Power Transformer
Buchholz relay
Differential relay
Transformer Protection
D.C Supply
Direct current (DC)
History
Various definitions
Applications Domestic and Commercial
Direct current as source of operating power
Types of batteries
Equipment used in 220V DC supply system
Use of battery if power station
Purpose of DC system
Cooling Towers
Types of cooling Towers
Temperature measurement in cooling tower
Auxiliaries of cooling tower
Traveling screens
Pumps
Vacuum gauges
Switch Yard
Bus Bar
Disconnects
Circuit breaker
Current transformer
Voltage transformer
Earthing switch
Surge arrestor
Overhead ground wire
Preventive maintenance
Electrical Substation Components and working
Relays
Capacitor Banks
Q and A
GIS GRID Stations
Advantages of GIS
Synchronous Condenser
Capacitor Banks
black start Definition
PTW
Fore Types of PTW
TR ( trouble Reports)
Demineralization ( DM ) Water Treatment Plants
Balance of plant (BOP)
Heating ventilation and air conditioning HVAC
Predictive and Preventive Maintenance
Thermo vision survey for switch yard
Principles of thermal imaging
Thermal Imaging Cameras
Buhut Buhut Shukeriya(Thanks)
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
Health ,Safety and Fire
in
ENGINEERING
(HSE)
FIRE
Fire is the rapid oxidation of a material in the exothermic chemical process of
combustion, releasing heat, light, and various reaction products i.e. toxic gases and
smoke.
PRINCIPLE OF FIRE
Fires start when a flammable or a combustible material, in combination with a sufficient
quantity of an oxidizer such as oxygen gas, is exposed to a source of heat or ambient
temperature above the flash point for the fuel/oxidizer mix, and is able to sustain a rate
of rapid oxidation that produces a chain reaction. This is commonly called the fire
tetrahedron (three-dimensional case).
Fire cannot exist without all of these elements in place and in the right
proportions
1. Oxygen
2. Fuel
3. Heat
When fire take place, below mentioned three objects can be observed easily.
1. Hot Gases (emission)
2. Light
3. Heat
The emission gases have different properties regarding fuel. The visibility of
flame light depends on the particles which have not been burned completely. Hence,
they become visible.
The different gases contain in atmosphere are listed below.
S/No. Name of Gas Symbol % in air
1 Nitrogen N2 78%
2 Oxygen O2 21%
3 Carbon Dioxide CO2 1%
The flash point of different fuels is listed below.
S/No. Name of Gas Flash Point Auto ignition
temperature
1 Gasoline (Petrol) -43 O
C 280 O
C
2 Furnace Oil (RFO) >60 O
C 407 O
C
3 Natural Gas >93.3 O
C 580 O
C
4 Kerosene Oil >37 to 65 O
C 229 O
C
Flash Point
The flash point indicates how easy a chemical may ignite and burn
Auto Ignition Temperature
The Auto-Ignition Temperature - or the minimum temperature required to ignite a
gas or vapor in air without a spark or flame
FUEL
Fuels are any materials that store potential energy in forms that can be practicably
released and used for work or as heat energy.
OR
Those materials that are storing energy in the form of chemical energy that could be
released through combustion.
Types of Fuels
1. Solid -- Wood, Coal, Lignite, Peat etc.
2. Liquid -- Petroleum, Diesel, Fuel Oils, Alcohols etc.
3. Gaseous – Natural Gas, Coal Gas, Hydrogen etc.
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
Types of Fire
S/No. Fire Class Symbol Properties
1 A
Fires that involve flammable solids such
as wood, cloth, rubber, paper, and some
types of plastics
2 B
Fires that involve flammable liquids or
liquefiable solids such as petrol/gasoline,
oil, paint, some waxes & plastics, but not
cooking fats or oils
3 C
Class C fires are fires involving energized
electrical equipment such as motors,
transformers, and appliances
4 D
Fires that involve combustible metals,
such as sodium, magnesium, and
potassium
5 E
Fires that involve flammable gases, such
as natural gas, hydrogen, propane, butane
6 F or K
Fires involving cooking fats & oils. The
high temp. of oils when on fire far exceeds
that of other flammable liquids making
normal extinguishing agents ineffective.
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
Types of Fire and extinguishing
Fuel Source
Class
of Fire
Type of Extinguisher (Extinguishing
Agent)
Ordinary combustibles
(e.g. trash, wood, paper, cloth)
A Water; chemical foam
Flammable liquids
(e.g. oils, grease, tar, gasoline,
paints, thinners)
B
Carbon dioxide (CO2); dry chemical;
film forming foam
Electricity
(e.g. live electrical equipment)
C CO2; dry chemical
Combustible metals
(e.g. magnesium, titanium)
D
Dry powder (suitable for the specific
combustible metal involved)
Combustible gases
(e.g. Natural Gas, Butane)
E A.B.C powder
Combustible Cooking
(e.g. cooking oils; animal fats,
vegetable fats)
F or K
Wet chemical (Potassium acetate
based)
Fire Class Extinguisher Type
A Soda Acid
A Water Type
BCDE Carbon Dioxide
AB Foam Type
ABCD Chemical Powder, Dry Type
ABCE B.C.F Halon
BE Carbon Tetrachloride
Portable and semi portable fire extinguishers.
HOW TO OPERATE FIRE EXTINGUISHNER
Check either extinguisher is fully charged or not
Ensure you remain a safe distance from the fire and remove the safety pin
Where to aim the fire extinguisher hose:
Fires spreading horizontally: Aim the hose at the base of the fire, moving the jet
across the area of the fire
Fire spreading vertically: Aim the hose at the base of the fire, slowly moving the
jet upwards following the direction of the fire
Squeeze the lever slowly to begin discharging the extinguisher, as the fire starts to
diminish carefully move closer to it.
Ensure all the fire has been extinguished; try to focus on any hot spots that may re-
ignite.
Non-portable Fire Extinguishing Systems
Mulsi Fire System
Used to extinguishing the fire occurred at electrical transformer
The MulsiFire system applies water in the form of a conical spray consisting of droplets
of water travelling at high velocity. These droplets bombard oil surface to form a mixture
of oil & water. This mixture significantly cools fire reducing the rate of liquid vaporization,
While water droplets are passing through flame zone, some of the water is formed into
steam that dilutes the air feeding the fire and creates a smothering effect to extinguish
the fire.
Sprinkler System
Used to extinguishing the fire occurred in cable trenches
A fire sprinkler system is an active fire protection measure, consisting of water supply
system, providing adequate pressure & flow rate to a water distribution piping system,
onto which fire sprinklers are connected
Auto Carbon Dioxide
Used to extinguishing the fire occurred on Turbine & Generator.
The non-portable fire extinguishing systems are often
used at large power plants.
WHENEVER FIRE OCCURRED
When you find fire, inform the concern. Restrict the fire by using extinguishing. Activate
the fire alarm. Leave your self and exit
Enter low into fire zone. Remove endanger person Take control
Fundamentals for extinguishing fire
The below mentioned are basic fundamental rules to extinguishing fire
1. Starvation
2. Smothering
3. Cooling
Starvation
Removing fuel from fire triangle is called elimination of fire starvation.
Smothering
Removing oxygen from fire triange is called smothering
Cooling
To decrease the temperature of fuel from ignition point is called cooling
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
PRECAUTIONARY MEASURES
1. To store carefully hazardous fuels i.e. petrol, oil, thinner etc.
2. To stop leakage in oil lube, hydrogen, natural gas lines etc.
3. To observe the increase in bearing temperature of I.D and F.D fans.
4. Always observe the oil leakage where steam and oil lines in vicinity.
5. Cotton rags should be kept in safe place.
6. Whenever oil is used in plant or workshop the excessive quantity should be
returned back to store.
7. Where smoking is not allowed, make sure that the rule is followed.
8. Always make close watch over electric supply cables and wires.
DIFFERENT SAFETY SIGNS
THE MANAGEMENT OF HEALTH AND
SAFETY AT WORK REGULATIONS
Employers must:
Assess risks to the health and safety of their employees and non-employees arising in,
or from, the workshop, and review them when there is significant change. Records of
significant findings of the assessment must be kept where there are five or more
employees plan, organize, control, monitor and review the preventative and protective
measures taken as a result of the assessment
provide health surveillance where necessary,
for example to help control health risks from metalworking fluids appoint any
competent person needed to help them comply with legal obligations, for example,
when having lifting equipment thoroughly examined set out
what should be done in case of serious and imminent danger in the workshop, such as
the spillage of a large amount of degreasing solvent tell employees about the risks and
precautions involved in their work train employees to work safely.
SAFETY & HEALTH GOALS
The following goals have been established for XYZ Manufacturing Company:
(1) Provide workers with a safe work environment.
(2) Conduct routine/regular workplace inspections.
(3) Provide Personal Protective Equipment.
(4) Develop and implement safe work procedures and rules.
(5) Provide on-going safety training
(6) Enforce safety rules and appropriate discipline.
(7) Provide on-going property conservation practices.
NEW EMPLOYEE ORIENTATION
The following topics will be covered in the Safety Orientation Session:
1. Company History
2. Safety Program/Policy & Work rules
3. Responsibilities
4.Safety Education/Training
5. Safety Audit/Inspections
6. Accident Reporting/Investigation Requirements
7. First Aid & Blood borne Pathogens
8. Personal Protective Equipment
9. Tool & Equipment Use
10. Material Handling
11. Lockout-Tag out
12. Machine Guarding
13. MVR Requirements
14. Hazard Communication
15. Emergency Action
16. Return-to-work & Light Duty Assignments
All new hires will be provided an opportunity to ask any question that pertains to their
job duties and employment at XYZ Manufacturing Company
SAFETY & TRAINING
All in-house Safety & Training sessions will be coordinated by (Name of Safety
Director). Foremen and Assistant Foremen are required to be trained in Accident
Investigation Procedures by the Safety Director.
Operators of forklift trucks are to be trained in-house in accordance with federal/state
requirements. Operators must attend classroom instruction as well as ―behind the wheel
training‖. All employees who work with, or are exposed to, hazardous chemicals are to
be trained in Hazard Communication, in accordance with federal and state regulations.
All employees who don respirators are to be trained in accordance with federal and
state regulations. Those individuals who don respirators are required to have annual
physicals.
Machine operators and maintenance personnel are to be trained in Lockout/Tagout
procedures. Individual locks/keys will be assigned to those individuals participating in
the LOTO program. All employees who don Personal Protective Equipment (PPE) will
be trained in the proper use of such equipment.
First-aid training and Bloodborne Pathogen (BBP) training will be conducted by (Name
of Hospital) and the local chapter of the American Red Cross. Machine/Equipment
operators are to be trained in-house. Emphasis is to be placed on point of operation
guarding. No employee is allowed to operate a machine unless it is properly guarded.
Employees who operate company vehicles are required to participate in an in-house
Defensive Driving Program. Foremen and Assistant Foremen are to meet with the
Safety Director on a quarterly basis to discuss training needs and goals.
SAFETY RULES
All safety rules must be obeyed. Failure to do so will result in strict disciplinary action.
1. All injuries must be reported as soon as possible.
2. No horseplay, alcohol, or drugs allowed on premises.
3. No alcohol usage allowed during lunch break.
4. PPE must be worn as prescribed by management.
5. All tools/equipment must be maintained in good condition.
6. Only appropriate tools shall be used for specific jobs.
7. All guards must be kept in place.
8. No spliced electrical cords/wiring allowed.
9. Only authorized personnel can operate forklift vehicles.
10. Smoking allowed only in lunchroom.
11. Seat belt use required of all drivers/passengers.
SAFETY COMMITTEE
General functions of the Safety Committee can include:
1. Identifying workplace hazards
2.Enforcement of Safety Rules
3. Measuring safety performance
4. Reducing frequency/severity of injuries
5. Creating safety policies
6. Developing and monitoring safety programs
Specific tasks of the Safety Committee can
include:
1. Conducting self-inspections of the workplace
2. Review employee reports of hazards
3. Assist in safety training
4. Creating safety incentive programs
5. Publish/distribute safety newsletter
6. Inspect PPE
7. Post safety posters/slogans on bulletin board
8. Identify Light Duty Jobs
SAFETY:
Safety is the state of being ―safe‖. The condition of being protected against physical,
social, financial, political or other types damages, harm accidents or any other event
which would be considered non-desirable.
Safety can also be defined to be the control of recognized hazards to achieve an
acceptable level of risk. It includes protection of people of possession.
Regulation of Safety Code
It power plant and other industrial workers should use safety codes and follow safety
precautions during work hrs, so that no harm or fatal accident does not take place
DUTIES OF WORKERS
All employees should follow safety rules and always try best to avoid redundant
situation regarding his own and other co-workers.
SAFETY CODE
The safety code contains all information and guideline to restrain from accidents during
job and further if any accident take place then how the aftereffect can be minimized.
Thus, safety code is used to minimize the risk of accident for example: safety tags etc.
SAFETY FUNDAMENTALS
There are two major rules of safety
Good House Keeping
Good Operation
Good housekeeping
Your work location should be kept clean and orderly. Keep machines and other objects
(merchandise, boxes, shopping carts, etc.) out of the center of aisles. Clean up spills,
drips, and leaks immediately to avoid slips and falls. Place trash in the proper
receptacles. Stock shelves carefully so merchandise will not fall over upon contact.
GOOD OPERATION
Good operation means to take necessary measures to safe operation of all
appliances at industry i.e. If you have to work on breaker then it should be isolated,
check its isolation and connect a earth lead. The worker should take serious efforts on
the following.
Missing Warning Sign.
Without warning sign any work on equipment can be very dangerous and severe
damage to life and equipment can take place.
Improper Guarding
During work all safety gears should be wear i.e. gloves, safety shoes, safety goggles
etc.
Defective Material
Before starting work proper tools and safety gears should be used to avoid any
accident. It should be ensured that tools are made in accordance with international laws
and they have not been broken nor have bad workmanship quality.
Causes of accidents
Hazards
Everything which came under hazards is dangerous. i.e. oil leakage, cotton rags, and
bad sanitation.
Insufficient lighting
At work place insufficient lighting is can be a part during accident. Thus, sufficient
lighting at work place should be ensured.
Air Ventilation
At work place harmful gases should not be gathered i.e. acid vapors and dust. Thus,
proper ventilation of air should be ensured.
Loose Cloths
Loose cloths should not be wearing at work place.
SAFETY GEARS
Safety gears are used as prime substance to ensure safety to worker. Thus, before
working on electrical system this should be checked and ensure according to rules and
regulation of department.
Kinds of safety gears
Safety Helmet
It protect worker from head and eye injury, further it protects from heat stroke and dust.
Thus, this should be wear during work hrs.
Safety equipment
Ear Muffs
This protect human ear from excessive noise a work place which can damage hearing
efficiency. Normal noise level is 85~90db. Thus if the noise exceed from above the ear
muffs should be used.
Safety shoes.
At industrial area the safety shoes are used to restrain hazards at wet, oils places or
any place where foot injury is one of most prime cause. These shoes can be used at
chemical plant, However they are called long rubber shoes. They also insulate human
body from electrical shock.
Protective Cloth
Use appropriate protective cloth during decanting of furnace oil, acid tankers and
batteries.
Respirator mask
This should be wear, where industrial exhaust i.e. stacks or where any other dangerous
gases contacting human body. If respirators are not used that this will bring deceases
like i.e. chest infection and allergies during respiration.
Safety glasses
The wearing of safety glasses by all shop employees and work on sand blasting etc.
Strict adherence to this policy can significantly reduce the risk of eye injuries.
Safety gloves.
Through this apparatus worker can be safe during work on acid, handing furnace oil,
steam and hot valves or electrical contacts.
Safety belts.
This safes the worker from fall down from height. Thus during work on electrical pole or
any place alike that, safety belt must be used.
Safety shoes
Welder protective shield.
During welder a vital sparking light may cause an injury to eye. Thus, to restrain such
type of injury protection shield must be wear before welding.
Safety programs
The below are prime objects to conduct safety programs.
1. To point out unsafe practice, so that employees and appliances are prevented
from accident.
2. To empower the administrative to follow ensure the regulation of safety code.
3. To abide the SOP for safety code.
4. To prepare a comprehensive accident reports this contains causes of accident
and prevention, so that other may follow to restrain such accidents.
5. Work plan may be made in accordance with safety rules.
6. To conduct safety seminars in-between other power plants, so that awareness to
new technology may be discussed and this will bring knowledge for safe
operations.
Safety is of the utmost importance while operating the main engine. Failure to
observe safety precautions can result in damage to the main engine, personnel injuries,
or even death. Even though many safety precautions seem to be common sense, many
times personnel fail to consider the results of their actions.
Never place any part of the body near rotating machinery. While it is highly unlikely
anyone will ever attempt to grab the main shaft while it is rotating at 200 rpm, there are
other things to be considered. While the main engine jacking gear is engaged, the shaft
is rotating at a very slow rate. Despite this slow rotation, watch standers still should not
be permitted to do any type of work to the main shaft, such as painting or cleaning the
main shaft.
Do not wear jewelry, neckties, or loose fitting clothing while operating equipment. This
clothing can become entangled in the machinery and cause injury or death.
Oil leaks shall be corrected at their source. Spills of any kind shall be wiped up
immediately and the wiping rags disposed of immediately or stored in fire safe
containers. Failure to observe safety with any petroleum product can result in a major
Class B fire.
Promptly reinstall shaft guards, coupling guards, deck plates, handrails, flange shields
and other protective devices removed as interferences immediately after completion of
maintenance on machinery, piping, valves or other system components.
An open main engine presents special safety precautions. While the main engine is
open, an E-5 or above is required to stand guard. A security area is established around
the main engine using ropes and signs. No tools are permitted within the security area
without first being inventoried by the guard. Before personnel are permitted to enter the
security area, they are required to remove all jewelry, securely fasten eyeglasses and
tools to their body using lanyards, and all clothing fasteners must be covered with tape.
As an added safety precaution, ensure all warfare and rank devices are removed before
entering the security area. This precaution prevents inadvertent introduction of anything
that could cause damage to the turbines.
ACCIDENTS AND ILL HEALTH
There are many thousands of accidents and In any particular Plant risks which cases
of ill health reported every year in are relevant should be assessed. Those small
engineering workshops. Almost two- likely to be of most concern include:
thirds of all such accidents reported to HSE V movement of people, goods and arise
from the movement of people, goods vehicles around the Plant, and vehicles into,
around and out of particularly manual handling workshops. Of these `movement'
accidents
- About half involve lifting and moving metalworking fluids, degreasing solvents,
goods, and
- About half involve slips, trips and falls and hitting stationary or moving plant and
equipment
- 'Non-movement' accidents usually arise
and varied sector is available from a from the use of machinery; these account
number of sources, including published for between 10 and 15% of all accidents.
- Electrical accidents are not uncommon and
union publications, although it is difficult frequently have the potential for more
to see the whole picture. The interpret-serious injuries than those recorded.
- The most common occupational diseases are
in dealing with the sector. white finger, and back, hand, arm,
shoulder and neck problems.
.- In any particular workshop risks which
cases of ill health reported every year in are relevant should be assessed. Those
small engineering workshops. Almost two- likely to be of most concern include:
- Movement of people, goods and
arise from the movement of people, goods vehicles around the Plant,
and vehicles into, around and out of particularly manual handling
- Machinery safeguarding
- Hazardous substances, particularly metalworking fluids, degreasing solvents,
goods, and and dust or fume from welding, brazing, soldering,coating and painting
noise, and vibration.
WHAT FIRST AID IS NEEDED IN
WORKPLACES?
First aid is the immediate and basic care given to an injured or sick person before a
doctor, other health professional or emergency services take over their treatment.
It focuses on preserving life and minimizing serious injury by maintaining breathing and
circulation, stemming blood, immobilizing broken bones etc.
First aid requirements at work fall into three categories:
- suitably stocked first aid kits and facilities
- where needed, an appropriate number of suitably trained first aiders
- information for employees about first aid arrangements.
This guide includes some suggestions to help you organise your first aid kits, facilities,
first aiders and information to employees.
Some workplaces have greater risks of injury and illness because of the sort of work
they do. These risks are an important factor in deciding first aid requirements, because
different first aid facilities may be needed for different
activities. Employers are required to provide first aid that takes into account the
individual circumstances of their workplace. Circumstances that can affect your first aid
needs include things like hazards common in your industry or workplace, the number of
employees you have, and how far away you are from medical help.
One way to identify the first aid needs of your business is to complete a Workplace First
Aid Needs Assessment. The section below can help you do that.
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
DEFINITIONS OF FRIST AID
1.1 First-aid in the workplace includes the provision of first-aid facilities, services
and personnel required for the initial treatment of persons suffering from injury
or illness at a workplace. It is the immediate treatment or care given to a victim of an
accident or sudden illness before qualified health personnel attend to provide treatment.
The aims of first aid are to:
• Preserve life;
• Prevent illness or injury from becoming worse;
• Reduce pain;
• Promote recovery; and
• Care of unconscious.
1.2 First-aid facilities includes
• first-aid box;
• first-aid room; and
• first-aid equipment, e.g. oxygen tanks and stretchers.
1.3 First-aid requirement means the requirements for first aid facilities, services
and personnel at a workplace;
1.4 First-aid services means any procedure or method associated with the provision of
first-aid at the workplace;
1.5 First-aider means a person who has successfully completed a first-aid course
and has been awarded with a certificate of proficiency in first-aid by an
institution listed in Appendix 1.
1.6 Risk means the likelihood that a hazard will cause harm.
1.7 Universal Precautions means a set of precautions designed to prevent
transmission of blood-borne pathogens when providing first aid or health care.
An Employer
shall, from time to time, recruit or select suitable persons to go for
first-aid training. The employer should consider persons with the following
qualities to be trained in first-aid:
• physically fit
• free from blood borne infectious diseases, e.g. Hepatitis B, HIV/AIDS
• free to leave their work immediately to respond to an emergency
Recommended Contents of a First-Aid Box
1. Triangular bandages 130cm x 90cm x 90cm
2. Sterile eye pads
3. Non-sterile 4x4‖ gauze pads
4. Sterile 4x4‖ gauze pads
5. Sterile 10x10‖ gauze pads
6. Elastic bandage
7. 4 Roller bandages 7.5 cm
8. 4 Roller bandages 3 cm.
9. 4 Roller bandages 2.5 cm
10. Cold pack compress gel
11. Burn sheet/dressing
12. Pairs of gloves (disposable/ non sterile)
13. Stainless steel bandage scissors
14. Adhesive tape
15. Sterile multi-trauma dressing/gauze
16. Alcohol prep pads
17. Cetavlon
18. Cotton buds
19. Barrier device for CPR (pocket mask, face shield)
20. Elastoplasts/sterile adhesive dressing
21. Safety pin for triangular bandages
22. Thermometer
23. First aid manual
24. Waterproof waste bag
INTRODUCTION TO
POWER PLANTS
(A power plant known as energy conversion station )
A power plant is assembly of systems or subsystems to generate electricity, i.e., power
with economy and requirements. The power plant itself must be useful economically
and environmental friendly to the society.
generation. While the stress is on energy efficient system regards conventional power
systems viz., to increase the system conversion efficiency the supreme goal is to
develop, design, and manufacturer the non-conventional power generating systems in
coming decades preferably after 2050 AD which are conducive to society as well as
having feasible energy conversion efficiency and non-friendly to pollution,
keeping in view the pollution act. The subject as a whole can be also stated as modern
power plants for power electricity generation in 21st century. The word modern means
pertaining to time. At present due to energy crisis the first goal is to conserve energy for
future A power plant may be defined as a machine or assembly of equipment that
generates and delivers a flow of mechanical or electrical energy. The main equipment
for the generation of electric power is generator. When coupling it to a prime mover runs
the generator, the electricity is generated. The type of prime move determines, the type
of power plants. The major power plants, which are discussed in this book, are,
Different prime movers installed for power plants
Basic concept of modern power plants
The modern power complex consists on Steam and Gas Turbine has three major
concepts.
S/No. Name and History Concept
1 Willian Rankine‘s (1845~1865)
Thermodynamics
Where heat is added in water boiler to
convert heat into work
2 George Brayton (1872)
Thermodynamics
Where heat is added and discharged
at constant pressure
3 Michael Faraday (1831)
discovery of induction in 1831
When a permanent magnet is moved
relative to a conductor, or vice versa,
an electromotive force is created. If
the wire is connected through an
electrical load, current will flow, and
thus electrical energy is generated
Faraday's iron ring apparatus. Change in the magnetic flux of the left coil induces a
current in the right coil.
Entropy of Rankine Cycle
Where heat is added in water boiler to convert heat into work
Entropy of Braytone Cycle
Where heat is added and discharged at constant pressure
Types of Power Plants
1. Conventional Power Plants.
Those power plants, which can be installed at any
where easily i.e. Thermal Power Plants.
2. Non-conventional Power Plants.
Those Power Plants, which cannot be installed at any
where easily i.e. Wind Electric Power.
Those power plants, which produce electricity by
converting chemical into electric energy called thermal
power plant.
Different categories of power plants
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
Combined cycle power plant
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
Combined Cycle Plant for Power Generation:
Introduction
The process for converting the energy in a fuel into electric power involves the creation
of mechanical work, which is then transformed into electric power by a generator,
causing efficiency losses in the process. Depending on the fuel type and
thermodynamic process, the overall efficiency of this conversion is typically around 30 –
40%. This means that a significant amount of the latent energy of the fuel ends up
wasted. Much of this wasted energy ends up as thermal energy in the hot exhaust
gases from the combustion process.
To increase the overall efficiency of electric power plants, multiple processes can be
combined to recover and utilize the residual heat energy in hot exhaust gases. In
combined cycle mode, power plants can achieve electrical efficiencies of up to 60
percent. The term ―combined cycle‖ refers to the combining of multiple thermodynamic
cycles to generate power. Combined cycle operation employs a heat recovery steam
generator (HRSG) that captures heat from high temperature exhaust gases to produce
steam, which is then supplied to a steam turbine to generate additional electric power.
The process for creating steam to produce work using a steam turbine is based on
the Rankine cycle.
The most common type of combined cycle power plant utilizes gas turbines and is
called a combined cycle gas turbine (CCGT) plant. Because gas turbines have low
efficiency in simple cycle operation, the output produced by the steam turbine accounts
for about half of the CCGT plant output. There are many different configurations for
CCGT power plants, but typically each GT has its own associated HRSG, and multiple
HRSGs supply steam to one or more steam turbines. For example, at a plant in a 2x1
configuration, two GT/HRSG trains supply to one steam turbine; likewise there can be
1x1, 3x1 or 4x1 arrangements. The steam turbine is sized to the number and capacity of
supplying GTs/HRSGs.
Combined Cycle Principles of Operation
The HRSG is basically a heat exchanger, or rather a series of heat exchangers. It is
also called a boiler, as it creates steam for the steam turbine by passing the hot exhaust
gas flow from a gas turbine or combustion engine through banks of heat exchanger
tubes. The HRSG can rely on natural circulation or utilize forced circulation using
pumps. As the hot exhaust gases flow past the heat exchanger tubes in which hot water
circulates, heat is absorbed causing the creation of steam in the tubes. The tubes are
arranged in sections, or modules, each serving a different function in the production of
dry superheated steam. These modules are referred to as economizers, evaporators,
super heaters /re heaters and pre heaters.
The economizer is a heat exchanger that preheats the water to approach the saturation
temperature (boiling point), which is supplied to a thick-walled steam drum. The drum is
located adjacent to finned evaporator tubes that circulate heated water. As the hot
exhaust gases flow past the evaporator tubes, heat is absorbed causing the creation of
steam in the tubes. The steam-water mixture in the tubes enters the steam drum where
steam is separated from the hot water using moisture separators and cyclones. The
separated water is re circulated to the evaporator tubes. Steam drums also serve
storage and water treatment functions. An alternative design to steam drums is a once-
through HRSG, which replaces the steam drum with thin-walled components that are
better suited to handle changes in exhaust gas temperatures and steam pressures
during frequent starts and stops. In some designs, duct burners are used to add heat to
the exhaust gas stream and boost steam production; they can be used to produce
steam even if there is insufficient exhaust gas flow.
Saturated steam from the steam drums or once-through system is sent to the super
heater to produce dry steam which is required for the steam turbine. Pre heaters are
located at the coolest end of the HRSG gas path and absorb energy to preheat heat
exchanger liquids, such as water/glycol mixtures, thus extracting the most economically
viable amount of heat from exhaust gases.
The superheated steam produced by the HRSG is supply to the steam turbine where it
expands through the turbine blades, imparting rotation to the turbine shaft. The energy
delivered to the generator drive shaft is converted into electricity. After exiting the steam
turbine, the steam is sent to a condenser which routes the condensed water back to the
HRSG.
CCGT Design Considerations
Designs and configurations for HRSGs and steam turbines depend on the exhaust gas
characteristics, steam requirements, and expected power plant operations. Because the
exhaust gases from a gas turbine can reach 600ºC, HRSGs for GTs may produce
steam at multiple pressure levels to optimize energy recovery; thus they often have
three sets of heat exchanger modules – one for high pressure (HP) steam, one for
intermediate pressure (IP) steam, and one for low pressure (LP) steam. The high
pressure steam in a large CCGT plant can reach 40 – 110 bar. With a multiple-pressure
HRSG, the steam turbine will typically have multiple steam admission points. In a three-
stage steam turbine, HP, IP and LP steam produced by the HRSG is fed into the turbine
at different points.
The HRSGs present operational constraints on the CCGT power plant. As the HRSGs
are located directly downstream of the gas turbines, changes in temperature and
pressure of the exhaust gases cause thermal and mechanical stress. When CCGT
power plants are used for load-following operation, characterized by frequent starts and
stops or operating at part-load to meet fluctuating electric demand, this cycling can
cause thermal stress and eventual damage in some components of the HRSG. The HP
steam drum and super heater headers are more prone to reduced mechanical life
because they are subjected to the highest exhaust gas temperatures. Important design
and operating considerations are the gas and steam temperatures that the module
materials can withstand; mechanical stability for turbulent exhaust flow; corrosion of
HRSG tubes; and steam pressures that may necessitate thicker-walled drums. To
control the rate of pressure and temperature increase in HRSG components, bypass
systems can be used to divert some of the GT exhaust gases from entering the HRSG
during startup.
The HRSG takes longer to warm up from cold conditions than from hot conditions. As a
result, the amount of time elapsed since last shutdown influences startup time. When
gas turbines are ramped to load quickly, the temperature and flow in the HRSG may not
yet have achieved conditions to produce steam, which causes metal overheating since
there is no cooling steam flow. In 1x1 configurations, the operation of the steam turbine
is directly coupled to the GT/HRSG operation, limiting the rate at which the power plant
can be ramped to load. Steam conditions acceptable for the steam turbine are dictated
by thermal limits of the rotor, blade, and casing design.
Control equipment for nitrogen oxides (N Ox) and carbon monoxide (CO) emissions are
integrated into the HRSG. As these systems operate efficiently over a narrow range of
gas temperatures, they are often installed between evaporator modules.
Flexible Combined Cycle: The Flexi cycle Power
Plant
The Flexi cycle power plant is a combined cycle power plant with unique characteristics
based on Wärtsilä gas or dual-fuel combustion engines. Because combustion engines
convert more of the fuel energy into mechanical work, they have higher simple cycle
efficiencies, averaging near 50 percent. The exhaust gases from reciprocating internal
combustion engines are around 360ºC, much lower temperature than GT exhaust. Due
to the lower exhaust gas temperatures, HRSGs designed for combustion engine power
plants are much simpler in design, creating steam at one pressure level – approximately
15 bar. The steam turbine process adds approximately 10-20% to the efficiency of the
Flexi cycle power plant.
In a Flexi cycle power plant, each combustion engine generator set has an associated
HRSG. Bypass valves are used to control the admission of steam to the steam turbine
when an engine set is not operating. One engine can be used to preheat all the HRSG
exhaust gas boilers with steam to keep the HRSGs hot and enable fast starting. Flexi
cycle power plants combine the advantages of high efficiency in simple cycle and the
modularity of multiple engines supplying the steam turbine. The steam turbine can be
run with only 25 percent of the engines at full load, or 50 percent of the engines at half
load. For a 12-engine power plant of around 200 megawatts (MW), this means only
three of the engines need to be operating to produce enough steam to run the steam
turbine. The result is a very efficient power plant that retains the operational agility of a
power plant based on simple-cycle engines.
Supplementary firing and blade cooling
The HRSG can be designed with supplementary firing of fuel after the gas turbine in
order to increase the quantity or temperature of the steam generated. Without
supplementary firing, the efficiency of the combined cycle power plant is higher, but
supplementary firing lets the plant respond to fluctuations of electrical load.
Supplementary burners are also called duct burners.
More fuel is sometimes added to the turbine's exhaust. This is possible because the
turbine exhaust gas (flue gas) still contains some oxygen. Temperature limits at the gas
turbine inlet force the turbine to use excess air, above the optimal stoichiometric ratio to
burn the fuel. Often in gas turbine designs part of the compressed air flow bypasses the
burner and is used to cool the turbine blades.
combined cycle power plants Fuel for
Combined cycle plants are usually powered by natural gas, although fuel oil, synthesis
gas or other fuels can be used. The supplementary fuel may be natural gas, fuel oil, or
coal. Bio fuels can also be used. Integrated solar combined cycle power stations
combine the energy harvested from solar radiation with another fuel to cut fuel costs
and environmental impact. The first such system to come online is Yazd power plant,
Iran[3][4] and more are under construction at Hassi R'mel, Algeria and Ain Beni Mathar,
Morocco [5]. Next generation nuclear power plants are also on the drawing board which
will take advantage of the higher temperature range made available by the Brayton top
cycle, as well as the increase in thermal efficiency offered by a Rankine bottoming
cycle.
Advantages
Combined cycle power plants and cogeneration power plants that use the gas turbine
engine as their primary driver have been popular for a number of years for a number of
reasons.
Efficiencies of over 60% based on lower heating of the fuel have been achieved by
these facilities. Other fossil fuel power plants, such as plants with conventional boilers,
have efficiency in the range 40–42% for supercritical technology and 45–47% for ultra
supercritical technology based on lower heating value of the fuel.
Gaseous emissions from gas turbine–based power plants are very low. Oxidizing
catalysts can be used to convert carbon monoxide to carbon dioxide, and NOx reduction
catalysts that utilize ammonia can be used to convert oxides of nitrogen to nitrogen and
water vapor and reduce these two types of emissions to 2 ppm. Due to their high
efficiency and the fact that they usually burn natural gas fuel, gas turbine–based power
plants also emit far less carbon dioxide than other types of fossil fuel power plants.
Capital cost is lower than other power plants.
Reasonably priced natural gas (primarily due to the development of shale gas) is
available at least in the US market.
They have a small footprint and do not require much space when compared to other
modes of power generation.
A small operating and maintenance staff is all that is required.
It is relatively easy to permit them.
Construction time is short compared to other types of power plants.
Lastly, due to its ability to start up quickly and respond to demand changes rapidly, the
combined cycle power plant has become the ideal companion for renewable power
generation sources such as wind energy and solar energy, whose output is variable.
Integrated gasification combined cycle (IGCC)
An integrated gasification combined cycle, or IGCC, is a power plant using synthetic gas
(syngas).
Automotive use
Combined cycles have traditionally only been used in large power plants. BMW,
however, has proposed that automobiles use exhaust heat to drive steam turbines.[7]
This can even be connected to the car or truck's cooling system to save space and
weight, but also to provide a condenser in the same location as the radiator and
preheating of the water using heat from the engine block. However, sterling engines can
also be used if light weight is a priority (such as in a sports car or racing application),
because they use air rather than water as the working fluid.
It may be possible to use the pistons in a reciprocating engine for both combustion and
steam expansion like in the Crower six stroke.[8]
Aero motive use
Some versions of the Wright R-3350 were produced as turbo-compound engines. Three
turbines driven by exhaust gases, known as power recovery turbines, provided nearly
600 hp at takeoff. These turbines added power to the engine crankshaft through bevel
gears and fluid couplings.
more than one thermodynamic cycle. Heat engines are only able to use a portion of the
energy their fuel generates (usually less than 50%). ...
en.wikipedia.org/wiki/Combined cycle power plant
cycle burns a fuel inside a gas turbine, and the gas turbine drives an electric generator.
Abstract:
This chapter deals with the theory behind power plants with particular reference
to cogeneration and combined cycle power plants (CCPPs). The two key cycles are the
Brayton (gas turbine) and Rankine (steam turbine) cycles, within each of which there
are further subdivisions. A combination of the Brayton and Rankine cycles, often known
as the combined cycle, has been found to obtain efficiencies as high as 60% and
consequently is now used extensively worldwide as the main source of power. It is also
more commonly being used in combined heat and power (CHP) plants that provide
power and other sources of energy such as heat and air conditioning for major
complexes or parts of cities. The chapter also deals with availability and reliability of
major power plants and with power plant emissions and techniques to contain the
emissions from these plants. Gas steam combined cycle power plants have been
playing an important role in peak shaving of a power grid. The increasingly complexity
of power demand and power supply structure puts forward higher requirements for
flexible operation, which is characterized by frequent load changes and start-stop
operation. Under such circumstances, obtaining an optimal operation strategy becomes
essential for profitability of combine cycle power plants. In this paper, a thermodynamic
model comprising key functional modules of a combined cycle power plant and its
overall cycle process are presented. An economic analysis method based on heat
consumption rate is proposed. The proposed model is applied in a combined cycle
power plant in China, and quantitative impacts of flexible operation on maintenance cost
are discussed. Results show that the model can reflect the thermal economy of the
power plant under variable environmental conditions. The economic analysis shows that
there are significant economic differences between different flexible operation cases
GAS TURBINE
Gas Turbine for Power Generation: Introduction
The use of gas turbines for generating electricity Today, gas turbines are one of the
most widely-used power generating technologies. Gas turbines are a type of internal
combustion (IC) engine in which burning of an air-fuel mixture produces hot gases that
spin a turbine to produce power. It is the production of hot gas during fuel combustion,
not the fuel itself that the gives gas turbines the name. Gas turbines can utilize a variety
of fuels, including natural gas, fuel oils, and synthetic fuels. Combustion occurs
continuously in gas turbines, as opposed to reciprocating IC engines, in which
combustion occurs intermittently.
How Do Gas Turbines Work
Gas turbines are comprised of three primary sections mounted on the same shaft: the
compressor, the combustion chamber (or combustor) and the turbine. The compressor
can be either axial flow or centrifugal flow. Axial flow compressors are more common in
power generation because they have higher flow rates and efficiencies. Axial flow
compressors are comprised of multiple stages of rotating and stationary blades (or
stators) through which air is drawn in parallel to the axis of rotation and incrementally
compressed as it passes through each stage. The acceleration of the air through the
rotating blades and diffusion by the stators increases the pressure and reduces the
volume of the air. Although no heat is added, the compression of the air also causes the
temperature to increase.
The compressed air is mixed with fuel injected through nozzles. The fuel and
compressed air can be pre-mixed or the compressed air can be introduced directly into
the combustor. The fuel-air mixture ignites under constant pressure conditions and the
hot combustion products (gases) are directed through the turbine where it expands
rapidly and imparts rotation to the shaft. The turbine is also comprised of stages, each
with a row of stationary blades (or nozzles) to direct the expanding gases followed by a
row of moving blades. The rotation of the shaft drives the compressor to draw in and
compress more air to sustain continuous combustion. The remaining shaft power is
used to drive a generator which produces electricity. Approximately 55 to 65 percent of
the power produced by the turbine is used to drive the compressor. To optimize the
transfer of kinetic energy from the combustion gases to shaft rotation, gas turbines can
have multiple compressor and turbine stages.
Because the compressor must reach a certain speed before the combustion process is
continuous – or self-sustaining – initial momentum is imparted to the turbine rotor from
an external motor, static frequency converter, or the generator itself. The compressor
must be smoothly accelerated and reach firing speed before fuel can be introduced and
ignition can occur. Turbine speeds vary widely by manufacturer and design, ranging
from 2,000 revolutions per minute (rpm) to 10,000 rpm. Initial ignition occurs from one or
more spark plugs (depending on combustor design). Once the turbine reaches self-
sustaining speed – above 50% of full speed – the power output is enough to drive the
compressor, combustion is continuous, and the starter system can be disengaged.
Parts of Gas Turbine
1. Filter House
2. Axial Flow Compressor
3. Combustion Chamber
4. Gas Turbine
Filter House
It consists of 1200 approx. air inlet filter which cleans atmospheric air for compressor.
These filters are cartridge type and their use full life is around 2 years further due to
these air inlet filer hard particulars cannot penetrate into compressor.
Axial Flow Compressor
This compressor intake air through air inlet filters and sent into combustion chamber.
The air is pases through different stages and attains pressure & temperature. On every
stage the temp and pressure arises with a certain ratio. Compressor has 16 stages and
its comparison ratio is 1-10 bar. Thus if the inlet pressure is 1 bar then compressor
outlet pressure will be 10bar and temperature arises upto 355 0
C. This mean at every
stage temperature raises upto 22 0
C and in final this compressed and temperature air
enter into combustion chamber
Combustion Chamber
Combustion chamber is that part of turbine where energy converts from chemical
energy to heat energy. Some gas turbines have 14 combustors and hot gases are
passes through each combustor and enter into turbine. Some gas turbines have 02
combustion chambers and contain 8 burners.
Gas Turbine Performance
The thermodynamic process used in gas turbines is the Braton cycle. Two significant
performance parameters are the pressure ratio and the firing temperature. The fuel-to-
power efficiency of the engine is optimized by increasing the difference (or ratio)
between the compressor discharge pressure and inlet air pressure. This compression
ratio is dependent on the design. Gas turbines for power generation can be either
industrial (heavy frame) or aero derivative designs. Industrial gas turbines are designed
for stationary applications and have lower pressure ratios – typically up to 18:1. Aero
derivative gas turbines are lighter weight compact engines adapted from aircraft jet
engine design which operate at higher compression ratios – up to 30:1. They
offer higher fuel efficiency and lower emissions, but are smaller and have higher initial
(capital) costs. Aero derivative gas turbines are more sensitive to the compressor inlet
temperature.
The temperature at which the turbine operates (firing temperature) also impacts
efficiency, with higher temperatures leading to higher efficiency. However, turbine inlet
temperature is limited by the thermal conditions that can be tolerated by the turbine
blade metal alloy. Gas temperatures at the turbine inlet can be 1200ºC to 1400ºC, but
some manufacturers have boosted inlet temperatures as high as 1600ºC by engineering
blade coatings and cooling systems to protect metallurgical components from thermal
damage.
Because of the power required to drive the compressor, energy conversion efficiency for
a simple cycle gas turbine power plant is typically about 30 percent, with even the most
efficient designs around 40 percent. A large amount of heat remains in the exhaust gas,
which is around 600ºC as it leaves the turbine. By recovering that waste heat to produce
more useful work in a combined cycle configuration, gas turbine power plant efficiency
can reach 55 to 60 percent. However, there are operational limitations associated with
operating gas turbines in combined cycle mode, including longer startup time,
purge requirements to prevent fires or explosions, and ramp rate to full load.
Typical performance values for new gas turbines
Gas turbine type
Power output
(MW el)
Efficiency,
Simple cycle (%), LHV
Efficiency,
Combined cycle (%), LHV
Aeroderivative 30-60 39-43 51-54
Small scale heavy duty 70-200 35-37 53-55
Large scale heavy duty 200-500 37-40 54-60
Gas Turbine Theory
A simple gas turbine is comprised of three main sections a compressor, a combustor,
and a power turbine. The gas-turbine operates on the principle of the Brayton cycle,
where compressed air is mixed with fuel, and burned under constant pressure
conditions. The resulting hot gas is allowed to expand through a turbine to perform
work. In a 33% efficient gas-turbine approximately two / thirds of this work is spent
compressing the air, the rest is available for other work ie.( mechanical drive, electrical
generation)
One variation of this basic cycle is the addition of a regenerator. A gas-turbine with a
regenerator (heat exchanger) recaptures some of the energy in the exhaust gas, pre-
heating the air entering the combustor. This cycle is typically used on low pressure ratio
turbines.
Gas-turbines with high pressure ratios can use an intercooler to cool the air between
stages of compression, allowing you to burn more fuel and generate more power.
Remember, the limiting factor on fuel input is the temperature of the hot gas created,
because of the metallurgy of the first stage nozzle and turbine blades. With the
advances in materials technology this physical limit is always climbing.
GAS-TURBINE HISTORY
The history of the gas turbine begins with a quest for jet propulsion.
Gas Turbine Theory
The earliest example of jet propulsion can be traced as far back as 150 BC to an
Egyptian named Hero. Hero
invented a toy that rotated on
top of a boiling pot due to the
reaction effect of hot air or
steam exiting several nozzles
arranged radially around a
wheel. He called this invention
an aeolipile.
In 1232 the Chinese used
rockets to frighten enemy
soldiers.
Around 1500 A.D. Leonardo da
Vinci drew a sketch of a device
that rotated due to the effect of
hot gasses flowing up a
chimney. The device was
intended to be used to rotate
meat being roasted. In 1629
another Italian named Giovanni
Branca actually developed a
device that used jets of steam to rotate a turbine that in turn was used to operate
machinery. This
was the first
practical
application of a
steam turbine.
Ferdinand
Verbiest a Jesuit
in China built a
model carriage
that used a
steam jet for
power in 1678.
The first patent for a turbine engine was granted in 1791 to an Englishman named John
Barber. It incorporated many of the same elements of a modern gas turbine but used a
reciprocating compressor. There are many more early examples of turbine engines
designed by various inventors, but none were considered to be true gas turbines
because they incorporated steam at some point in the process.
In 1872 a man by the name of Stolze designed the first true gas turbine. His engine
incorporated a multistage turbine section and a multi stage axial flow compressor. He
tested working models in the early 1900's.
Charles Curtis the inventor of the Curtis steam engine filed the first patent application in
the U.S. for a gas turbine engine. His patent was granted in 1914 but not without some
controversy.
The General Electric company started their gas turbine division in 1903. An engineer
named Stanford Moss lead most of the projects. His most outstanding development was
the General Electric turbosupercharger during world war 1. ( Although credit for the
concept is given to Rateau of France.) It used hot exhaust gasses from a reciprocating
engine to drive a turbine wheel that in turn drove a centrifugal compressor used for
supercharging. The evolutionary process of turbosupercharger design and construction
made it possible to construct the first reliable gas turbine engines.
Sir Frank Whittle of Great Britain patented a design for a jet aircraft engine in 1930.He
first proposed using the gas turbine engine for propulsion in 1928 while a student at the
Royal Air Force College in Cramwell, England. In 1941 an engine designed by Whittle
was the first successful turbojet airplane flown in Great Britain.
Concurrently with Whittle's development efforts, Hans von Ohain and Max Hahn, two
students at Gottingen in Germany developed and patented their own engine design in
1936 these ideas were adapted by The Ernst Heinkel Aircraft company. The German
Heinkel aircraft company is credited with the first flight of a gas turbine powered jet
propelled aircraft on August 27th 1939.The HE178 was the first jet airplane to fly.
The Heinkel HeS-3b developed 1100 lbs. of thrust and flew over 400 mph, later came
the ME262, a 500 mph fighter, more than 1600 of these were built by the end of WWII.
These engines were more advaced than the British planes and had such features as
blade cooling and a variable area exhaust nozzles.
In 1941Frank Whittle began flight tests of a turbojet engine of his own design in
England. Eventually The General Electric company manufactured engines in the U.S.
based on Whittle's design.
SFC CIRCUIT
SFC Static Frequency Converter
Frequency converter converts the frequency of ac current, that is it converts a 50 or 60
hz ac current to ac current of any desired frequency. The device may also change the
voltage if it is required.
Static frequency Converter (SFC). Function of SFC is to change the generator into the
motor at start up process. This will rotate gas turbine for combustion. After
combustion, gas turbine can turn generator then it SFC auto stop at 2000 rpm.
1 Introduction. The PCS100 Static Frequency Converter (SFC) is a low voltage (LV)
AC-AC power electronic converter system. While the converter integrates all the
electronics and sine wave filtering, it does require an isolation transformer for correct
operation
Static Frequency Converter Analysis
Induction motor speed control requires a 3-phase power supply that can vary both
voltage and frequency. Such a power supply creates a variable speed rotating field in
the stator that allows the rotor to spin at the required speed with low slip. The static
frequency converter can efficiently provide full torque from zero speed to full speed, can
over speed if necessary, and can, by changing phase rotation, easily provide bi-
directional operation of the induction motor.
Although the principles of static frequency converters are not new, advances in power
semiconductors, control electronics, and microprocessors have increased their
popularity. Adding to this are vector control methods that give the static frequency
converter the capability and flexibility.
Static Frequency Converter
Following figure shows the essential elements of a static frequency converter. The 3-
phase supply is rectified and filtered to produce a DC bus, which powers the inverter
section of the static frequency converter. The inverter consists of three pairs of
semiconductor switches (MOSFET, GTO, power transistor, IGBT, etc.) with associated
diodes. Each pair of switches provides the power output for one phase of the motor.
Each pair of semiconductor switches is driven by the control electronics to generate a
high frequency square wave carrier pulse waveform at each of the phase outputs.
Since the carrier is identical on all three phases, the net voltage appearing across any
phase of the motor windings due to the carrier alone is zero. In order to drive the motor,
the control electronics generate three low-frequency sine waves, 120 degrees apart,
which modulate the carrier pulses to each pair of switches. The width of positive and
negative pulse within each carrier cycle is modulated according to the amplitude of the
low frequency sine waveform of that phase. As a result, the average voltage presented
to the motor winding is approximately sinusoidal. The two other phases of the motor
winding have similar average voltages spaced 120 degrees apart.
Most frequency converters operate with a fixed carrier frequency that is several times
higher than the highest output frequency that is to be used. As static static frequency
converters operate with an output frequency from a few Hz up to about 100 Hz, they
use a carrier frequency in the range of 2 kHz up to about 10 kHz. As power
semiconductors improve, the trend is to increase carrier frequencies up to ultrasonic
frequencies (> 18 kHz), which can lower losses in the motor since the current is more
sinusoidal. The down side is higher switching losses in the inverter and potential for
more radiated frequency noise. Thus, careful measurements must be made on static
frequency converter input and output to make the optimum carrier frequency choice for
a given application.
Although the static frequency converter output voltage contains a large number of
frequency components other than the fundamental, these components are generally of
higher frequency and suppressed by the inductance of the motor winding. However, a
motor is not simply an inductor and it is therefore important that the modulation of the
carrier frequency be designed to produce a current that is as sinusoidal as possible. In
particular, care must be taken to minimize low order harmonic voltages as the
impedance of the motor to these voltages is low.
In practice, a static frequency converter produces a "wanted" component of current at
the fundamental frequency and "unwanted" components of current at frequencies that
are multiples or components of the fundamental frequency. The "unwanted"
components in the motor current can lead to problems such as additional heat, reduced
motor efficiency and lower power output.
The effects of these unwanted components on the operation of the motor can be
expressed by measurement of the fundamental and total output power of the inverter,
by harmonic analysis of the voltage and current waveforms, and by torque/speed
measurements on the motor. The most efficient static frequency converters are those
that not only minimize losses in the converter, but also generate the most pure current
waveforms to minimize power and torque losses.
Motor Output Measurements
Motor output measurements can be made by installing speed and torque transducers
on the output shaft of the motor to calculate output power. In order to determine the
efficiency of a motor and static frequency converter combination, the designer must
consider both the electrical input to the system, and the mechanical power produced on
the output of the motor.
System efficiency is calculated from:
(Power out / Power in) x 100%
By measuring both the electrical power consumed on the input to the static frequency
converter, as well as torque and speed on the motor‘s output, the efficiency of the
system can be measured. The simplest approach to making this measurement is with a
power analyzer that includes sensor inputs designed to connect torque and speed
transducers.
Static Frequency Converter Output
As noted previously, the output waveform of a static frequency converter is very
complex, consisting of a mixture of high frequency components due to the carrier and
components at low frequency due to the fundamental current. This presents a problem
for some power analyzers that can either measure at high frequencies, in which case
low frequency information in the waveform is lost, or they can filter the PWM waveform
to measure at low frequencies, in which case high frequency data is lost. The difficulty
occurs because the waveform is being modulated at low frequency. High frequency
measurements, such as total rms voltage or total power must therefore be made at high
frequency but over an integral number of cycles of the low frequency component in the
output waveform.
The latest power analyzers overcome this problem by using a special operating mode
for static frequency converter output measurements. The data is sampled at high speed,
and total quantities, including all harmonic and carrier components, are computed in
real time. At the same time, the sampled data is digitally filtered to provide low
frequency measurements such as fundamental and measurement of output frequency.
In addition to providing both low and high frequency results from the same
measurement, this technique allows the high frequency measurements to be
synchronized to the low frequency signal, providing high frequency measurement
results that are both accurate and stable.
To perform a static frequency converter output measurement, a power analyzer is wired
to the output in a three phase, three-wire configuration. For static frequency converters
up to 30 A rms output current, the power analyzer can be wired directly into the static
frequency converter output. For currents above this level, an external shunt or current
transducer may be required.
Once the analyzer is connected and configured, also ensure that the correct filter
frequency range has been specified. Note that the Vrms, Arms, and Watts figures are
measured from pre-filtered values and therefore include all high frequency components,
whereas the fundamental values only consider contributions to work in the motor. It is
normal to have a significant difference between the rms and fundamental voltage.
Normally there is a smaller difference in current and watts because the inductive motor
filters the current.
High frequency losses may be estimated by the difference between the total watts and
the fundamental watts read on the SUM channel. This represents electrical power
delivered by the static frequency converter which does not contribute to mechanical
output power and therefore adds to the heating of the motor.
High Frequency Losses = Total Watts – Fundamental Watts
This is a useful measurement when comparing static frequency converters.
Static Frequency Converter DC bus
Although the link between the input and the output section of the static frequency
converter is referred to as the DC bus, the voltage and current in this bus are far from
pure DC, so care must be taken in making the necessary measurements.
DC bus measurements are best made on the input side of the storage capacitors, since
the current here is essentially low-frequency capacitor charging pulses from the AC
supply, and free from the high frequency current pulses that may be drawn by the
inverter section. If DC bus measurements are made on their own, a single channel of
analyzer can be used. However, DC bus measurements are often made in conjunction
with three-phase two-wire measurements of either the input or output of a static
frequency converter. In this case the DC bus should be measured using one of the
remaining channels operating independently. Suggested DC bus measurements are
shown in following Table.
Measurement Reason
W Total power in dc bus. Can be used in efficiency calculations.
Arms RMS charging current in d.c. bus. Useful for sizing conductor or fuses.
AHO DC component of current in dc bus. This is smaller than Arms.
VHO Mean voltage across storage capacitor.
Vpk Peak voltage across storage capacitor.
Table 1. Critical Measurement parameters for frequency converter DC bus.
Static Frequency Converter Input
The input circuitry of most static frequency converters is essentially a three-phase diode
rectifier bridge with capacitor filter. The input current to such a circuit consists, on each
input phase, of pulses of current that charge the storage capacitor as show in following
figure. Input current is therefore a distorted current waveform, with a fundamental
component at supply frequency, but with considerable harmonic content.
Input current drawn is essentially independent of the converter output frequency since
the instantaneous power drawn by the static frequency converter is a constant, and
therefore the current required from the input to charge the capacitor on the DC bus is a
constant.
The analyzer is wired to the input in 3-phase 3-wire configuration. In this wiring
configuration it is possible to use a third channel of a power analyzer as an independent
channel to measure, for example, the DC bus within the static frequency converter. If
the readings vary too much, for example, when measuring on single-phase frequency
converters, increasing averaging may help stabilize the measurements.
Loss And Efficiency
On any system, measurements of losses and efficiency are best made by making
simultaneous measurements on the input and output of the system. This is particularly
important for systems with high efficiency, such as static frequency converters. If
separate measurements are made on input and output and the system is shut down
between measurements to transfer instrumentation, one cannot always be certain that
exactly the same load conditions exist for both measurements. Any unnoticed difference
in load conditions will appear as an error in measured losses.
The following method is effective for making measurements of static frequency
converter efficiency and static frequency converter losses using a single power
analyzer.
Static frequency converters are now becoming the dominant method of induction motor
variable speed controls, and are being used not only in industry, but in applications as
diverse as electric vehicles and domestic air conditioners. Static frequency converters
produce complex waveforms, both on their output to the motor, and also in the electrical
supply to the frequency converter.
The output waveform of a static frequency converter is very complex, consisting of a
mixture of high frequency components due to the carrier and components at low
frequency due to the fundamental current. This presents a problem for some power
analyzers that can either measure at high frequencies or they can filter the PWM
waveform to measure at low frequencies. Modern power analyzer overcome this
problem with a dedicated PWM mode that combines sampling and filtering to provide
accurate measurements including input, outputs and efficiency.
Abstract
Static starting devices,
also called static frequency converters (SFCs), have been utilized to start gas turbines
in gas turbine combined cycle (GTCC) power plants, etc. In general, a gas turbine is
started using a generator as a synchronous motor with a single-shaft arrangement that
is rotated by the electric power fed from the SFC. Because the rotor position signal of
the generator is indispensable for controlling the SFC, a mechanical position sensor is
installed beside the rotor shaft. However, such mechanical position sensors require
considerable time for installation and adjustment at the site. Therefore, a sensor less
control method called the advanced position sensor (APS) has been developed and
applied to an SFC. In this paper, we describe an SFC that employs this position sensor
less control method. Further, we investigate the applicability of the APS by comparing
the pulses of the two systems-APS and the traditional position sensor- observed during
start-up.
Starting for heavy-duty gas turbines
load-commutated inverter (LCI)
GE‘s LS2100e Static Starter is a
load-commutated inverter (LCI)available in
four power ratings: 8.5, 11, 14, and 22 MVA, matching the starting
requirements of the largest gas turbine in the world.
Part of the family
As a member of the GE Mark* VIe Controls Technology family, the LS2100e
communicates peer-to-peer on the Mark VIe UDH network to reduce field wiring and to
improve data coordination between the starter, Ex2100e exciter, and Mark VIe turbine
controller.
ControlST* is the common configuration tool for the GE Mark VIe controller family
including LS2100e static starter. GE‘s HMI systems utilize common operator stations
and engineer workstations to simplify plant operations and maintenance.
To save capital costs, GE‘s static starter can be configured to start more than one
turbine. This provides starting flexibility and choices between starting redundancy and
cost savings. LS2100e can be applied as part of a new unit gas turbine installation,
either as a replacement of any vintage of existing GE static starter or as a controls
migration for the Innovation Series.
Key benefits
1.Lower cost and minimal space requirement than other starting means for large gas
turbines
2.Ability to generate sufficient current for high-acceleration torque requirements
3.Common Control ST* software suite supports a wide range of starting profiles to
improve ease of operation and maintenance
4.Low mean-time-to-repair (MTTR) with detailed system diagnostics and an easy to
repair design
5.Higher power, multi start capability enabled through an integrated liquid cooling
system
6.Full system and digital front end (DFE) options to serve all starter modernization
needs
7.Controls are part of GE‘s Mark VIe family with improved lifecycle management
capabilities
8.Improved sequencing control in cross-over applications
9.Improved cooling system, sequencing, and power converter status annunciation
Configuration options include:
10.A static starter for each gas turbine
11.A static starter for multiple gas turbines (up to four)
12.Two static starters cross-linked to multiple gas turbines (up to eight)
GT ACCESSORY DRIVES , RQUECONVERTER
AND STARTINGCLUTCH
Aerodynamic Torque Converter for Gas
Turbines
A new concept in transmissions for gas turbines, called an Aerodynamic Torque
Converter, is proposed. The ATC is similar to a hydraulic torque converter but uses a
compressible working fluid which results in several unique characteristics when
combined with a gas turbine cycle. Control and operational aspects of the ATC are
discussed and equations showing its basic thermodynamic characteristics are
developed.
Definition of torque converter
: a device for transmitting and amplifying torque especially by hydraulic means
The stator directs the flow of transmission fluid inside the torque converter.— is a big
upgrade from the GT-Line trim which only uses a regular torque converter automatic
transmission.
Compressor starting torque converter
Abstract
A large compressor (18) is powered by a single-shaft gas turbine (12) via shaft (14),
gearbox (16) and a hydraulic torque converter (10), which is undersized relative to the
maximum shaft power requirement of compressor (18). The hydraulic torque converter
(10) has a lock-up device (40) that locks the impeller (24) and the turbine wheel (28) at
25% of the maximum shaft power requirement of compressor (18). Gas turbine (12) has
a starter (34). Optionally, compressor (18) has its outlet connected to auxiliary
compressor (50) that assists the starting process by decreasing the back pressure of
compressor (18).
Description
01.The present invention relates to methods and apparatus for starting single
shaft gas turbine driven or electric motor driven compressor sets, and in a further
embodiment relates to methods and apparatus for starting large single shaft gas
turbine driven compressor sets of greater than 43,700 horsepower.
Background of the Invention
02.Present compressor plants, such as those used in liquified natural gas (LNG)
plants, use either the smaller two-shaft gas turbine driver (which has no driver
compressor starting problems) or the larger, more cost-effective single-shaft gas
turbine driver with its presently-associated complex compressor starting method
and apparatus. While two-shaft gas turbine drivers are suitable for starting
compressors, they are commercially unavailable a in sizes greater than 43,700
horsepower. There is a need for a device which can efficiently start single-shaft
gas turbine driven centrifugal compressor sets in processes requiring total power
up to 350,000 horsepower and more.
03.Large single-shaft gas turbines have a standard starting system that at most
can only start up the gas turbine driver itself and an unloaded, connected electric
generator. A specific problem with the single-shaft gas turbine is that everything
is connected mechanically on a single common shaft, hence the starting device
must start up not only the gas turbine itself, but also the connected load (for
example, an electric generator or centrifugal compressor). Everything must be
started up and accelerated simultaneously from rest continuously up to full
speed. The added load produced by an electric generator in an unloaded state,
that is, not connected to the electrical power grid during starting, can be handled
by a single-shaft gas turbine's standard starting system, but not the inertia and
aerodynamic loads associated with a large centrifugal compressor.
04.For starting up large, single-shaft gas turbine compressor sets, an additional
starting device (an electric motor or steam turbine helper driver or engine) is
typically added at the outboard free end of the driven compressor . This starting
device can either be a steam turbine driver or an electric motor driver, which
typically includes a Variable Frequency Electrical Drive system (VFD) to provide
variable speed. The electric motor driver requires an external source of electric
current, while the steam turbine requires an external source of steam, hence both
starting device types are not independent or stand-alone devices. Because both
of these systems, in turn, have many sub-systems, they are costly, complex, and
are very maintenance intensive.
05.Further, many times because of a remote location, a plant does not have a
readily available nearby electrical grid or a steam system. Steam systems require
a large source of water. In addition, it is generally more economical to utilize air
instead of water for cooling.
06.It is desirable to provide a method and apparatus to start up large loads, such
as centrifugal compressors, axial compressors and the like, which is simpler,
lower in cost, and requires less maintenance than the systems currently
available.
Summary of the Invention
07.Accordingly, it is desirable to provide a less costly, less complex, less
maintenance-intensive, more reliable and more efficient device and method
utilizing proven equipment for starting up compressors and specifically single-
shaft, gas turbine-driven or electric motor-driven compressor sets.
08.Again it is desirable to provide a device and method that can be used to start
up centrifugal compressors, axial compressors, and combinations thereof.
09.Once again it is desirable to allow the more cost-effective single-shaft gas
turbine to be used more readily for gas turbine compressor drivers.
10.In carrying out these and other objects of the invention, there is provided, in
one form, a power transmission system for driving at least one compressor. The
system has a driver, where one end of the shaft is the driver output shaft. A
compressor starting torque converter (CSTC) is also present which has a pump
impeller on an input shaft and a turbine wheel on an output shaft, where the
CSTC input shaft is coaxially connected to the driver output shaft. Further, there
is a compressor with an input shaft coaxially connected to the CSTC output shaft.
The CSTC further comprises a lock-up device between the pump impeller and
the turbine wheel to lock the impeller and the turbine wheel together. The driver
may be a single shaft gas turbine or an electric motor. The compressor may be a
centrifugal compressor, an axial compressor or a combination thereof.
11.It will be appreciated that the Figures are not to scale or proportion as it is
simply a schematic for illustration purposes. Even in the schematic, the
compressor starting torque converter (CSTC) is oversized with respect to the
other components of the system, to show detail.
Detailed Description of the Invention
13.The invention herein employs an improved starting method for starting
compressors and specifically compressor trains driven by a single shaft gas
turbine machine, such as are used in liquefied natural gas (LNG) plants, namely,
using a compressor starting torque converter (CSTC) located between the gas
turbine output shaft and the compressor input shaft. Preferably the compressor is
either a centrifugal compressor, an axial compressor or a combination of the two.
Most preferably the compressor is a centrifugal compressor.
14.Referring to FIG.1 in general terms, the CSTC consists of a torque converter
(which can be drained of its working oil ) and a lock-up device that mechanically
connects the gas turbine's output shaft to the driven compressor's input shaft .
15.Briefly, there are two operating modes for the CSTC namely (i) "Start-Up" and
(ii) "Normal Operation". "Start-Up" involves the filled torque converter being in
operation while in "Normal Operation", the torque converter is drained and out of
operation while the lock-up device is engaged mechanically connecting the gas
turbine directly to the compressor (and not via the fluid 30 in the torque
converter as in "Start-Up"). Briefly, in use, oil is first drained from the CSTC's
torque converter to uncouple the driven centrifugal compressor from the gas
turbine , and then the gas turbine is started conventionally. With the gas turbine
at minimum governing speed, the CSTC is re-filled and then the centrifugal
compressor is started by increasing the power output from the gas turbine .
Once the centrifugal compressor is up to a speed which closely matches the gas
turbine speed, a lock-up device is activated mechanically connecting the gas
turbine to the centrifugal compressor .
16.While the invention is expected to find utility in starting up compressors for
LNG plants and other closed refrigeration cycles, particularly propane
refrigeration cycles, it is expected that the invention will find utility in starting and
driving compressors, preferably centrifugal and/or axial compressors, in other
type processes, utilizing single-shaft gas turbine drivers or electric motors.
17.The invention will be described more specifically with reference to FIG. 1.
Shown in FIG. is a power transmission system , having a single shaft gas turbine
(GT) , a CSTC and at least one compressor with their respective shafts in
coaxial alignment. A conventional gearbox may be present between the output
shaft of the single shaft gas turbine and the input shaft of the CSTC only if the
speed of turbine and required speed of compressor do not match.
18.The CSTC is an enclosed mechanical device consisting of an input shaft
having centrifugal pump impeller thereon and an independent output shaft
having an associated turbine wheel thereon. The working medium is oil or other
suitable hydraulic fluid, and when the centrifugal pump impeller is rotated by
having energy put into it from the gas turbine , the turbine wheel rotates, that is,
energy is transmitted out of CSTC via output shaft . In other words, the
mechanical energy input to the input shaft and centrifugal pump impeller is first
transformed into hydraulic energy by the pump impeller , and then converted
from hydraulic energy back into mechanical energy by the turbine wheel and
delivered out of CSTC by output shaft , which in FIG. 1 is identical to the input
shaft of compressor . The arrows in FIG. 1 show the circulation path of the oil .
19.Two shafts ( and ) hydraulically coupled by a fluid (oil ) is defined as a fluid
coupling, while a fluid coupling with guide vanes in the fluid circulation path is
defined as a torque converter, a well-known machine perhaps most commonly
encountered in the automatic transmission of automobiles. The orientation of the
guide vanes help determine the torque amplification produced by the CSTC .
20.A torque converter has a characteristic torque output (or twisting capacity)
curve of maximum torque output at zero speed, with decreasing torque output at
increasing speed. This is ideal because the driven compressor has the exact
opposite torque input requirements, and a characteristic curve of zero torque at
zero speed and increasing torque with increasing speed. The excess available
output torque of a torque converter at low speeds over the small input torque
required by the compressor results in the ability of the gas turbine driver to
accelerate the large mass and inertia of the driven compressor (s) from rest up
to speed.
21.A unique feature of the CSTC is the ability to drain and refill the unit of its
operating fluid , which is the media used for transmitting energy and the
transformation of energy. The mechanical shaft energy input into the CSTC is
transmitted by and transformed by the fluid in the unit into mechanical shaft
output energy, when the lock up device is not activated. By draining the fluid
from the CSTC , the input shaft and output shaft are physically decoupled,
meaning that there is no connection whatsoever between the input shaft with the
output shaft .
22.The basic operating principle behind the CSTC (as used in the power
transmission system shown) is to first drain the CSTC of its fluid , and allow the
single shaft gas turbine 's standard starting device to start the gas turbine itself.
Once operational, the starting device is dropped out of operation and the gas
turbine brings itself up to minimum governing speed as it normally would if it were
connected to an unloaded electrical generator (not shown). Conventional starting
device typically drops out and is disconnected once the gas turbine is up to
about 40% of operating speed. Such starting devices or motors typically produce
approximately 300 to 1,000 hp and greater. However in the case of the invention,
the job is easier as there is no connected electrical generator or other load. Once
the gas turbine is up to speed and ready to accept load, the CSTC is re-filled
and the compressor(s) brought up to speed by the gas turbine driver through the
CSTC in a timed manner.
23.In other words, the fundamental principle is a device which allows the driven
compressor (s) to be isolated (de-coupled) from the gas turbine driver , allowing
the gas turbine's standard starter system to start and bring the gas turbine itself
up to self-sustaining speed, without the driven compressor. When the gas turbine
is operational, up to minimum governing speed and ready to be loaded, the gas
turbine driver, through the CSTC , starts up the compressor . Although torque
converter operation during start-up is inefficient, it is quite short term. Once
locked-up, as during normal operation, the torque converter is no longer in
operation. An additional advantage of the invention is that start-up time is
reduced significantly, as compared with prior art processes. Starting up the
compressor using the procedure of this invention is estimated to take from about
0.5 to about 2.0 minutes.
24.Although normally a single-shaft gas turbine cannot start up both itself and a
centrifugal compressor from rest, it can start the compressor 1once the turbine
itself is operational and up to speed. The CSTC makes this possible. In essence,
there is a two-phase start-up. First, the gas turbine itself is started, then the gas
turbine starts the compressor by means of the CSTC .
25.Once the compressor (s) are up to speed, or output shaft (compressor input
shaft) speed at least closely matches (to within 2 % of its speed) CSTC input
shaft speed, lock up device is engaged to physically connect gas turbine to
centrifugal compressor . Lock up device , shown in more detail in FIG. 3, has a
circular, one piece lock-up ring having teeth on the inside and outside thereof,
and is mechanically bolted to a circular, single piece engagement piston .
Hydraulic pressure moves the locking ring /engagement piston towards the
centrifugal pump impeller (to the left in FIGS. 1 and 3) to physically connect
pump impeller with turbine wheel . The hydraulic fluid to move locking ring
/engagement piston is admitted through engagement piston hydraulic fluid inlet .
The CSTC thus becomes a mechanical connection device or gear coupling with
extremely low power transmission loss. In one non-limiting embodiment, the
transmission efficiency would be approximately 99.5% in lock-up mode
(approximately 0.5% power loss). This is the "Normal Operation" Mode for the
gas turbine/CSTC/compressor unit of system and in this mode, the compressor
would inherit the speed variation capability of the gas turbine .
26.Also shown in FIG. 1 is compressor discharge line , high stage flash gas
stream , intermediate stage flash gas stream , and low stage flash gas stream
returning back to compressor . On existing processes and apparatus, as shown
in prior art FIG. 2, if the start-up motor or stream turbine driver (located at the
free, non-driven shaft end of compressor ) is not large enough, the gas pressure
inside compressor has to be reduced, typically by venting it, sometimes down to
almost a vacuum, in order to get compressor started. With the present invention,
the compressor does not have to be vented thus avoiding losing a valuable gas
like propane to the atmosphere.
27.If the CSTC or other equipment is not powerful enough to start compressor ,
one option is to add a small auxiliary compressor parallel to and in the
compressor discharge line to draw down the pressure somewhat. Lowering the
pressure in the process loop lowers compressor start-up power requirements. In
one non-limiting embodiment, auxiliary compressor is envisioned to be a screw
compressor.
28.An advantage of the CSTC of the invention is that it is a simple, independent,
self-sufficient, stand-alone mechanical device that is not a driver or an engine,
and thus does not have the complexities and costs associated with a driver or
engine nor requires an external power source. While by itself, the CSTC is not a
starting device, when skillfully used in conjunction with a single-shaft gas turbine
, it allows the single-shaft gas turbine itself to act as the driver to start up the
driven compressor(s) , a feat a single-shaft gas turbine normally cannot do. In
other words, another complicated driver is not required to start up the total gas
turbine compressor system.
29.The invention permits single-shaft gas turbine drivers to be readily used
instead of steam turbine drivers. Steam turbine drivers do not have centrifugal
compressor start-up problems because-its high pressure motive fluid (steam) is
available (from a separate source) before compressor start-up while in a single-
shaft gas turbine no hot motive fluid (gas from the gas turbine itself) is available
until the gas turbine is started and is up and running. Gas turbines are a less
costly alternative to steam turbine drivers because no steam generation
equipment is needed and the cooling system is smaller. Gas turbines have a
higher thermal efficiency than steam turbines, are more compact, more reliable,
and offer a faster start-up. Further, the time taken to manufacture and install a
gas turbine is shorter than for a comparable steam turbine system.
30.In another embodiment, the CSTC also can eliminate costly, special and
complex motors with variable frequency drives for future motor-driven integrally-
geared LNG compressors. The CSTC will allow standard, less costly and more
reliable fixed speed electric motors to be used. The main drive electric motor can
be started up unloaded by using a small electric motor starter with the CSTC
drained mechanically isolating the main drive motor from the compressor. After
the main drive electric motor is brought up unloaded to full speed and then
connected to the electric grid, the CSTC can be filled and the compressor
started. Although little or no speed control is available with the CSTC in this
arrangement, compressor capacity control can still be obtained, for example, by
adding compressor inlet guide vanes (a standard option on integrally-geared
compressors employed in LNG liquefaction processes and on some normal
centrifugal compressors).
31.An additional advantage of the invention is that if there is a process trip or
problem, the invention permits only the compressor or other process to cease
without necessarily tripping the gas turbine . The procedure would be to first
unload the compressor until the lock-up device can be disengaged and allow the
compressor to coast to a standstill while the gas turbine is kept operational but at
minimal speed. Stopping and re-starting a gas turbine is a complicated, lengthy
process one tries to avoid.
32.A related advantage of the invention is ease of maintenance. In the present
invention, the compressor , as one example, is automatically decoupled from the
gas turbine upon draining of the torque converter and the compressor can then
be serviced with no fear of physical danger to repair personnel and surrounding
equipment.
33.Starting-up a gas turbine is a complex, detailed procedure as it is by nature a
mini power plant which runs hot hence rate of temperature rise throughout the
machine must be regulated and controlled in a very strict manner. Thus starting-
up, shutting down and restarting of a gas turbine is to be avoided or at least
minimized as much as possible. The absolute best operating condition for a gas
turbine is continuous operation as starting and stopping shortens its life and
increases the required maintenance. In the present state of the art, if any
component causes a problem during starting; the gas turbine most probably has
to be stopped and restarted. With the CSTC , the gas turbine is isolated from the
compressor that allows, for example, the gas turbine to be started while the
compressor and the process is being readied. The gas turbine once started can
be idled until the compressor and process are ready to be started. If after normal
operation begins, problems occur for example with the compressor and/or the
process during starting, the gas turbine does not need to be stopped and instead
the CSTC simply has to be drained which isolates the gas turbine. The gas
turbine can be kept idling while the problem (s) in the compressor and/or process
are worked out.
34.Further, the apparatus and controllability method of the invention is simpler
than prior art start up devices and procedures, since the coupling of the
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
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A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
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A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
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A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
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A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
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A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
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A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
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A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
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A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf
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A BOOK ON BASIC CONCEPT OF MODERN POWER PLANTS by khalid ayaz soomro.pdf