The document evaluates applying an Electric-Turbo-Compound system to recover waste heat from marine diesel engines. Modeling shows a system with an expansion ratio of 1.5 and engine design point of 85% could generate 490kWe per engine on a frigate, saving 43 tons of fuel annually and reducing payback time to 4.2 years with projected 2021 costs. Overall, the analysis found waste heat recovery via Electric-Turbo-Compound can provide cost-effective emissions reductions on certain vessel types.
Evaluation of Electric-Turbo-Compounding Technology applied to Marine Diesel-Engines for Waste Heat Recovery
1. Evaluation of Electric-Turbo-Compound applied to Marine
Diesel-Engines for Waste Heat Recovery
October 4th, 2018
Prof Richard Bucknall (UCL)
Presenter: Dr Santiago Suárez de la Fuente (UCL)
Dr Shinri Szymko (Bowman Power Group Ltd.)
Will Bowers (Bowman Power Group Ltd.)
Alastair Sim (Rolls-Royce)
Presenter: Keith Douglas (Bowman Power Group Ltd.)
3. Introduction
Innovate UK project [101987]: Vessel efficiency at sea, Marine ETC
Lead Partner: Bowman Power Group Ltd
Partners: Lloyd’s Register, Rolls-Royce and UCL
Length: 30 months (between 2015 and 2018)
Objectives:
• To develop a new, marine-capable ETC system for 4-stroke diesel engines
(< 4 MW);
• To develop a market study for the new ETC system;
• To model the ETC system performance on different ships, layouts and
operational profiles; and
• To open new development roads for the marine ETC.
4. Objectives
• Model and test different ETC designs for the Frigate’s diesel
engines and quantify:
• ETC electric power output
• Fuel savings
• CO2 emission reductions
• Secondary impacts Cylinder backpressure
• Initial cost
• Payback time
What are the benefits and secondary impacts when
installing an ETC system on-board a Frigate?
5. • Exhaust gas, with high temperature and pressure flows
from the engine and enters the ETC 1000
• The stationary Nozzle Guide Vanes (NGV) direct and
accelerate the flow toward the rotating rotor blades
downstream
• The flow from the NGV transfers the exhaust energy (high
temperature and high pressure) to the turbine blades and
rotor
• The gases exit the ETC 1000 at close to the exhaust stack
• The rotor is connected to the high speed alternator
producing a non-stable AC current, which is exported to the
Power Electronics unit
• This AC input current is converted to DC before final
conversion to 3 phase AC grid quality (50/60Hz) output
(Can also be used to power site auxiliaries or charge
batteries for hybrid solutions)
KEY COMPONENTS
Turbo
Generator
Power
Electronics
1
2
3
4
5
1
2
3
4
5
6
6
6. EXAMPLE ETC SYSTEM SET UP
1: TURBO GENERATOR
Located downstream of the
engine’s turbocharger to recover
further energy. Produces
electricity typically > 1000 Hz
3: POWER ELECTRONICS
The high frequency electricity is
converted to grid quality
electricity at 50/60 Hz
Also available in single system
set up
2: TURBOCHARGER
To maintain engine performance
this is re-matched to work with
the turbo generator
2
1
3
7. ELECTRIC TURBO-COMPOUNDING (ETC)
ETC is currently applied: 1 - In-line with the engine’s turbocharger as shown:
1. ETC power is increased by decreasing the TG NGV, thus increasing back pressure on
the TC, slowing it and dragging down the air fuel ratio (AFR)
Increased combustion & exhaust temperatures and pumping losses
2. This is offset by decreasing the TC NGV, increasing TC speed and AFR
Further increased pumping losses, residual fraction & firing pressures
1
2
TG & TC NGV’s optimised together to maximise ETC power within engine limits
8. EFFECT ON ENGINE PERFORMANCE
0
100
200
300
400
500
600
700
Temperature
(°C)
Engine Baseline
System Optimisation
50
150
250
350
450
Pressure(kPa)
1. Increased dP across engine leads to pumping
losses. At constant fuel consumption this results in
a decrease in engine power
2. Increased engine out pressure results in increased
expansion ratio for turbocharging system and more
power extracted from exhaust gases
Increased system power
Typical pressures and temperatures for
ETC application
2
1
2
1
1
2
9. ELECTRIC TURBO-COMPOUNDING (ETC)
ETC is currently applied: 1 - In-line with the engine’s turbocharger as shown:
Engine size
Fuel
Type
Typical fuel saving and /
or Power uplift
Typical ROI payback (months)
0.5 – 2.5MWe
Natural Gas 3 – 5%
18 - 30Bio Gas / Low BTU 5 – 7%
Diesel 4 – 7%
10. WASTEGATE VARIANT
Engine size
Fuel
Type
Typical fuel saving and /
or Power uplift
Typical ROI payback (months)
10 - 20MWe Natural Gas 1 – 3 % 24 - 36
ETC is currently applied: 2 - Parallel to the engine’s turbocharger as shown:
11. OTHER ADVANTAGES
Downsizing the engine’s turbo brings through increased AFR at idle, low speeds and loads:
• Better transient response and acceleration
• Lower transient emissions (NOx and PM)
• Reduced Methane slip / UHC emissions (SI gas engines)
12. Case Study - Frigate
• Propulsion layout = CODLOG
• Engines = 4 x MTU4000 (20 cylinder each) 16 MW
• Electrical Generator Efficiency = 91%
• Gas Turbine = 1 36 MW (Out of the scope of this work)
• Hotel Demand = 1.9 MWe (Assumed constant)
• Fuel (Diesel engines) = F76 (42,700 kJ/kg)
[CF = 3.206 t CO2/t of fuel ]
[Cost = £392.9/t – average between April 2017 and April 2018]
[1]
13. Case Study - Frigate
Power Curve Assumed a cubic relationship
14. • Propulsion layout = CODLOG
• Engines = 4 x MTU4000 (20 cylinder each) 16 MW
• Gas Turbine = 1 36 MW (Out of the scope of this work)
• Hotel Demand = 1.9 Mwe (Assumed constant)
• Fuel (Diesel engines) = F76 (42,700 kJ/kg)
• Maximum Speed Diesel only (kn) = 20.0
• Maximum Speed (kn) = 30.0
• Operational time (days) = 215 (59% of a year)
Case Study - Frigate
[1]
17. Approach
A sensitivity analysis was performed:
• ETC Design Expansion Ratios
(ER):
• 1.1 – 1.7 in steps of 0.2
• 4-stroke diesel engine Design
Point (DP):
• 75% & 85% MCRe
• Operational Point (OP):
• 57% to 95% MCRe 9 points
• One year operation
[2]
18. Results
ETC Electric Power Output (per engine)
18
Larger design ER produce more electrical
power.
• 680 KWe (ER 1.7) vs 220 kWe (ER 1.1)
Higher DP loads produce less electrical power
for the same loading condition and ER.
• ER 1.7: 680 kWe vs 600 kWe
• Better efficiencies and higher ER when
the DP is set at 75% MCRe
Low design ER do not produce electrical
power when:
• DP is @ 75% MCRe and OP < 65% MCRe
• DP is @ 85% MCRe and OP < 70% MCRe.
19. Results
Pressure before the TC turbine
Low DP and ER reduce the
backpressure at low loads
• Better TC efficiency
High ER for any DP can reach a change
above 40% at any loading condition
(Max. 68% change)
• This will be an important issue with respect
to NOx formation Engine recertification
may be needed
• Exhaust gas leaking to intake manifold
combustion temperature increase
20. Results
Mechanical Power Reduction per Cylinder
20
Drop in mechanical power:
• Increase in cylinder backpressure
Pumping losses rise
• Lower electrical demand due to ETC
operation
Larger change happens with larger ER &
lower loading at DP and larger OP
Larger ETC Power = Larger Mechanical
Power Reduction
21. Results
Annual Overall Fuel Savings
Frigate annual fuel consumption 680 t (633 t from the 4-stroke & 47 t gas
turbine)
CO2 emissions 2,180 t (2,030 t from the 4-stroke & 150 t gas turbine)
• 60 t of fuel reduced (More than what the GT consumes)
• And 190 t of CO2
• And £23,500
• But there is an important increment in backpressure
ETC Expansion Ratio
(-)
Engine Design Point
(% MCRe)
1.1 1.3 1.5 1.7
75 2.1% 5.2% 7.3% 8.8%
85 1.0% 4.2% 6.4% 7.9%
22. Results
Initial and Running Costs (Best estimated)
• ETC (110 kWe kit)
• Specific cost = £700/kWe (Today) Target 2021 = £350/kWe
• Running cost = £0.30/h
• Lowest overall cost = £0.39 million (DP 85% MCRe & ER 1.1)
• 2 - 110 kWe ETC per engine
• Highest overall cost = £1.55 million (DP 75% MCRe & ER 1.7)
• 7 - 110 kWe ETC per engine
£0.19 million
£0.78 million
2021
23. Results
Carbon Emission Reduction Costs
•Assuming an operative life of 25 years, reducing CO2
emissions could cost:
• DP 85% MCRe & ER 1.1 (Lowest total cost) = £620/t CO2
• DP 85% MCRe & ER 1.5 (Mid total cost) = £190/t CO2
• DP 75% MCRe & ER 1.7 (Highest total cost) = £200/t CO2
[3]
£95/t CO2
£100/t CO2
2021
£310/t CO2
24. Results
Payback Time
Shortest payback time is 8.4 years DP 85% MCRe with ER 1.5
• Lower initial cost
• Frigate navigates only 59% of the year and the 4-stroke diesel + ETC just 31%
25. Results
Payback Time (Other ships)
Ship Type DWT
ETC
Location
Number of ETC
per Engine (-)
Ship Fuel
Savings (%)
Payback Time
(Years)
Coastal Cargo 6,500 ME 1 3.2 3.9
Dry Bulk 96,140 AE 2 7.4 5.2
PSV (Small) 1,315 AE 2 7.3 5.2
PSV (Medium) 4,470 AE 3 5.2 7.5
Passenger (Small) 527 ME 2 3.0 9.0
Passenger (Medium) 5,770 AE 4 5.6 7.1
Tanker 363,280 AE 2 1.2 2.3
Optimum payback time depends on:
• Ship utilisation
• How the ship is being operated (ETC utilisation)
• Complexity
26. Results
Payback Time (Other ships)
Ship Type DWT
ETC
Location
Number of ETC
per Engine (-)
Ship Fuel
Savings (%)
Payback Time
– 2021 Costs
(Years)
Coastal Cargo 6,500 ME 1 3.2 1.8
Dry Bulk 96,140 AE 2 7.4 2.6
PSV (Small) 1,315 AE 2 7.3 2.6
PSV (Medium) 4,470 AE 3 5.2 3.8
Passenger (Small) 527 ME 2 3.0 4.5
Passenger (Medium) 5,770 AE 4 5.6 3.6
Tanker 363,280 AE 2 1.2 1.2
Optimum payback time depends on:
• Ship utilisation
• How the ship is being operated (ETC utilisation)
• Complexity
27. Conclusions
Performed ETC sensitivity analysis and found that the
frigate will benefit from an ETC with a:
Design point at 85% MCRe with a design ER of 1.5
• Initial cost of £1.1 million 5-110 kWe ETC per engine
• Max. electrical power output per engine (kWe) = 490
• Max. cylinder backpressure change (kPa) = 116 (40%)
• Annual fuel savings (t) = 43 (140 t CO2)
• Cost CO2 reduction (£/t CO2) = 195
• Payback time (years) = 8.4
• Payback time (years, specific costs 2021) = 4.2 years