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DESIGN AND TESTING OF DISC
TYPE HYBRID TURBINE-PUMP
Guided by,
Er. Jiju John
Assistant Professor
ME Department
Submitted by,
Denny John
Roll No: 19
S7
CONTENTS
INTRODUCTION
PROBLEM DESCRIPTION
LITERATURE REVIEW
WORKING PRINCIPLE
DESIGN
EXPERIMENTAL TESTING AND RESULTS
ADVANTAGES AND DISADVANTAGES
CONCLUSION
REFERENCE
INTRODUCTION
• Nikola Tesla invented the bladeless turbine in 1913.
• Instead of using fan type blades he used solid disc metal.
• Here we uses properties of fluids like viscosity, adhesion, cohesion,
instead of conventional energy transfer mechanisms.
• In this presentation, Integration of two types of viscous drag hydraulic
machines- tesla turbine & tesla pump are made.
• Fluid transportation and power development is the advantage of these
type of power unit.
LITERATURE REVIEW
• Nikola tesla invented bladeless turbine in 1909 and patented in1913.
• In 1948, tesla turbine pump started its initial production.
• In 1993 John pacello & Peter hanas studied the hard to pump
applications of tesla pump.
• In 2013, Dr. Amalraju published a research paper regarding hybrid
tesla turbine pump
PROBLEM DESCRIPTION
• Tesla pumps have a great application in lifting highly viscous fluids.
• Ordinary pumps have the following disadvantages
o Difficulty in pumping highly viscous fluids.
o Difficulty in pumping highly abrasive slurries with high
amount of solid particles.
• Disadvantages of ordinary tesla pump are
oHigh inlet pressure required at inlet.
oLow torque.
oLow efficiency.
WORKING PRINCIPLE
• Both turbine and pump operates mainly on the principles of boundary
layer effect and viscous drag.
• Fluid layer closer to the inner disc surface in the inner disc spacing are
almost stationary from external point of view but they are at highest
velocity.
• Energy is transferred to adjacent layers.
• By viscous drag principle middle layer has maximum velocity.
• Operation of turbine depends upon impinging velocity
• A portion of the fluid pumped by the pump is bypassed to the turbine inlet
which rotates the turbine and turbine outlet is connected to the pump.
Fig 1: Fluid path in a Tesla pump
Fig 2:Fluid path in a Tesla turbine
DESIGN OF TURBINE PUMP
 Uses same type of packing(metal, plastics, ceramics) and
sealing(carbon, ceramic, silicon carbide) arrangements as a
centrifugal pump.
 Disc assembly and pumping mechanisms can be varied by
 Number of discs.
 Diameter of disc (8,10,12,14,17,20 inches are
standard).
 Spacing of the disc (determined by solids to be
passed and nature of fluids).
 Discs are of smooth or ribbed.
 Spacers are used in between discs.
Contd…
 Disc are arranged in tandem and are fitted to a circular flange which is
coupled with a shaft.
Fig 3: Forms of discs
TESTING BY SIMULATION
 Flow simulation by cosmos flow is presented.
 A prototype is created for this purpose.
 Pump is simulated for head range of 2 to 10m with 1m
interval.
 Simulation Configuration-
 No of discs: 10.
 Inlet pressure: Environmental pressure.
 Outlet pressure: 20000 to 100000 Pa.
 RPM: 1440
 It doesn’t account losses.
Fig 4: Simulation model
• Head vs Discharge: for each head, discharge is
obtained. Results are plotted to know the pump
performance.
TABLE: Head Vs Discharge
• Velocity :
 Flow produce a vortex in the outlet
 Pressure produced by boundary layer effect is
effectively collected to produce more head.
 Volute casing is used for this.
• Pressure :
 centrifugal force by the disc to the fluid pro-
duce high pressure inside casing.
 It is effectively transferred to make a higher
head of delivery by pump.
Fig 5: Velocity plot
Fig 6: Pressure plot
• Turbine output:
TABLE 2: discharge vs RPM
EXPERIMENTAL TESTING AND RESULTS
• Pump testing
 Pump is tested to variable head from 1 to 10m.
 1m suction lift is used.
 Discharge head= total head-suction head.
 Pipe friction losses are 1m/10m for selected pipe system.
TABLE 3: Experimental(Q Vs H) value
• Turbine testing:
 A control valve is used to get the desired flow rates.
 Theoretically required angular velocity is obtained by
 V=ω * R
Where V= velocity in m/s
ω= angular velocity in rad/s
R= radius in m
 ω= (2ΠN)/60
 By controlling mass flow, velocity at outlet is varied and desired
angular velocity is achieved.
TABLE 4: Q Vs RPM
RESULTS COMPARISON
• Discharge decline is in a linear manner.
• Difference in the graphs indicates the losses due to pumping, friction,
sealing.
• To collect maximum pressure volute casing is recommended.
• To produce best power outputs effective nozzle configurations should
be implemented.
TABLE 5: Comparison Table
ADVANTAGES
 Use of different kind of exotics fluids, with particles, droplets,
multiphase is possible.
More stable flow and lower cavitation occurrence.
It can turn at much higher speeds with total safety.
Tesla disk is the double clockwise and anticlockwise direction of
rotation in a single machine.
It can be used for lifting highly viscous fluids , viscosities upto several
10000 cP.
Little wear from abrasion during pumping, slurries containing upto
80% solids by volume can be pumped without clogging the system.
 Tesla was able to demonstrate a
fuel efficiency of 60% with his
bladeless turbine design. Most of
engines today do not get above 27
– 28% energy efficiency in their
conversion of fuel to work.
 Rotor has high efficiency as
shown in the figure
Fig 7: Efficiency comparison
Fig 8: Rotor efficiency
DISADVANTAGES
High speed but low torque.
Experimentally has been found many difficulties to achieve high
efficiencies in nozzles and rotors.
Proof of its efficiency compared to conventional turbines is still
questionable and needs more research.
APPLICATION
 Geothermal applications
 Chemical, oil & petrochemical processing.
 Pulp & paper manufacturing.
 Waste water treatment &disposal applications.
 Food & sanitary applications.
 Mining & environmental cleanup.
CONCLUSION
• Comparative study of experimental and simulation results shows that
disc pump is more suitable for high viscous liquids.
• It requires effective nozzle design to produce more efficient output.
• This integration of two hydraulic fluids forms a base of new
application and can be considered for further research.
REFERENCE
• “Rebirth of the Tesla Turbine”, Published in “Extra Ordinary
Technology” magazine – July 2003.
• Danny Blanchard, Phil Ligrani, Bruce Gale. “Single-disc and double-
disc viscous, Micro pumps”.
• Petr Bloudicek, David Palousek. “Design of tesla turbine”.
Konference diplomovych praci 2007
• Warren Rice, “Tesla Turbomachinery”, Proc. IV International Nikola
Tesla Symposium (Sep. 23 – 25 1991).
• H. S. Couto1, J.B.F. Duarte2 and D. Bastos-Netto, “The Tesla Turbine
Revisited”, 8thAsia-Pacific International Symposium on Combustion
and Energy Utilization October 10-12, 2006, Sochi, Russian
Federation.
THANK YOU

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Design and testing of disc type hybrid turbine pump

  • 1. DESIGN AND TESTING OF DISC TYPE HYBRID TURBINE-PUMP Guided by, Er. Jiju John Assistant Professor ME Department Submitted by, Denny John Roll No: 19 S7
  • 2. CONTENTS INTRODUCTION PROBLEM DESCRIPTION LITERATURE REVIEW WORKING PRINCIPLE DESIGN EXPERIMENTAL TESTING AND RESULTS ADVANTAGES AND DISADVANTAGES CONCLUSION REFERENCE
  • 3. INTRODUCTION • Nikola Tesla invented the bladeless turbine in 1913. • Instead of using fan type blades he used solid disc metal. • Here we uses properties of fluids like viscosity, adhesion, cohesion, instead of conventional energy transfer mechanisms. • In this presentation, Integration of two types of viscous drag hydraulic machines- tesla turbine & tesla pump are made. • Fluid transportation and power development is the advantage of these type of power unit.
  • 4. LITERATURE REVIEW • Nikola tesla invented bladeless turbine in 1909 and patented in1913. • In 1948, tesla turbine pump started its initial production. • In 1993 John pacello & Peter hanas studied the hard to pump applications of tesla pump. • In 2013, Dr. Amalraju published a research paper regarding hybrid tesla turbine pump
  • 5. PROBLEM DESCRIPTION • Tesla pumps have a great application in lifting highly viscous fluids. • Ordinary pumps have the following disadvantages o Difficulty in pumping highly viscous fluids. o Difficulty in pumping highly abrasive slurries with high amount of solid particles. • Disadvantages of ordinary tesla pump are oHigh inlet pressure required at inlet. oLow torque. oLow efficiency.
  • 6. WORKING PRINCIPLE • Both turbine and pump operates mainly on the principles of boundary layer effect and viscous drag. • Fluid layer closer to the inner disc surface in the inner disc spacing are almost stationary from external point of view but they are at highest velocity. • Energy is transferred to adjacent layers. • By viscous drag principle middle layer has maximum velocity. • Operation of turbine depends upon impinging velocity • A portion of the fluid pumped by the pump is bypassed to the turbine inlet which rotates the turbine and turbine outlet is connected to the pump.
  • 7. Fig 1: Fluid path in a Tesla pump
  • 8. Fig 2:Fluid path in a Tesla turbine
  • 9. DESIGN OF TURBINE PUMP  Uses same type of packing(metal, plastics, ceramics) and sealing(carbon, ceramic, silicon carbide) arrangements as a centrifugal pump.  Disc assembly and pumping mechanisms can be varied by  Number of discs.  Diameter of disc (8,10,12,14,17,20 inches are standard).  Spacing of the disc (determined by solids to be passed and nature of fluids).  Discs are of smooth or ribbed.  Spacers are used in between discs.
  • 10. Contd…  Disc are arranged in tandem and are fitted to a circular flange which is coupled with a shaft. Fig 3: Forms of discs
  • 11. TESTING BY SIMULATION  Flow simulation by cosmos flow is presented.  A prototype is created for this purpose.  Pump is simulated for head range of 2 to 10m with 1m interval.  Simulation Configuration-  No of discs: 10.  Inlet pressure: Environmental pressure.  Outlet pressure: 20000 to 100000 Pa.  RPM: 1440  It doesn’t account losses. Fig 4: Simulation model
  • 12. • Head vs Discharge: for each head, discharge is obtained. Results are plotted to know the pump performance. TABLE: Head Vs Discharge
  • 13. • Velocity :  Flow produce a vortex in the outlet  Pressure produced by boundary layer effect is effectively collected to produce more head.  Volute casing is used for this. • Pressure :  centrifugal force by the disc to the fluid pro- duce high pressure inside casing.  It is effectively transferred to make a higher head of delivery by pump. Fig 5: Velocity plot Fig 6: Pressure plot
  • 14. • Turbine output: TABLE 2: discharge vs RPM
  • 15. EXPERIMENTAL TESTING AND RESULTS • Pump testing  Pump is tested to variable head from 1 to 10m.  1m suction lift is used.  Discharge head= total head-suction head.  Pipe friction losses are 1m/10m for selected pipe system.
  • 16. TABLE 3: Experimental(Q Vs H) value
  • 17. • Turbine testing:  A control valve is used to get the desired flow rates.  Theoretically required angular velocity is obtained by  V=ω * R Where V= velocity in m/s ω= angular velocity in rad/s R= radius in m  ω= (2ΠN)/60  By controlling mass flow, velocity at outlet is varied and desired angular velocity is achieved.
  • 18. TABLE 4: Q Vs RPM
  • 19. RESULTS COMPARISON • Discharge decline is in a linear manner. • Difference in the graphs indicates the losses due to pumping, friction, sealing. • To collect maximum pressure volute casing is recommended. • To produce best power outputs effective nozzle configurations should be implemented.
  • 21. ADVANTAGES  Use of different kind of exotics fluids, with particles, droplets, multiphase is possible. More stable flow and lower cavitation occurrence. It can turn at much higher speeds with total safety. Tesla disk is the double clockwise and anticlockwise direction of rotation in a single machine. It can be used for lifting highly viscous fluids , viscosities upto several 10000 cP. Little wear from abrasion during pumping, slurries containing upto 80% solids by volume can be pumped without clogging the system.
  • 22.  Tesla was able to demonstrate a fuel efficiency of 60% with his bladeless turbine design. Most of engines today do not get above 27 – 28% energy efficiency in their conversion of fuel to work.  Rotor has high efficiency as shown in the figure Fig 7: Efficiency comparison Fig 8: Rotor efficiency
  • 23. DISADVANTAGES High speed but low torque. Experimentally has been found many difficulties to achieve high efficiencies in nozzles and rotors. Proof of its efficiency compared to conventional turbines is still questionable and needs more research.
  • 24. APPLICATION  Geothermal applications  Chemical, oil & petrochemical processing.  Pulp & paper manufacturing.  Waste water treatment &disposal applications.  Food & sanitary applications.  Mining & environmental cleanup.
  • 25. CONCLUSION • Comparative study of experimental and simulation results shows that disc pump is more suitable for high viscous liquids. • It requires effective nozzle design to produce more efficient output. • This integration of two hydraulic fluids forms a base of new application and can be considered for further research.
  • 26. REFERENCE • “Rebirth of the Tesla Turbine”, Published in “Extra Ordinary Technology” magazine – July 2003. • Danny Blanchard, Phil Ligrani, Bruce Gale. “Single-disc and double- disc viscous, Micro pumps”. • Petr Bloudicek, David Palousek. “Design of tesla turbine”. Konference diplomovych praci 2007 • Warren Rice, “Tesla Turbomachinery”, Proc. IV International Nikola Tesla Symposium (Sep. 23 – 25 1991). • H. S. Couto1, J.B.F. Duarte2 and D. Bastos-Netto, “The Tesla Turbine Revisited”, 8thAsia-Pacific International Symposium on Combustion and Energy Utilization October 10-12, 2006, Sochi, Russian Federation.