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TTEC Concept 5kW to 100 MW Plasma Pulse Shock Wave Gas Turbine Generator
TTEC Gas Turbine 5 kW to 100 MW




TTEC exclusive Plasma Pulse Shock Wave Gas Turbine Generator @ 60% Thermal
efficiency without waste heat recuperation… TTEC Exclusive Aerovalve oxygen intake
requires No Compressor Section

 Our combustion Cycle is self aspirating…and self-sustaining detonation combustion
2000 deg. F @ over 400 cycles per second per combustion chamber…this is the jet
engine way of the future…
Because of self-sustaining detonation combustion, our turbine can produce near peak
  torque at low rpms. Conventional turbines produce very little torque at low rpm's.
TTEC Plasma Shock Wave Combustor eliminates
                                               The need for Turbine compressor!
                                                     Saving 40% Energy
 TTEC Gas Turbine requires no Gearbox,
     we direct connect to our unique
High Speed Permanent Magnet Generators
GE 15 MW Gas Turbine Generator is 10 times the size of our TTEC Plasma Pulse Shock
Wave Gas Turbine because we are twice as efficient and have no makup combustion
air compressor section, the compressor on conventional Gas Turbines, consume 40%
of the energy input…TTEC replaces the compressor with our Plasma Shock Wave
Compression Ratio @ 150:1 many times more efficient in energy saving and equipment
size.
AeroValve Pulse Combustors
3 ea Red section




                                            Compressor Module CFD Analysis
                    Compressor Module       During our First Generation Testing
                    Per TTEC Conventional
                    Turbine Design


                                Turbine Module
1.
Because of self-sustaining detonation combustion, our turbine can produce near peak
  torque at low rpms. Conventional turbines produce very little torque at low rpm's.

                                         2.
 Boundary Layer turbo physics provides more gas expansion work than conventional
                                   turbine cycles
                       leading to greater thermal efficiency.

                                         3.
Turbine can be direct coupled to high-speed generator which eliminates the need for a
                              speed reducing gearbox.

                                             4.
    Use of oil-free foil bearings reduces maintenance costs, and provides improve
                                        reliability.

                                        5.
  Simpler design construction reduces capital costs by 40% vs. conventional turbine
                                    technology.
6.
  Quiet operation as turbo engine uses a "bladeless" turbine section and no
                                compressor.
  Boundary Layer turbine generates no blade frequency noise generation.

                                  7.
   Shock wave detonation enhanced compression occurs directly inside of
                              combustion
          chamber not generated by external mechanical means.

                                      8.
Modular "Power Section" construction makes for a compact, and power dense
                                  turbo-gen.
               that is easy to scale for a given power output.

                                  9.
Plasma enhanced detonation combustion provides for low exhaust emissions
                            (CO, NOx, HC).

                                     10.
Boundary layer turbine provides greater compression ratio than conventional
                               turbines which
                        increases thermal efficiency.
The World as well as our view of the Universe continues to amaze how naturally, atoms,
molecules as well as fluids and gases all reveal the boundary layer effects on one to another
in pure spiral paths of influence…

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TTECH Gas Micro-Turbine

  • 1. TTEC Concept 5kW to 100 MW Plasma Pulse Shock Wave Gas Turbine Generator
  • 2. TTEC Gas Turbine 5 kW to 100 MW TTEC exclusive Plasma Pulse Shock Wave Gas Turbine Generator @ 60% Thermal efficiency without waste heat recuperation… TTEC Exclusive Aerovalve oxygen intake requires No Compressor Section Our combustion Cycle is self aspirating…and self-sustaining detonation combustion 2000 deg. F @ over 400 cycles per second per combustion chamber…this is the jet engine way of the future…
  • 3. Because of self-sustaining detonation combustion, our turbine can produce near peak torque at low rpms. Conventional turbines produce very little torque at low rpm's.
  • 4. TTEC Plasma Shock Wave Combustor eliminates The need for Turbine compressor! Saving 40% Energy TTEC Gas Turbine requires no Gearbox, we direct connect to our unique High Speed Permanent Magnet Generators
  • 5. GE 15 MW Gas Turbine Generator is 10 times the size of our TTEC Plasma Pulse Shock Wave Gas Turbine because we are twice as efficient and have no makup combustion air compressor section, the compressor on conventional Gas Turbines, consume 40% of the energy input…TTEC replaces the compressor with our Plasma Shock Wave Compression Ratio @ 150:1 many times more efficient in energy saving and equipment size.
  • 6.
  • 7. AeroValve Pulse Combustors 3 ea Red section Compressor Module CFD Analysis Compressor Module During our First Generation Testing Per TTEC Conventional Turbine Design Turbine Module
  • 8. 1. Because of self-sustaining detonation combustion, our turbine can produce near peak torque at low rpms. Conventional turbines produce very little torque at low rpm's. 2. Boundary Layer turbo physics provides more gas expansion work than conventional turbine cycles leading to greater thermal efficiency. 3. Turbine can be direct coupled to high-speed generator which eliminates the need for a speed reducing gearbox. 4. Use of oil-free foil bearings reduces maintenance costs, and provides improve reliability. 5. Simpler design construction reduces capital costs by 40% vs. conventional turbine technology.
  • 9. 6. Quiet operation as turbo engine uses a "bladeless" turbine section and no compressor. Boundary Layer turbine generates no blade frequency noise generation. 7. Shock wave detonation enhanced compression occurs directly inside of combustion chamber not generated by external mechanical means. 8. Modular "Power Section" construction makes for a compact, and power dense turbo-gen. that is easy to scale for a given power output. 9. Plasma enhanced detonation combustion provides for low exhaust emissions (CO, NOx, HC). 10. Boundary layer turbine provides greater compression ratio than conventional turbines which increases thermal efficiency.
  • 10.
  • 11.
  • 12.
  • 13.
  • 14.
  • 15.
  • 16.
  • 17. The World as well as our view of the Universe continues to amaze how naturally, atoms, molecules as well as fluids and gases all reveal the boundary layer effects on one to another in pure spiral paths of influence…