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

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…

TTEC Gas Turbine 5 kW to 100 MW

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

 

TTEC Plasma Shock Wave Combustor eliminatesThe 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.

Compressor Module CFD AnalysisDuring our First Generation Testing

AeroValve Pulse Combustors3 ea Red section

Turbine Module

Compressor ModulePer TTEC ConventionalTurbine Design

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 aspeed reducing gearbox.

 4.

Use of oil-free foil bearings reduces maintenance costs, and provides improvereliability.

 5.

Simpler design construction reduces capital costs by 40% vs. conventional turbinetechnology.

 

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…