Tangential combustion turbine

Details Tangential combustion turbine Tangential combustion turbine

2009-07-07

2011-11-22

Denion, Thomas (Department: 3748)

Internal-combustion engines

Rotary

With compression, combustion, and expansion in a single...

C123S241000

Reexamination Certificate

active

08061327

ABSTRACT:
A tangential combustion turbine is disclosed which is based on a casing, a rotor, and moving levers. A radial compressor is attached to the rotor and creates air pressure which pushes air into the combustion chamber based on the position and design of the combustion lever. The combustion chamber is defined by spaces between rotor lobes, and by combustion levers and exhaust levers which follow the rotor surface. A premix fuel system or direct fuel injection is used to create combustion. The exhaust gases then pass through the exhaust lever into the exhaust piping as the rotor rotates.

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