Rotary air valve firing patterns for resonance detuning

Details Rotary air valve firing patterns for resonance detuning Rotary air valve firing patterns for resonance detuning

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 5/12 (2006.01) F02K 3/00 (2006.01) F02K 7/06 (2006.01)

Patent

CA 2696289

An engine (100) contains a compressor stage (101), a plurality of pulse detonation combustors (103) and a rotary inlet valve structure (105) having a plurality of inlet ports (104) through which at least air flows to enter the pulse detonation combustors during operation of the engine. Downstream of the pulse detonation combustors is a turbine stage (111). Further, the ratio of the pulse detonation combustors to the inlet ports is a non-integer.

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