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US08341932B2 Rotary air valve firing patterns for resonance detuning 有权
用于共振失谐的旋转空气阀发射模式

Rotary air valve firing patterns for resonance detuning
摘要:
An engine contains a compressor stage, a plurality of pulse detonation combustors and a rotary inlet valve structure having a plurality of inlet ports 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. Further, the ratio of the pulse detonation combustors to the inlet ports is a non-integer.
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