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GROUND-BASED SIMPLE CYCLE PULSE DETONATION COMBUSTOR-BASED HYBRID ENGINE FOR POWER GENERATION

机译:基于地面的简单循环脉冲爆震基于燃烧器的混合动力发电机

摘要

PROBLEM TO BE SOLVED: To improve a method of mounting a PDC in a turbine based engine and a power generation device.;SOLUTION: This engine 100 includes a compressor stage 101, a compressor plenum 103, an inlet valve stage 105, a PDC stage 107, a PDC exit nozzle stage 109, a transition stage 111, a high pressure turbine stage 113, a turbine plenum 115, and a low pressure turbine stage 117. The PDC stage 107 includes at least one pulse detonation combustor 123 and each of the compressor plenum 103, the PDC exit nozzle stage 109, and the turbine plenum 115 includes a volume 110 used to reduce and/or widen pressure peaks generated by the operation of the PDC stage 107.;COPYRIGHT: (C)2010,JPO&INPIT
机译:解决的问题:改进在涡轮发动机和发电装置中安装PDC的方法。解决方案:该发动机100包括压缩机级101,压缩机增压室103,进气门级105,PDC级107,PDC出口喷嘴级109,过渡级111,高压涡轮级113,涡轮增压室115和低压涡轮级117。PDC级107包括至少一个脉冲爆震燃烧器123,每个压缩机气室103,PDC出口喷嘴级109和涡轮机气室115包括一个容积110,该容积用于减少和/或加宽由PDC阶段107的操作产生的压力峰值。版权所有:(C)2010,JPO&INPIT

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