发明名称 COMBINED CYCLE PULSE DETONATION TURBINE ENGINE
摘要 PROBLEM TO BE SOLVED: To provide a pulse detonation device for turbo fan engine. SOLUTION: A turbo engine comprises a pulse detonation device for generating a temperature rise and a pressure rise inside of the engine and for generating the thrust from the engine. This device includes a pulse detonation augmenter including a shock wave tube device. The shock wave tube device includes plural shock wave tubes for mixing the air and the fuel to be led into the pulse detonation augmenter and for exploding the air-fuel mixture. The detonation generates the high temperature combustion gas, and this high temperature gas is led from the engine so as to generate the thrust of the engine. This device includes a pulse detonation augmenter device to be substituted for a core engine of the turbo fan engine.
申请公布号 JP2001355515(A) 申请公布日期 2001.12.26
申请号 JP20010097814 申请日期 2001.03.30
申请人 GENERAL ELECTRIC CO <GE> 发明人 JOHNSON JAMES EDWARD;DUNBAR LAWRENCE WAYNE;BUTLER LAWRENCE
分类号 F02C7/18;F02K3/075;F02K3/08;F02K7/02;F02K7/06;F02K7/16;F02K7/20;F02K9/78;(IPC1-7):F02K7/02 主分类号 F02C7/18
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