发明名称 Micro pulse jet engine
摘要 A millimetre-scale pulse jet engine comprises an engine body that defines a combustion chamber, a fuel, an air intake, and an exhaust. The fuel inlet is arranged to inject fuel directly into the combustion chamber. The air intake and the exhaust are in fluid communication with the combustion chamber, and the combustion chamber is configured such that air from the air intake and fuel from the fuel inlet cyclically combust in the combustion chamber to produce exhaust gases.
申请公布号 AU2007253069(B2) 申请公布日期 2012.02.23
申请号 AU20070253069 申请日期 2007.05.09
申请人 BAE SYSTEMS PLC 发明人 HUCKER, MARTYN JOHN;HOLDEN, HARRIET ANN;WARSOP, CLYDE
分类号 F02K7/04 主分类号 F02K7/04
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