发明名称 Multistage ramjet engine for propulsion of high-speed aircraft
摘要 A motor-driven axial compressor (2) is mounted at the air inlet of a combustion chamber (4) and its power is sufficient to set the combustion chamber in operation. A short connecting pipe is fitted at the outlet of the combustion chamber, and by its other end the pipe is fitted to the inlet of an additional combustion chamber of the same size. The connecting pipe has air inlet openings which are designed and arranged so that external air is drawn in by passing combustion gases from the combustion chamber.
申请公布号 DE19815723(A1) 申请公布日期 1999.10.14
申请号 DE19981015723 申请日期 1998.04.08
申请人 ZEMANN, HERBERT 发明人 ZEMANN, HERBERT
分类号 F02K7/10;F02K7/12;F02K7/16;(IPC1-7):F02K7/16 主分类号 F02K7/10
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