发明名称 Combustion chamber for a ram-jet and ram-jet with such a combustion chamber
摘要 The combustion chamber (14) is delimited by an internal porous skin (17) and an external skin (18) forming an intermediate space between them. The fuel supplying the injectors (9) passes through the intermediate space. An exhaust pipe (16) channels the combustion gases (28) leaving the heart of the combustion chamber.
申请公布号 EP1342904(A1) 申请公布日期 2003.09.10
申请号 EP20030290448 申请日期 2003.02.26
申请人 EADS SPACE TRANSPORTATION SA;MBDA FRANCE 发明人 BOUCHEZ, MARC;FALEMPIN, FRANCOIS
分类号 F02K7/10;F02K9/64;(IPC1-7):F02K7/10 主分类号 F02K7/10
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