发明名称 Transpiration cooled fuel injector bar for a ramjet engine
摘要 The panel (6) has a nose section (7) with a leading edge (8) which receives the incoming oxidant flow. The nose section is hollow, with side walls (12) and an inner chamber (11) containing an injection bar (16) with outlets to deliver cooling jets of fluid, e.g. fuel, to the perforated leading edge. To the rear of the leading edge the panel comprises a housing containing primary chambers in the form of perforated open-ended cylinders set one on top of another. The cylinders are connected at one end to the main fuel injector and at the other to the injection bar inside the leading edge.
申请公布号 EP0846920(A1) 申请公布日期 1998.06.10
申请号 EP19970402899 申请日期 1997.12.02
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 CHEVALIER, ALAIN;BOUCHEZ, MARC
分类号 F02K7/10;F23R3/20;F23R3/28 主分类号 F02K7/10
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