发明名称 |
HYPERSONIC SCRAMJET ENGINE FUEL INJECTOR |
摘要 |
HYPERSONIC SCRAMJET ENGINE FUEL INJECTOR A fuel injector for a hypersonic scramjet engine is described. The fuel injector has a horizontal top wall with a fuel injection orifice, an inclined bottom wall, a vertical end wall with a plurality of spaced apart convergent-divergent fuel outlet nozzles and vertical side walls, whereby the injector housing defines a substantially right angled cross-section. A plurality of fuel injectors are connected to the top portion of the combustor of an scramjet engine and are particularly designed to provide sufficient cooling protection against the hypersonic-speed impingement of the compressed inlet air.
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申请公布号 |
CA1329992(C) |
申请公布日期 |
1994.06.07 |
申请号 |
CA19890601471 |
申请日期 |
1989.06.01 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
LEE, CHING-PANG;VENKATARAMANI, KATTALAICHERI S.;LAHTI, DANIEL J.;LEE, VINCENT H. |
分类号 |
F02K7/14;F02K7/10;F02K9/52;F23R3/28;(IPC1-7):F02K7/10 |
主分类号 |
F02K7/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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