Hypersonic scramjet engine fuel injector

F - Mech Eng,Light,Heat,Weapons – 02 – K

Patent

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60/70

F02K 7/10 (2006.01) F02K 9/52 (2006.01) F23R 3/28 (2006.01)

Patent

CA 1329992

HYPERSONIC SCRAMJET ENGINE FUEL INJECTOR Abstract of the Disclosure 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.

601471

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