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Fuel injector for a ramjet working at high Mach number

机译:用于高马赫数冲压发动机的喷油器

摘要

A fuel injector for a ramjet engine on an aircraft designed to travel at high Mach numbers, e.g. Mach 12 - 15, made to deliver a flow of fuel to a combustion chamber, consists of a body (10) and a bow (7) made from a carbon/carbon composition material. The body has a leading edge (16) forming an angle of about 15 degrees, partially cut away to form a flat face (17). The bow (11) is made from a thin layer of carbon/carbon composition material and has a leading edge (11A) with a radius of curvature of up to 2 mm. The material has a woven fibrous structure and a matrix of pyrolysed tar and graphite. The bow (11) is fixed and sealed to the body of the injector so that it forms a sealed inner chamber with a system (23, 27) for injecting a coolant fluid through jets in the face (17). After impacting against the inner surface of the skin the coolant fluid is evacuated through an outlet system (28, 29, 30).
机译:设计用于以高马赫数行进的飞机上的冲压喷气发动机的喷油器用来将燃料流输送到燃烧室的马赫数12至15,由主体(10)和由碳/碳复合材料制成的船首(7)组成。主体具有形成约15度角的前缘(16),该前缘被部分切除以形成平坦表面(17)。弓形件(11)由碳/碳复合材料的薄层制成,并具有曲率半径最大为2mm的前缘(11A)。该材料具有机织纤维结构以及热解焦油和石墨的基质。弓形件(11)被固定并密封到喷射器的主体上,从而其与系统(23、27)形成密封的内腔,该系统用于通过面(17)中的射流喷射冷却剂流体。在撞击皮肤的内表面之后,冷却剂流体通过出口系统(28、29、30)排空。

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