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Fuel injector for a ramjet working at high Mach number
Fuel injector for a ramjet working at high Mach number
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机译:用于高马赫数冲压发动机的喷油器
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摘要
The fuel injector for delivering fuel to a combustion chamber in a ramjet engine on an aircraft designed to operate at a high Mach level (e. g. Mach 2 - 15) has a bow which receives the fuel flow and a row of injection orifices. The bow is formed, at least adjacent to its leading edge (11A), from a thin panel (11) of a thermally conducting material, e.g. stainless steel or copper, folded at an angle of about 15 degrees and having a leading edge radius of up to 2 mm. Inside the panel (11) the injector has a sealed chamber containing injectors (27) for a coolant fluid under pressure, and a system (28, 29, 30) for removing the coolant fluid after it has impacted against the concave face of the panel. The conductivity of the panel is of the order of 70 W/m/K, and the coolant fluid is a low-temperature gas or fuel.
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机译:在设计成以高马赫数(例如2-15马赫)运行的飞机上,用于将燃料输送到冲压发动机中的燃烧室的燃料喷射器具有接收燃料流的弓形件和一行喷射孔。弓至少由其前缘(11A)形成,由导热材料例如薄板制成的薄板(11)形成。不锈钢或铜,以约15度角折叠,且前缘半径最大为2 mm。喷射器在板(11)内部具有密封腔,该密封腔包含用于在压力下冷却剂流体的喷射器(27),以及用于在冷却剂冲击到板的凹面之后去除冷却剂流体的系统(28、29、30)。 。面板的电导率约为70 W / m / K,冷却液为低温气体或燃料。
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