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SUPERSONIC RAMJET ENGINE TRACTION AND ECONOMIC CHARACTERISTICS INCREASING METHOD (OPTIONS)

机译:超音速喷气发动机的牵引和经济特性的增加方法(选择)

摘要

FIELD: engines and pumps.;SUBSTANCE: supersonic ramjet engine traction and economic characteristics increasing method includes flowing into its flow path supersonic air stream compression with the air intake device multi-jerk braking surface, air flow into the combustion chamber supply through the flow path, the fuel into the combustion chamber supply and the fuel combustion products discharge through the jet nozzle. Also performing the air flow removal, and the air duct closing by the closing device. Removal is performed from the braking surface in front of the air intake device neck through the grid of holes and the air duct into the external air flow reduced pressure acting zone, after the static pressure increase in the air intake device neck. At that, the air flow part removal is carried out through the opening in the flow path wall at the combustion chamber input and the combustion chamber and the jet nozzle cavity. For the air duct closing device operation using the air flow increased static pressure at the combustion chamber input after the fuel ignition therein.;EFFECT: invention is aimed at the air from the air intake device removal communication channel closing device design simplification and the aircraft side wall additional heating elimination.;2 cl, 3 dwg
机译:领域:发动机和泵。物质:超音速冲压喷气发动机的牵引力和经济特性的提高方法包括:将超音速气流压缩到带有进气装置的多冲击制动表面的超音速气流中,使空气通过流路进入燃烧室供应,燃料进入燃烧室供应,燃料燃烧产物通过喷嘴排出。还执行气流去除,并且通过关闭装置关闭风道。在进气装置颈部中的静压增加之后,从进气装置颈部前面的制动表面通过孔的网格和空气导管进行排气,以进入外部气流减小的压力作用区域。在此,通过在燃烧室入口处以及燃烧室和喷嘴腔处的流路壁中的开口进行空气流动部分的去除。对于风道关闭装置的操作,其使用的空气流在燃料被点燃之后在燃烧室输入处增加了在燃烧室输入处的静压力。效果:本发明旨在简化来自进气装置移除连通通道的空气封闭装置的设计和飞机侧消除墙面的额外热量。; 2 cl,3 dwg

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