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Variable air intake ramps for aerospace vehicles

机译:航空航天器的可变进气道

摘要

The invention relates to engine air intakes for aerospace vehicles in which a variable geometry ramp system is employed for matching air intake flow to propulsion engine demand. To alleviate the induced high pressure loads on the ramps and the ramp actuators arising from the air intake flow a reacting pressure is applied to the opposite face of the ramps. The ramp assembly in addition to defining the required air intake duct geometry further defines the adjacent boundary of an enclosure which is pressurised by ram air and vented as required as a function of the load on one of the ramp actuating jacks to give the desired load alleviation.
机译:本发明涉及用于航空航天器的发动机进气口,其中采用可变几何形状的坡道系统使进气流量与推进发动机需求相匹配。为了减轻由进气流引起的在斜坡和斜坡致动器上引起的高压负载,将反作用压力施加到斜坡的相对面。坡道组件除了定义所需的进气管道几何形状外,还定义了外壳的相邻边界,该外壳边界被冲压空气加压并根据需要根据坡道致动千斤顶之一上的负载进行排气,以减轻所需的负载。

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