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Nacelle cooling and ventilation system

机译:机舱冷却和通风系统

摘要

A nacelle cooling and ventilation system for an aircraft gas turbine engine which includes a chin scoop and duct assembly for directing air through the engine bay where it is exhausted into the engine exhaust through an exhaust shroud eductor. The nacelle is enclosed so that effectively all of the cooling air entering the bay leaves the bay through the engine exhaust and is not dumped overboard, thereby adding to the effective thrust of the engine. An engine oil and generator oil heat exchanger is positioned in the cooling air duct into the bay so that the same air which cools the bay also cools engine and generator oil. The oil heat exchanger includes directional louvers which regulate and keep to a minimum the amount of cooling air and direct cooling air forwardly in the bay so that the entire bay area is cooled, and which can be shut as a fire control measure. The nacelle includes bay vent doors which are opened in response to a high oil temperature condition or in an engine shut-off condition on ground to provide auxiliary air flow from the bay. The doors are positionable by an actuator but can be disconnected from the actuator to pivot freely in response to a sudden increase in nacelle bay pressure.
机译:用于飞机燃气涡轮发动机的机舱冷却和通风系统,包括下巴铲和管道组件,用于引导空气通过发动机舱,然后通过排气罩喷射器将空气排放到发动机排气中。机舱是封闭的,因此进入机舱的所有冷却空气均有效地通过发动机排气口离开机舱,并且不会倾泻到舷外,从而增加了发动机的有效推力。机油和发电机油的热交换器位于进入机架的冷却空气管道中,因此,冷却机架的空气也可以冷却机油和发电机油。机油热交换器包括方向性百叶窗,该方向性百叶窗将冷却空气的量调节并保持在最低限度,并在机架中将冷却空气向前直接引导,以使整个机架区域得到冷却,并且可以将其关闭以作为消防措施。机舱包括舱门通风口门,这些门根据机油温度高的情况或在地面上的发动机关闭条件而打开,以提供来自舱门的辅助空气流。门可由致动器定位,但可以响应于机舱舱口压力的突然增加而与致动器断开连接以自由枢转。

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