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Aero engine storage chamber venting system and method of providing a desired pressure ratio to bearing chamber seals of an air sealed storage chamber

机译:航空发动机储藏室排气系统和向气密储藏室的轴承室密封件提供所需压力比的方法

摘要

A storage compartment ventilation system for an aircraft engine, comprising: - at least one storage chamber (1) air-sealed via sealing chamber seals (7) with bearing elements (2) which are intended to support a mechanical part (3) of an aircraft engine, - at least one with the Bearing chamber (1) connected vent line (9) via which in the storage chamber (1) befindliches oil / air mixture from the storage chamber (1) is vented, - an oil separator (11) into which the vent line (9) opens, the oil separator (11) is supplied with the oil / air mixture of the storage chamber (1), - an oil return line (12) connected to the oil separator, through which oil separated from the oil / air mixture is discharged, and - an air discharge line connected to the oil separator (13) through which purified air (23) into the environment (14) is derived, wherein in the air outlet duct (13) an air ejector (15) is arranged, the is provided, the gas ejector (15) supplied gas (17) at a speed in the air outlet pipe (13) eject, which is greater than the speed of in the air outlet line (13) flowing from the oil separator (11) into the environment (14 ) derived air (23), characterized in that the air ejector (15) with the supply air or the exhaust air of a starter (19) of the aircraft engine can be acted upon.
机译:一种用于飞机发动机的储藏室通风系统,包括:-至少一个储藏室(1),通过带有轴承元件(2)的密封室密封件(7)进行气封,该轴承元件用于支撑发动机的机械部件(3)。飞机发动机,-至少一个轴承室(1)连接有排气管(9),通过它在存储室(1)中排出从存储室(1)流出的油/空气混合物,-油分离器(11 ),通向排气管路(9)的油,向油分离器(11)供给储油腔(1)的油/空气混合物,-与油分离器连接的回油管线(12),通过油分离出与油/空气混合物分离的空气,以及-连接至油分离器(13)的空气排放管线,通过该空气排放管线将净化后的空气(23)引入到环境(14)中,其中,在空气出口管道(13)中设置,设置有空气喷射器(15),气体喷射器(15)以一定速度在空气出口管中供应气体(17)。 (13)喷射,其速度大于从油分离器(11)流入环境(14)的空气出口管路(23)衍生的空气(23)的速度,其特征在于,空气喷射器(15)具有可以作用于飞机发动机的启动器(19)的供应空气或排气。

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