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Triple circuit lubrication device with increased reliability for a main power transmission gearbox of an aircraft

机译:用于飞机主动力传动齿轮箱的可靠性提高的三回路润滑装置

摘要

A triple circuit lubrication device for lubricating a mechanical system, the lubrication device being provided with two independent lubrication circuits, a tank common to both lubrication circuits and containing a lubrication liquid, and a tertiary circuit in which a tertiary liquid flows. Each lubrication circuit comprises pipes, and respective pressure sensors, pumps, heat exchangers, spray nozzles, and suction points for sucking up the lubrication liquid situated in the tank. The second suction point is situated below the high first suction point. The tertiary circuit comprises a third pump, a third pressure sensor, the second heat exchanger, and a third heat exchanger, thus serving to cool the lubrication liquid flowing through the second lubrication circuit.
机译:一种用于润滑机械系统的三回路润滑装置,该润滑装置设置有两个独立的润滑回路,两个润滑回路共用的并包含润滑液的储罐以及第三液体在其中流动的第三回路。每个润滑回路均包括管道,以及各自的压力传感器,泵,热交换器,喷嘴和吸油口,这些吸油口用于吸取位于油箱中的润滑液。第二抽吸点位于较高的第一抽吸点之下。第三回路包括第三泵,第三压力传感器,第二热交换器和第三热交换器,因此用于冷却流过第二润滑回路的润滑液。

著录项

  • 公开/公告号US9829088B2

    专利类型

  • 公开/公告日2017-11-28

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号US201514924776

  • 发明设计人 DAMIEN GOUJET;

    申请日2015-10-28

  • 分类号F16H57/04;B64C27/12;B64C27/14;

  • 国家 US

  • 入库时间 2022-08-21 12:54:53

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