首页> 外国专利> A DUAL CIRCUIT LUBRICATION METHOD AND DEVICE WITH INCREASED RELIABILITY FOR A MAIN POWER TRANSMISSION GEARBOX OF AN AIRCRAFT

A DUAL CIRCUIT LUBRICATION METHOD AND DEVICE WITH INCREASED RELIABILITY FOR A MAIN POWER TRANSMISSION GEARBOX OF AN AIRCRAFT

机译:飞机主动力传动齿轮箱的双回路润滑方法及可靠性提高的装置

摘要

The present invention relates to a lubrication device (1) dual-circuit of a mechanical system (3), said lubricating device (1) having two lubricating circuits (10,20) and independent from a reservoir (2) common to the two lubricating circuits (10,20) and containing a lubricating liquid. A first lubrication circuit (10) comprises two first suction point (16,17) of said lubricating liquid in said reservoir (2) and a second lubrication circuit (20) includes a second suction point (27) said lubricating liquid in said reservoir (2). Said lubricating device (1) dual-circuit comprises a passage detecting means below a limit height of said lubricating liquid in said container (2) formed by a first suction high point (16) located at said boundary height, said second suction point (27) being located below said limit height and a first low point of suction (17) being below said second suction point (27).
机译:本发明涉及一种机械系统(3)的双回路润滑装置(1),所述润滑装置(1)具有两个润滑回路(10,20),并且独立于两个润滑共用的储液器(2)。回路(10,20)并包含润滑液。第一润滑回路(10)包括在上述储存器(2)中的所述润滑液体的两个第一抽吸点(16,17),第二润滑回路(20)包括在上述储存器(2)中的所述润滑液体的第二抽吸点(27) 2)。所述润滑装置(1)双回路包括通道检测装置,其位于所述容器(2)中的所述润滑液的极限高度以下,该极限高度由位于所述边界高度处的第一抽吸高点(16),所述第二抽吸点(27)形成)位于所述极限高度之下,而第一低吸力点(17)位于所述第二吸力点(27)之下。

著录项

  • 公开/公告号EP3021030A1

    专利类型

  • 公开/公告日2016-05-18

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号EP20150186183

  • 发明设计人 HARREAU JEAN-GUY;

    申请日2015-09-22

  • 分类号F16N29/00;F16H57/00;

  • 国家 EP

  • 入库时间 2022-08-21 14:49:38

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