首页> 外国专利> Dual circuit lubrication method and device with increased reliability for a main power transmission gearbox of an aircraft

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可靠性提高的双回路润滑方法及装置

摘要

A dual circuit lubrication device for lubricating a mechanical system, the lubrication device being provided with two independent lubrication circuits and a tank that is common to both lubrication circuits and that contains a lubrication liquid. A first lubrication circuit has two first suction points for sucking in the lubrication liquid and situated inside the tank, and a second lubrication circuit includes a second suction point for sucking in the lubrication liquid and situated inside the tank. The dual circuit lubrication device has means for detecting the lubrication liquid passing below a limit depth in the tank, which means are formed by a high first suction point situated at the level of the limit depth, the second suction point being situated below the limit depth, and a low first suction point being below the second suction point.
机译:一种用于润滑机械系统的双回路润滑装置,该润滑装置设置有两个独立的润滑回路和一个油箱,该油箱对于两个润滑回路都是公用的,并包含润滑液。第一润滑回路具有两个第一抽吸点,用于吸入润滑液并位于油箱内,第二润滑回路包括第二抽吸点,用于吸入润滑液并位于油箱内。该双回路润滑装置具有用于检测在油箱中的极限深度以下通过的润滑液的装置,该装置由位于极限深度水平的较高的第一抽吸点形成,第二抽吸点位于极限深度以下,并且较低的第一吸气点低于第二吸气点。

著录项

  • 公开/公告号US9732840B2

    专利类型

  • 公开/公告日2017-08-15

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号US201514924790

  • 发明设计人 JEAN-GUY HARREAU;

    申请日2015-10-28

  • 分类号F16H57/04;B64C27/14;F16N29/00;

  • 国家 US

  • 入库时间 2022-08-21 13:47:04

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