首页> 外国专利> Safety clutch for aircraft propeller, has strangled openings to control and regulate hydraulic fluid flow for varying sliding between driving and driven shafts to absorb weak and strong vibrations, and irregular and inverse torques

Safety clutch for aircraft propeller, has strangled openings to control and regulate hydraulic fluid flow for varying sliding between driving and driven shafts to absorb weak and strong vibrations, and irregular and inverse torques

机译：飞机螺旋桨安全离合器，具有绞合开口，可控制和调节液压油流量，以改变驱动轴和从动轴之间的滑动，从而吸收弱振动和强振动以及不规则和反向扭矩

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摘要

The clutch has a casing (2) integral with driving and driven shafts having housings for hydraulic pump units. The casing has a hydraulic fluid cavity (17), a low pressure reservoir (14) and a high pressure reservoir (16). Strangled openings (7) control and regulate the hydraulic fluid flow to vary angular sliding between the shafts for absorbing weak and strong vibrations, high irregular torques and inverse torques.

机译：该离合器具有与驱动轴和从动轴成一体的壳体（2），该驱动轴和从动轴具有用于液压泵单元的壳体。壳体具有液压流体腔（17），低压储液器（14）和高压储液器（16）。弯曲的开口（7）控制和调节液压流体的流量，以改变轴之间的角向滑动，从而吸收弱振动和强振动，高不规则扭矩和反扭矩。

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公开/公告号FR2856123A1

专利类型
公开/公告日2004-12-17

原文格式PDF
申请/专利权人 MASSE CLAUDE PHILIPPE;
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申请/专利号FR20030007071
发明设计人 MASSE CLAUDE PHILIPPE;
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申请日2003-06-12
分类号F16D31/04;
国家 FR
入库时间 2022-08-21 21:58:26

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