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Transmission System in aero-engine Hydraulic Pumping.

机译:航空发动机液压泵中的传动系统。

摘要

Hydraulic Transmission System in aero-engine.Comprises: a Hydraulic Fluid Reservoir (13) arranged on the platform (4) that has a Cylinder (29) with a Sealing ring (31) in contact with the casing (10) and lock the bearing surfaces (5,6); a Fluid pump (14) that drives the Hydraulic Fluid; a Collector device (15) which has a Central Body (7) and a casing (10) or support bearings (8, 9); connecting Pipes,Drive (16) and (17) between the return Fluid pump (14) and Connecting Pipes Flow and return between the collector device (15) and the engine that drives the Hydraulic pump.
机译:航空发动机的液压传动系统,包括:布置在平台(4)上的液压油箱(13),该液压油箱(13)的气缸(29)带有与壳体(10)接触的密封环(31),并锁定轴承表面(5,6);驱动液压油的液压泵(14);具有中央主体(7)和壳体(10)或支撑轴承(8、9)的收集器装置(15);在回油泵(14)和连接管之间连接管道,驱动器(16)和(17),并在收集器(15)和驱动液压泵的发动机之间进行回油。

著录项

  • 公开/公告号ES8701092A1

    专利类型

  • 公开/公告日1987-02-16

    原文格式PDF

  • 申请/专利权人 FIGOLS MANESCAL JUAN;

    申请/专利号ES19860551881

  • 发明设计人

    申请日1986-02-03

  • 分类号B64C27/64;

  • 国家 ES

  • 入库时间 2022-08-22 07:17:18

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