首页> 外国专利> HELICOPTER ROTOR AND TRANSMISSION MOUNTING AND VIBRATION ISOLATION SYSTEM

HELICOPTER ROTOR AND TRANSMISSION MOUNTING AND VIBRATION ISOLATION SYSTEM

机译:直升机转子和变速器的安装和振动隔离系统

摘要

The rotor(16) & the transmission(14) of a helicopter are mounted on the fuselage(12) by a vibration isolating assembly. The assembly includes a number of elastomeric counts(20,22) each of which incorporates alternate layers of elastomer and metal laminates. The mounts are subject to compression & are located about the axis of the rotor. Four mounts are used, the axes of the forward two intersecting on the roll axis, & the axes of the rearward two also intersecting on the roll axis but further back.
机译:直升机的旋翼(16)和变速器(14)通过隔振组件安装在机身(12)上。该组件包括多个弹性体计数(20,22),每个弹性体计数都包含弹性体和金属层压板的交替层。支座承受压缩力,并且绕转子轴线定位。使用四个安装座,前两个的轴在侧倾轴上相交,后两个的轴在侧倾轴上相交,但又向后。

著录项

  • 公开/公告号KR820000274B1

    专利类型

  • 公开/公告日1982-03-15

    原文格式PDF

  • 申请/专利权人 UNITED TECHN CORP;

    申请/专利号KR19770003018

  • 发明设计人 EASTMAN LARRY B;KENIGSBERG IRWIN J;

    申请日1977-12-23

  • 分类号B64C27/00;

  • 国家 KR

  • 入库时间 2022-08-22 13:02:20

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