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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

HELICOPTER ROTOR AND TRANSMISSION MOUNTING AND VIBRATION ISOLATION SYSTEM A helicopter rotor and transmission mounting and vibration isolation system in which the transmission is supported from the fuselage by a plurality of elastomeric mounts which are selectively positioned and focused to establish a system roll axis and a system pitch axis on opposite sides of the elastomeric mounts and which mount members are of selected stiffness to establish selected roll stiffness and selected pitch stiffness of the system, to establish the natural frequencies of the system sufficiently below the blade passage frequency to minimize the response of the fuselage to forces and moments imparted by the helicopter rotor and to provide selected torque restraint and lift restraint for the system.
机译:直升机旋翼和变速箱的安装和振动隔离系统一种直升机旋翼和变速箱的安装和振动隔离系统,其中变速箱由多个弹性体支架从机身支撑,这些弹性体支架被选择性地定位和聚焦以建立系统侧倾轴线和系统俯仰角轴位于弹性体安装座的相对两侧,并且这些安装座部件具有选定的刚度,以建立系统的选定的侧倾刚度和选定的俯仰刚度,以建立足够低于叶片通过频率的系统固有频率,以最小化机身的响应直升机直升机施加的力和力矩,并为系统提供选定的扭矩限制和升力限制。

著录项

  • 公开/公告号IL53523A

    专利类型

  • 公开/公告日1982-11-30

    原文格式PDF

  • 申请/专利权人 UNITED TECHNOLOGIES CORP;

    申请/专利号IL19770053523

  • 发明设计人

    申请日1977-12-02

  • 分类号B64C27/00;

  • 国家 IL

  • 入库时间 2022-08-22 11:08:49

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