发明名称 HELICOPTER ROTOR AND TRANSMISSION MOUNTING AND VIBRATION ISOLATION SYSTEM
摘要 <p>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.</p>
申请公布号 CA1066683(A) 申请公布日期 1979.11.20
申请号 CA19770292588 申请日期 1977.12.07
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 KENIGSBERG, IRWIN J.;EASTMAN, LARRY B.
分类号 B64C27/51;B64C27/00;(IPC1-7):64C27/12 主分类号 B64C27/51
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