发明名称 REDUNDANT STABILIZER SUPPORT
摘要 A horizontal stabilizer for a helicopter has two airfoil sections, one on each side of a tail cone. A stabilizer joining and torque tube mechanism comprising two concentric tubes mounted on bearings in the tail cone extends through the tail cone and beyond into the airfoil sections wherein the tubes terminate at laterally spaced points, the inner tube being longer than the outer tube. To transmit torque from the shafts to the airfoil sections a torque tube housing is provided in each airfoil section which conforms externally to and is connected to its airfoil section and which receives the end portions of both tubes and is bolted to them. An actuating lever for the stabilizer is provided on the torque tube mechanism within the tail cone which is connected to pilot controlled linkage.
申请公布号 US3706432(A) 申请公布日期 1972.12.19
申请号 USD3706432 申请日期 1971.09.14
申请人 UNITED AIRCRAFT CORP. 发明人 JOHN ACCASHIAN
分类号 B64C27/26;B64C27/82;(IPC1-7):B64C13/04 主分类号 B64C27/26
代理机构 代理人
主权项
地址