Invention Grant
- Patent Title: Rotary wing aircraft pitch beam attachment with anti-rotation plate design
- Patent Title (中): 旋翼飞机俯仰梁附件带防旋转板设计
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Application No.: US13778741Application Date: 2013-02-27
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Publication No.: US09441495B2Publication Date: 2016-09-13
- Inventor: David N. Schmaling , Richard Thomas Hood , Evan Sobel
- Applicant: Sikorsky Aircraft Corporation
- Applicant Address: US CT Stratford
- Assignee: SIKORSKY AIRCRAFT CORPORATION
- Current Assignee: SIKORSKY AIRCRAFT CORPORATION
- Current Assignee Address: US CT Stratford
- Agency: Cantor Colburn LLP
- Main IPC: F01D7/00
- IPC: F01D7/00 ; F16D1/108 ; B64C27/82 ; F16D1/10

Abstract:
A retaining assembly for a tail rotor system is provided including a washer having a plurality of splines. The washer is configured to couple to an adjacent pitch change shaft. A retaining nut includes a self-locking feature and a flange arranged at a first end. The retaining nut is configured to threadably couple to the pitch change shaft such that the flange is in contact with the washer. The flange includes a plurality of first holes configured to at least partially align between the splines of the washer. A lock plate includes a body and a plurality of tabs extending generally perpendicularly from the body. The lock plate is slidably positioned about the pitch change shaft adjacent the flange. The lock plate is operably coupled to the retaining nut and the washer to limit rotational movement thereof relative to the pitch change shaft.
Public/Granted literature
- US20140241884A1 ROTARY WING AIRCRAFT PITCH BEAM ATTACHMENT WITH ANTI-ROTATION PLATE DESIGN Public/Granted day:2014-08-28
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