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US Patent 8038394 System and method of damping a 1P motion

Patent 8038394 was granted and assigned to Sikorsky Aircraft on October, 2011 by the United States Patent and Trademark Office.

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Patent
Patent

Patent attributes

Current Assignee
Sikorsky Aircraft
Sikorsky Aircraft
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
8038394
Patent Inventor Names
Brandon L. Stille2
William A. Welsh2
Timothy Fred Lauder2
Date of Patent
October 18, 2011
Patent Application Number
12015149
Date Filed
January 16, 2008
Patent Citations Received
‌
US Patent 12122525 Redundant load path for powered lift tilt actuator
1
Patent Primary Examiner
‌
Edward Look
Patent abstract

A rotor system includes a multiple of rotor blade yokes mounted to a rotor hub. A lead/lag damper is mounted to each of the rotor blade yokes and to a damper hub. An actuator system is operable to shift a damper hub axis of rotation relative the rotor axis of rotation to minimize 1P damper motions. A method of minimizing 1P damper motions within a rotor system includes shifting the damper hub axis of rotation relative the rotor axis of rotation to oscillate an inner connector of each lead/lag damper in phase with a 1P blade motion to minimize the 1P motion of the damper.

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