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Composite flight-control actuator developmentThe composite actuator is 'jam resistant', satisfying a survivability requirement for the Navy. Typically, the push-pull force needed to drive through the wound area of the composite actuator is 73 percent less than that of an all-metal actuator. In addition to improving the aircraft's combat survivability, significant weight savings were realized. The current design of the survivable, composite actuator cylinder is 36 percent lighter than that of the production steel cylinder, which equates to a 15 percent overall actuator weight savings.
Document ID
19950021860
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bott, Richard
(Naval Weapons Center China Lake, CA, United States)
Ching, Fred
(Textron, Inc. Valencia, CA., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Publication Information
Publication: FAA, Ninth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Volume 3
Subject Category
Aircraft Stability And Control
Accession Number
95N28281
Funding Number(s)
CONTRACT_GRANT: N60530-88-C-0260
Distribution Limits
Public
Copyright
Public Use Permitted.
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