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Control Surface ActuatorA device which actuates aircraft control surfaces is disclosed. The actuator is disposed entirely within the control surface structure. This allows the gap between the wing structural box and the control surface to be reduced. Reducing the size of the gap is especially desirable for wings with high aspect ratio, wherein the volume of the structural box is at a premium.
Document ID
19890002367
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Seidel, Gerhard E. (Boeing Commercial Airplane Co. Renton, Wash., United States)
Date Acquired
August 14, 2013
Publication Date
September 27, 1988
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-PATENT-4,773,620
Patent Number: NASA-CASE-LAR-12852-1
Patent Application Number: US-PATENT-APPL-SN-028832
Accession Number
89N11738
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,773,620|NASA-CASE-LAR-12852-1
Patent Application
US-PATENT-APPL-SN-028832

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