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Miniature Trailing Edge Effector for Aerodynamic ControlImproved miniature trailing edge effectors for aerodynamic control are provided. Three types of devices having aerodynamic housings integrated to the trailing edge of an aerodynamic shape are presented, which vary in details of how the control surface can move. A bucket type device has a control surface which is the back part of a C-shaped member having two arms connected by the back section. The C-shaped section is attached to a housing at the ends of the arms, and is rotatable about an axis parallel to the wing trailing edge to provide up, down and neutral states. A flip-up type device has a control surface which rotates about an axis parallel to the wing trailing edge to provide up, down, neutral and brake states. A rotating type device has a control surface which rotates about an axis parallel to the chord line to provide up, down and neutral states.
Document ID
20090002664
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Lee, Hak-Tae
Bieniawski, Stefan R.
Kroo, Ilan M.
Date Acquired
August 24, 2013
Publication Date
August 12, 2008
Subject Category
Aircraft Stability And Control
Report/Patent Number
Patent Number: US-Patent-7,410,133
Patent Application Number: US-Patent-Appl-SN-11/646,186
Funding Number(s)
CONTRACT_GRANT: NN104AAA79G
CONTRACT_GRANT: F49620-98-1-0299
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,410,133
Patent Application
US-Patent-Appl-SN-11/646,186
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