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Multi-Element Airfoil SystemA multi-element airfoil system includes an airfoil element having a leading edge region and a skin element coupled to the airfoil element. A slat deployment system is coupled to the slat and the skin element, and is capable of deploying and retracting the slat and the skin element. The skin element substantially fills the lateral gap formed between the slat and the airfoil element when the slat is deployed. The system further includes an uncoupling device and a sensor to remove the skin element from the gap based on a critical angle-of-attack of the airfoil element. The system can alternatively comprise a trailing edge flap, where a skin element substantially fills the lateral gap between the flap and the trailing edge region of the airfoil element. In each case, the skin element fills a gap between the airfoil element and the deployed flap or slat to reduce airframe noise.
Document ID
20150003321
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Turner, Travis L.
Khorrami, Mehdi R.
Lockard, David P.
McKenney, Martin J.
Atherley, Raymond D.
Kidd, Reggie T.
Date Acquired
March 19, 2015
Publication Date
July 1, 2014
Subject Category
Aerodynamics
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-13/449,807
Patent Number: US-Patent-8,763,958
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,763,958
Patent Application
US-Patent-Appl-SN-13/449,807
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