The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 01, 2014

Filed:

Apr. 18, 2012
Applicants:

Travis L. Turner, Yorktown, VA (US);

Mehdi R. Khorrami, Norfolk, VA (US);

David P. Lockard, Hampton, VA (US);

Martin J. Mckenney, Virginia Beach, VA (US);

Raymond D. Atherley, Norfolk, VA (US);

Reggie T. Kidd, Hampton, VA (US);

Inventors:

Travis L. Turner, Yorktown, VA (US);

Mehdi R. Khorrami, Norfolk, VA (US);

David P. Lockard, Hampton, VA (US);

Martin J. McKenney, Virginia Beach, VA (US);

Raymond D. Atherley, Norfolk, VA (US);

Reggie T. Kidd, Hampton, VA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 3/50 (2006.01);
U.S. Cl.
CPC ...
Abstract

A 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.


Find Patent Forward Citations

Loading…