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:
Jan. 26, 2016

Filed:

Oct. 20, 2011
Applicants:

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

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

David P Lockard, Hampton, VA (US);

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

Craig L. Streett, Virginia Beach, VA (US);

Douglas Leo Weber, Hayes, VA (US);

Inventors:

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

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

David P Lockard, Hampton, VA (US);

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

Craig L. Streett, Virginia Beach, VA (US);

Douglas Leo Weber, Hayes, VA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 9/24 (2006.01); B64C 9/22 (2006.01); B64C 3/48 (2006.01);
U.S. Cl.
CPC ...
B64C 9/22 (2013.01); B64C 3/48 (2013.01); B64C 9/24 (2013.01); B64C 2230/14 (2013.01); Y02T 50/145 (2013.01); Y02T 50/32 (2013.01);
Abstract

A slat cove filler is utilized to reduce airframe noise resulting from deployment of a leading edge slat of an aircraft wing. The slat cove filler is preferably made of a super elastic shape memory alloy, and the slat cove filler shifts between stowed and deployed shapes as the slat is deployed. The slat cove filler may be configured such that a separate powered actuator is not required to change the shape of the slat cove filler from its deployed shape to its stowed shape and vice-versa. The outer contour of the slat cove filler preferably follows a profile designed to maintain accelerating flow in the gap between the slat cove filler and wing leading edge to provide for noise reduction.


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