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:
May. 13, 2014

Filed:

Mar. 02, 2011
Applicants:

John Michael Welch, Wichita, KS (US);

Christopher Steven Sawyer, Udall, KS (US);

Inventors:

John Michael Welch, Wichita, KS (US);

Christopher Steven Sawyer, Udall, KS (US);

Assignee:

Spirit AeroSystems, Inc., Wichita, KS (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/02 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
F02K 1/763 (2013.01); F02K 1/766 (2013.01);
Abstract

A translating sleeve assembly for use with an aircraft engine thrust reverser broadly comprises a slider track, a lifting bolt, and a hinge. The slider track may include a tubular sidewall and a guide channel formed therein that follows a curved path along a length thereof. The lifting bolt may be slidably positioned within the slider track. The hinge may include a first hinge element with a base coupled to an outer cowl shroud, a second hinge element with a hinge rod slidably positioned within the guide channel, and a pin about which the first hinge element and the second hinge element pivot. During deployment of the thrust reverser, the lifting bolt slides aftward and the hinge rod slides within the guide channel, urging the lifting bolt to pivot and the hinge to open, thereby lifting the outer cowl shroud away from the center of the aircraft engine.


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