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:
Oct. 12, 2021

Filed:

Jul. 27, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Kyle A. Thomas, Bellevue, WA (US);

Rhoda Rebecca Toliver, Summerville, SC (US);

Michael Roethle, North Charleston, SC (US);

Matthew Joseph Woerly, Renton, WA (US);

Matthew Senesac, Charleston, SC (US);

Kushy Sachdeva, Renton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 29/06 (2006.01); E05B 79/20 (2014.01); B64D 29/08 (2006.01); E05B 83/00 (2014.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
B64D 29/06 (2013.01); E05B 79/20 (2013.01); B64D 29/08 (2013.01); E05B 83/00 (2013.01); E05Y 2900/502 (2013.01); F01D 25/24 (2013.01); F05D 2240/14 (2013.01); F05D 2260/50 (2013.01); F16C 2350/52 (2013.01);
Abstract

An aircraft nacelle is disclosed and includes a first fan cowl and a second fan cowl. An opening is defined in an exterior surface of the first fan cowl. The aircraft nacelle also includes a blade, a latch mechanism, an arm, and a linkage assembly operably connecting the arm to the blade. The blade is moveable along between a stowed position and a deployed position. The latch mechanism is moveable between a latched position an unlatched position where a portion of the latch mechanism obstructs a path of movement of the blade. The arm is unable to move from an extended position where a portion of the arm extends through the opening in the exterior surface of the aircraft nacelle into a retracted position within an interior volume of the aircraft nacelle when the blade is in the deployed position and the latch mechanism is in the unlatched position.


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