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:
Apr. 07, 2020

Filed:

Apr. 25, 2014
Applicant:

Rohr, Inc., Chula Vista, CA (US);

Inventor:

Stuart J. Byrne, San Diego, CA (US);

Assignee:

Rohr, Inc., Chula Vista, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/76 (2006.01); F02K 1/62 (2006.01); F02K 1/70 (2006.01); F16C 11/04 (2006.01);
U.S. Cl.
CPC ...
F02K 1/763 (2013.01); F02K 1/62 (2013.01); F02K 1/625 (2013.01); F02K 1/70 (2013.01); F02K 1/76 (2013.01); F02K 1/766 (2013.01); F16C 11/045 (2013.01); F16C 2360/00 (2013.01);
Abstract

A drag link assembly for use in a thrust reverser of a propulsion system is provided. The thrust reverser includes a fixed structure and a translating structure that at least partially define an annular airstream bypass duct there between. The translating structure is moveable relative to the fixed structure. The translating structure includes a blocker door disposed at least partially within the airstream bypass duct. The drag link assembly includes a drag link fitting and a drag link. The drag link fitting is fastened to the fixed structure of the thrust reverser. The drag link includes a first end portion and an opposing second end portion. The first end portion is pivotably connected to the blocker door. The second end portion is pivotably connected to the drag link fitting. The second end portion includes a curved section.


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