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:
Jun. 15, 2021

Filed:

Oct. 27, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Kevin R. Tsai, Seattle, WA (US);

Bruce A. Dahl, Kent, WA (US);

Gregory M. Santini, Bothell, WA (US);

Kyle A. Johnson, Fall City, WA (US);

Seiya Sakurai, Seattle, WA (US);

Stephen R. Amorosi, Seattle, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/38 (2006.01); B64C 5/10 (2006.01); F16H 21/44 (2006.01); F16H 51/00 (2006.01); B64C 5/08 (2006.01); F16H 25/22 (2006.01);
U.S. Cl.
CPC ...
B64C 5/10 (2013.01); B64C 3/38 (2013.01); B64C 5/08 (2013.01); F16H 21/44 (2013.01); F16H 25/2204 (2013.01); F16H 51/00 (2013.01);
Abstract

A trailing edge flap actuation mechanism has a flap drive link with a first end pivotally coupled to a fore flap structure of a flap and a second end pivotally coupled to an underwing support structure. An aft tension link has a leading end pivotally coupled proximate an aft end of the underwing support structure and a trailing end coupled to a mid-section structure of the flap. An actuator, when actuated, rotates the flap drive link about a first pivot axle to move the flap between a retracted position and a deployed lowered position. The actuator, including a ball-screw drive shaft having a universal joint, is positioned in a cove above the underwing support structure whereby the extent that the underwing support structure protrudes below the wing is reduced.


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