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. 05, 2021

Filed:

Jan. 18, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Neal V. Huynh, Bellevue, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/42 (2006.01); B64C 13/50 (2006.01); B64C 13/16 (2006.01); B64C 9/20 (2006.01); F15B 20/00 (2006.01); B64C 9/18 (2006.01);
U.S. Cl.
CPC ...
B64C 13/42 (2013.01); B64C 9/18 (2013.01); B64C 9/20 (2013.01); B64C 13/16 (2013.01); B64C 13/503 (2013.01); B64C 13/504 (2018.01); F15B 20/004 (2013.01);
Abstract

Distributed trailing edge wing flap systems are described. An example wing flap system for an aircraft includes a flap and an actuator. The flap is movable between a deployed position and a retracted position relative to a fixed trailing edge of a wing of the aircraft. The actuator is to move the flap relative to the fixed trailing edge. The actuator is hydraulically drivable via first pressurized hydraulic fluid to be supplied by a hydraulic system of the aircraft. The actuator is also hydraulically drivable via second pressurized hydraulic fluid to be supplied by a local power unit. The local power unit is selectively connectable to an electrical system of the aircraft. The electrical system is to power the local power unit to supply the second pressurized hydraulic fluid.


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