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:
Mar. 17, 2015

Filed:

Dec. 03, 2010
Applicant:

Michael John Burgess, Seattle, WA (US);

Inventor:

Michael John Burgess, Seattle, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/02 (2006.01); F02K 1/76 (2006.01); F02K 1/06 (2006.01); F02K 1/08 (2006.01); F02K 1/09 (2006.01); F02K 1/54 (2006.01); F02K 1/16 (2006.01); F15B 15/08 (2006.01); F15B 15/26 (2006.01); F02K 1/64 (2006.01);
U.S. Cl.
CPC ...
F02K 1/763 (2013.01); F02K 1/06 (2013.01); F02K 1/08 (2013.01); F02K 1/09 (2013.01); F02K 1/54 (2013.01); F02K 1/76 (2013.01); F02K 1/16 (2013.01); F15B 15/088 (2013.01); F15B 15/261 (2013.01); Y02T 50/671 (2013.01); F02K 1/64 (2013.01);
Abstract

There is provided an actuation system for a gas turbine engine including a thrust reverser and a variable area fan nozzle. The system has a plurality of linear actuators each having a first outer piston concentric with a second inner piston. The first outer piston is operatively connected to a thrust reverser. The second inner piston is operatively connected to a variable area fan nozzle. The system further has a piston lock assembly for selectively locking the first outer piston to the second inner piston. The system further has a control system coupled to the plurality of linear actuators for operating the variable area fan nozzle between a stowed position and a deployed position.


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