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. 21, 2020

Filed:

Mar. 19, 2018
Applicant:

Woodward, Inc., Fort Collins, CO (US);

Inventors:

Joseph Thomas Kopecek, Santa Clarita, CA (US);

Julian Sweet, Pasadena, CA (US);

Assignee:

Woodward, Inc., Fort Collins, CO (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/76 (2006.01); F02K 1/62 (2006.01); B64D 33/04 (2006.01); B64D 27/16 (2006.01); F02K 1/60 (2006.01); B64D 29/06 (2006.01);
U.S. Cl.
CPC ...
F02K 1/763 (2013.01); B64D 27/16 (2013.01); B64D 29/06 (2013.01); B64D 33/04 (2013.01); F02K 1/60 (2013.01); F02K 1/605 (2013.01); F02K 1/62 (2013.01); F02K 1/766 (2013.01); F05D 2260/57 (2013.01); F05D 2270/64 (2013.01);
Abstract

A thrust reverser includes: a thrust-reversing element movable between a stowed position and a deployed position; at least one hydraulic actuator operably coupled to move the thrust-reversing element between the stowed and deployed positions; at least one hydraulic primary lock configured to transition, in response to a first activation pressure, between an engaged state, where movement of the thrust-reversing element is inhibited, and a released state, where movement of the thrust-reversing element is uninhibited; and a directional control unit fluidly coupled to the hydraulic actuator and the hydraulic primary lock, the directional control unit configured to transition from a first stage to a second stage in response to a second activation pressure that is greater than the first activation pressure, and where a transition from the first stage to the second stage by the directional control unit causes the hydraulic actuator to move the thrust-reversing element to the deployed position.


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