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:
May. 16, 2017

Filed:

May. 15, 2014
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventors:

Kevin K. Chakkera, Chandler, AZ (US);

Ron Vaughan, Gilbert, AZ (US);

Steve Abel, Chandler, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/76 (2006.01); F01D 17/26 (2006.01); F02K 1/72 (2006.01); F02K 1/74 (2006.01);
U.S. Cl.
CPC ...
F02K 1/763 (2013.01); F01D 17/26 (2013.01); F02K 1/72 (2013.01); F02K 1/74 (2013.01); F02K 1/76 (2013.01); F02K 1/766 (2013.01); F05D 2250/411 (2013.01); F05D 2260/406 (2013.01); F05D 2270/64 (2013.01); F05D 2270/66 (2013.01);
Abstract

An aircraft thrust reverser actuation system includes a plurality of actuator assemblies that are each configured, upon receipt of a drive torque, to move to a position. The rotary hydraulic motor is coupled to each of the actuator assemblies and is configured, upon receipt of hydraulic fluid, to rotate and supply the drive torque to each of the actuator assemblies. The control valve is in fluid communication with the rotary hydraulic motor and is configured, upon receipt of electrical current, to move to a valve position based on the magnitude of the received electrical current, to thereby control the direction and flow of hydraulic fluid to the hydraulic motor. The valve control is configured, upon receipt of thrust reverser commands, to supply the electrical current to the control valve and selectively vary the magnitude of the electrical current based on the positions of the actuator assemblies.


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