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:
Jul. 27, 2021

Filed:

Apr. 13, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Michael Thomas Fox, Saint Charles, MO (US);

Eric Anton Howell, Ballwin, MO (US);

Jeffrey M. Roach, St. Charles, MO (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/40 (2006.01); F15B 1/02 (2006.01); F15B 1/26 (2006.01); F15B 13/04 (2006.01); F04B 1/146 (2020.01); F04B 49/08 (2006.01);
U.S. Cl.
CPC ...
B64C 13/40 (2013.01); F15B 1/02 (2013.01); F15B 1/26 (2013.01); F15B 13/0416 (2013.01); F04B 1/146 (2013.01); F04B 49/08 (2013.01);
Abstract

A hydraulic system for an aircraft. The hydraulic system can include a hydraulic actuator that is operatively coupled to a flight control member. Hydraulic fluid is moved through the hydraulic system by an engine driven pump that delivers hydraulic fluid to the actuator at a first pressure, and a boost pump that delivers hydraulic fluid to the actuator at a second pressure that is higher than the first pressure. The hydraulic system is configured such that the hydraulic fluid returning from the actuator to the engine driven pump can be delivered to the boost pump prior to reaching the engine driven pump.


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