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. 16, 2019

Filed:

Nov. 01, 2016
Applicant:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Inventor:

Mark Reinecke, Rockford, IL (US);

Assignee:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/26 (2006.01); F04C 14/24 (2006.01); F04C 2/10 (2006.01); F04C 14/18 (2006.01); F15B 7/00 (2006.01); F02K 9/84 (2006.01); F02K 9/97 (2006.01);
U.S. Cl.
CPC ...
B64G 1/26 (2013.01); F04C 2/10 (2013.01); F04C 14/18 (2013.01); F04C 14/24 (2013.01); F15B 7/003 (2013.01); F02K 9/84 (2013.01); F02K 9/97 (2013.01); F04C 2270/185 (2013.01); F04C 2270/44 (2013.01); F05D 2260/607 (2013.01); Y02T 50/675 (2013.01);
Abstract

A thrust vector control system is provided. The thrust vector control system may comprise an anti-stall hydraulic pump configured to deliver hydraulic fluid to at least one actuator, wherein each actuator may be configured to move an exhaust nozzle of a space vehicle. The anti-stall hydraulic pump may provide thermal conditioning to the thrust vector actuation control system during ground operation and/or periods of low output operation.


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