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:
Dec. 10, 2019

Filed:

Jul. 10, 2017
Applicant:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Inventors:

Robert M. DeRoy, Tolland, CT (US);

Adam Woods, Suffield, CT (US);

Assignee:

HAMILTON SUNDSTRAND CORPORATION, Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); F02C 9/52 (2006.01); F02C 6/08 (2006.01); B64D 31/06 (2006.01); F02C 7/18 (2006.01); B64D 13/06 (2006.01); B64D 15/04 (2006.01); B64D 13/08 (2006.01);
U.S. Cl.
CPC ...
F02C 9/52 (2013.01); F02C 6/08 (2013.01); B64D 13/08 (2013.01); B64D 15/04 (2013.01); B64D 31/06 (2013.01); B64D 2013/0618 (2013.01); B64D 2013/0696 (2013.01); F02C 7/18 (2013.01); F05D 2220/323 (2013.01); F05D 2220/50 (2013.01); F05D 2260/20 (2013.01); F05D 2270/11 (2013.01); F05D 2270/114 (2013.01); F05D 2270/44 (2013.01); F05D 2270/54 (2013.01);
Abstract

A fuel and bleed controller is provided. The fuel and bleed controller includes a processor and a memory. The memory stores program instructions thereon. The program instructions are executable by the processor to cause the fuel and bleed controller to send status requests to systems of the aircraft. The systems comprise a bleed system and bleed user controllers. The program instructions are further executable by the processor to cause the fuel and bleed controller to receive status responses from the systems of the aircraft and determine fuel requirements based on the status responses in advance of operational needs by the systems of the aircraft. The program instructions are further executable by the processor to cause the fuel and bleed controller to control engines of the aircraft based on the fuel requirements.


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