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. 29, 2015

Filed:

Sep. 18, 2013
Applicant:

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

Inventors:

Grant Gordon, Peoria, AZ (US);

Hector Alonso Peralta-Duran, Avondale, AZ (US);

Richard Ling, Scottsdale, AZ (US);

Michael Gorelik, Phoenix, AZ (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/28 (2006.01); G05B 9/03 (2006.01); B64C 27/04 (2006.01); G05B 23/02 (2006.01); F02C 9/42 (2006.01);
U.S. Cl.
CPC ...
B64C 27/04 (2013.01); F02C 9/28 (2013.01); F02C 9/42 (2013.01); G05B 23/0283 (2013.01); G05B 23/0294 (2013.01); F05D 2220/329 (2013.01); F05D 2260/81 (2013.01); F05D 2270/11 (2013.01); F05D 2270/13 (2013.01);
Abstract

A system and method of adaptively managing a plurality of engines in a multi-engine system, where each engine comprises hot gas components and non-hot gas components, and each engine exhibits a performance margin and a remaining useful life, includes continuously, and in real-time, determining a plurality of different degradation mechanisms for each of the plurality of engines, and continuously, and in real-time, determining which of the determined degradation mechanisms is most limiting. The engines are controlled, based on the most limiting degradation mechanism, in a manner that the remaining useful lives of each engine are substantially equal. The plurality of different degradation mechanisms of each engine are determined based on the engine performance margin, modeled failure predictions of the hot gas components, and modeled failure predictions of the non-hot gas components.


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