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:
Jan. 10, 2017

Filed:

Sep. 28, 2012
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Richard P. Meisner, Glastonbury, CT (US);

Brian V. Winebrenner, Tolland, CT (US);

Matthew R. Feulner, West Hartford, CT (US);

Boris Karpman, Marlborough, CT (US);

Juan A. Marcos, Middletown, CT (US);

David L. Ma, Avon, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/52 (2006.01); F02C 9/18 (2006.01); F01D 17/00 (2006.01); F01D 17/08 (2006.01); F04D 27/00 (2006.01); F02C 9/54 (2006.01);
U.S. Cl.
CPC ...
F01D 17/00 (2013.01); F01D 17/08 (2013.01); F02C 9/52 (2013.01); F02C 9/54 (2013.01); F04D 27/001 (2013.01); F02C 9/18 (2013.01); F05D 2270/101 (2013.01);
Abstract

A gas turbine engine comprises a compressor, a combustor, a turbine, and an electronic engine control system. The compressor, combustor, and turbine are arranged in flow series. The electronic engine control system is configured to generate a real-time estimate of compressor stall margin from an engine model, and command engine actuators to correct for the difference between the real time estimate of compressor stall margin and a required stall margin.


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