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:
May. 16, 2023

Filed:

Jun. 23, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Michael M. Romero, Manchester, CT (US);

Neil J. Terwilliger, Cheshire, CT (US);

Daniel B. Kupratis, Wallingford, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/20 (2006.01); B64D 27/24 (2006.01); B64D 31/00 (2006.01); B64D 27/10 (2006.01); H02K 7/18 (2006.01);
U.S. Cl.
CPC ...
F02C 6/20 (2013.01); B64D 27/10 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); F05D 2220/70 (2013.01); H02K 7/1815 (2013.01);
Abstract

Techniques for determining a fan spool speed value associated with a hybrid electric gas engine ('engine') are described herein. For example, a method includes generating a first fan spool speed value based on a base extraction amount. The method further includes generating a change in the first fan spool speed value based on a flight condition and a change in extraction amount. The method further includes generating a second fan spool speed value based on the extraction amount and an augmentation value for intersection of a combustion instability and burner pressure limit. The method further includes generating a second change in the second fan spool speed value based on the flight condition and the change in extraction amount. The method further includes determining a final fan spool speed value and operating the engine at the final fan spool speed value.


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