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:
Mar. 29, 2022

Filed:

Oct. 16, 2019
Applicant:

Rolls-royce North American Technologies Inc., Indianapolis, IN (US);

Inventors:

Douglas Boyd, Indianapolis, IN (US);

Douglas D. Dierksmeier, Franklin, IN (US);

Douglas J. Snyder, Carmel, IN (US);

Graham Burkholder, Avon, IN (US);

William B. Bryan, Indianapolis, IN (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/06 (2006.01); F02C 9/18 (2006.01); F02K 3/115 (2006.01); F02K 1/74 (2006.01); F02C 7/18 (2006.01); F02C 3/04 (2006.01); F02C 6/08 (2006.01);
U.S. Cl.
CPC ...
F02K 1/74 (2013.01); F02C 7/18 (2013.01); F02C 7/185 (2013.01); F02K 3/06 (2013.01); F02C 3/04 (2013.01); F02C 6/08 (2013.01); F02C 9/18 (2013.01); F02K 3/115 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2240/35 (2013.01); F05D 2260/213 (2013.01); F05D 2260/606 (2013.01);
Abstract

A gas turbine engine system includes a gas turbine engine having a fan bypass duct, a heat exchanger system, and a flow transfer unit configured to selectively allow or preclude flow between the fan bypass duct and the heat exchanger system. A controller is coupled to and configured to vary the state of one or more of a fan exit nozzle, a heat exchanger exit nozzle, and a flow control valve controlling flow between the fan bypass duct and the heat exchanger system.


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