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:
Feb. 18, 2020

Filed:

Oct. 23, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventor:

Steven M. O'Flarity, Glastonbury, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/04 (2006.01); F02K 1/80 (2006.01); F02K 3/077 (2006.01); F02K 3/10 (2006.01); F02C 3/107 (2006.01); F02C 3/04 (2006.01); F02C 7/36 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
F02K 3/04 (2013.01); F02C 3/04 (2013.01); F02C 3/107 (2013.01); F02C 7/36 (2013.01); F02K 1/80 (2013.01); F02K 3/077 (2013.01); F02K 3/10 (2013.01); B64D 2033/026 (2013.01); F05D 2240/40 (2013.01); F05D 2260/4031 (2013.01);
Abstract

A method of operating a gas turbine engine includes generating a flow of combustion products from a gas turbine generator that has a gas generator axis of rotation. A duct is oriented in a first position to direct the flow of combustion products that have passed over at least one gas generator turbine rotor through a fan drive turbine in response to a first desired flight condition. An axis of rotation of the fan drive turbine is transverse to a gas generator axis of rotation. The duct is oriented in a second position to direct the flow of combustion products that have passed over at least one gas generator turbine rotor through an augmentor section in response to a second desired flight condition.


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