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:
Sep. 01, 2026

Filed:

Sep. 27, 2024
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Russell Stratton, Toronto, CA;

Paul Weaver, Chateauguay, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/44 (2006.01); B64D 33/04 (2006.01); F02K 1/00 (2006.01); F02K 1/06 (2006.01); F02K 1/10 (2006.01);
U.S. Cl.
CPC ...
F02K 1/44 (2013.01); B64D 33/04 (2013.01); B64D 33/06 (2013.01); F02K 1/002 (2013.01); F02K 1/06 (2013.01); F02K 1/10 (2013.01);
Abstract

An aircraft powerplant includes a core of a gas turbine engine and an exhaust section. The core includes a core flowpath, a compressor section, a combustor section and a turbine section. The core flowpath extends longitudinally through the compressor section, the combustor section and the turbine section. The exhaust section includes an exhaust flowpath and a flow diverter. The flow diverter includes a diverter panel configured to pivot between a first position and a second position. The flow diverter is configured to fluidly couple the diffuser section to the first nozzle section and fluidly decouple the diffuser section from the second nozzle section when the diverter panel is in the first position. The flow diverter is configured to fluidly couple the diffuser section to the second nozzle section and fluidly decouple the diffuser section from the first nozzle section when the diverter panel is in the second position.


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