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:
Aug. 09, 2022

Filed:

Mar. 31, 2020
Applicants:

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

Rolls-royce Corporation, Indianapolis, IN (US);

Inventors:

David L. Sutterfield, Greenwood, IN (US);

Todd S. Taylor, Bargersville, IN (US);

Jack D. Petty, Indianapolis, IN (US);

Andrew Sanderson, Indianapolis, IN (US);

Bryan H. Lerg, Carmel, IN (US);

Assignees:

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

Rolls-Royce Corporation, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/08 (2006.01); F02K 1/34 (2006.01); F02K 1/70 (2006.01); F02K 1/04 (2006.01); F02K 1/62 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
F02K 1/34 (2013.01); F02K 1/04 (2013.01); F02K 1/08 (2013.01); F02K 1/62 (2013.01); F02K 1/70 (2013.01); F02K 1/763 (2013.01); F05D 2260/96 (2013.01);
Abstract

A propulsion unit includes a gas turbine engine arranged along an axis and an exhaust system coupled to the gas turbine engine. The gas turbine engine includes an engine core configured to discharge a core flow and a fan configured to be driven by the engine core to discharge a bypass flow. The exhaust system receives the mixed bypass and core flows from the gas turbine engine.


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