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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.

Patent No.:

US 9145213 B1

PDFFull Text
Date of Patent:
Sep. 29, 2015

Filed:

Dec. 18, 2013

Gas turbine engine configuration interface

Applicant:

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

Inventors:

Joseph D. Myer, Avon, IN (US);

Steven W. Tomlinson, Brownsburg, IN (US);

Assignee:

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

Attorneys:

Fishman Stewart Yamaguchi PLLC

Douglas P. LaLone

Primary Examiner:

Thomas G Black

Assistant Examiner:

Tyler Paige

Int. Cl.
CPC ...
G01C 23/00 (2006.01); B63H 11/00 (2006.01); B64D 31/06 (2006.01); F02C 9/48 (2006.01); B64D 31/00 (2006.01); B64D 27/10 (2006.01); F02C 6/20 (2006.01); F02C 7/12 (2006.01); F02C 9/00 (2006.01); F02C 9/26 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64D 27/10 (2013.01); B64D 31/00 (2013.01); F02C 6/20 (2013.01); F02C 7/12 (2013.01); F02C 9/00 (2013.01); F02C 9/26 (2013.01); F02C 9/48 (2013.01); F05D 2220/323 (2013.01); F05D 2270/051 (2013.01); F05D 2270/07 (2013.01); F05D 2270/20 (2013.01);
Abstract

A gas turbine engine is disclosed which is capable of being reconfigured for one operating mode to another. A display is provided that permits a pilot or other operator to select between engine modes. One aspect is the ability to provide variable cooling that can be controlled by various devices. The variable cooling features can be used with devices such as cooled turbine components like vanes and/or blades. Devices can be used to reconfigure the performance and/or operability of a gas turbine engine.

Find Patent Forward Citations

Myer, Joseph. (2015). Gas turbine engine configuration interface (U.S. Patent No. 9145213). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9145213

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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