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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 10774685 B1

PDFFull Text
Date of Patent:
Sep. 15, 2020

Filed:

Apr. 30, 2018

Gas turbine engine exhaust component

Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Jonathan Jeffery Eastwood, West Hartford, CT (US);

Adam Lee Hart, Stuart, FL (US);

Brian Craig, Palm Beach Gardens, FL (US);

Luis Miguel Ayalde, Weston, FL (US);

Brian Levy, Sunny Isles Beach, FL (US);

Assignee:

RATHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:

Carlson, Gaskey & Olds, P.C.

Primary Examiner:

Gerald L Sung

Assistant Examiner:

Marc J Amar

Int. Cl.
CPC ...
F01D 25/24 (2006.01); F01D 9/04 (2006.01); F02C 3/04 (2006.01); F02K 1/52 (2006.01); F02K 1/44 (2006.01); F02K 1/40 (2006.01); B64D 33/04 (2006.01); F01D 25/30 (2006.01);
U.S. Cl.
CPC ...
F01D 25/243 (2013.01); B64D 33/04 (2013.01); F01D 9/04 (2013.01); F01D 25/246 (2013.01); F02C 3/04 (2013.01); F02K 1/40 (2013.01); F02K 1/44 (2013.01); F02K 1/52 (2013.01); F01D 25/30 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2240/15 (2013.01);
Abstract

A heat shield for a gas turbine engine includes a radial heat shield flange that extends in a circumferential direction and forms a ring. A plurality of bosses extend from a first axial side of the radial heat shield flange. There is a plurality of guide pins. One of the plurality of guide pins extends from a corresponding one of the plurality of bosses.

Find Patent Forward Citations

Eastwood, Jonathan. (2020). Gas turbine engine exhaust component (U.S. Patent No. 10774685). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10774685

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

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