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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 10337334 B1

PDFFull Text
Date of Patent:
Jul. 02, 2019

Filed:

Dec. 07, 2015

Gas turbine engine component with a baffle insert

Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Brandon W. Spangler, Vernon, CT (US);

Atul Kohli, Tolland, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:

Cantor Colburn LLP

Primary Examiner:

Kayla Mccaffrey

Int. Cl.
CPC ...
F01D 5/18 (2006.01); F23R 3/00 (2006.01); F23R 3/04 (2006.01); F01D 9/02 (2006.01); F01D 11/08 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
F01D 5/188 (2013.01); F01D 9/02 (2013.01); F01D 11/08 (2013.01); F01D 25/12 (2013.01); F23R 3/002 (2013.01); F23R 3/04 (2013.01); F05D 2220/32 (2013.01); F05D 2240/126 (2013.01); F05D 2240/127 (2013.01); F05D 2240/35 (2013.01); F05D 2250/14 (2013.01); F05D 2250/25 (2013.01); F05D 2260/2212 (2013.01); F05D 2260/22141 (2013.01); F05D 2260/232 (2013.01);
Abstract

A component of a gas turbine engine, the component having: an internal cooling cavity extending through an interior of the component; a baffle insert configured to be inserted into the internal cooling cavity; a plurality of trip strips extending upwardly from an exterior surface of the baffle insert; and at least one rib extending upwardly from the exterior surface of the baffle insert, wherein the plurality of trip strips and the at least one rib are spaced from an interior surface of the internal cooling cavity.

Find Patent Forward Citations

Spangler, Brandon. (2019). Gas turbine engine component with a baffle insert (U.S. Patent No. 10337334). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10337334

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

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