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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 10648668 B1

PDFFull Text
Date of Patent:
May. 12, 2020

Filed:

Jun. 18, 2014

Gas turbine engine ceramic component assembly and bonding material

Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Grant O. Cook, III, Tolland, CT (US);

Michael G. Abbott, Jupiter, FL (US);

Michael G. McCaffrey, Windsor, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:

Carlson, Gaskey & Olds, P.C.

Primary Examiner:

Alain Chau

Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23R 3/60 (2006.01); C09J 5/00 (2006.01); F01D 25/24 (2006.01); F01D 11/08 (2006.01); F01D 5/28 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F23R 3/007 (2013.01); C09J 5/00 (2013.01); F01D 5/284 (2013.01); F01D 9/02 (2013.01); F01D 11/08 (2013.01); F01D 25/246 (2013.01); F23R 3/002 (2013.01); F23R 3/60 (2013.01); C09J 2400/123 (2013.01); C09J 2400/163 (2013.01); F05D 2230/236 (2013.01); F05D 2230/642 (2013.01); F05D 2240/11 (2013.01); F05D 2300/50212 (2013.01); F23R 2900/00005 (2013.01); F23R 2900/00017 (2013.01); Y02T 50/672 (2013.01);
Abstract

A gas turbine engine component assembly includes a ceramic component having a first thermal characteristic. A metallic component has a second thermal characteristic. A bonding material secures the ceramic component to the metallic component. The bonding material includes at least one of a transient liquid phase bond and a partial transient liquid phase bond. The bonding material is configured to withstand a shear stress parameter relating to a differential between the first and second thermal characteristics.

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Quick Actions:

Cook, III, Grant. (2020). Gas turbine engine ceramic component assembly and bonding material (U.S. Patent No. 10648668). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10648668

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

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