logo

For the Inventor, By the Inventor

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 9988923 B1

PDFFull Text
Date of Patent:
Jun. 05, 2018

Filed:

Aug. 29, 2014

Seal for gas turbine engine

Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Brooks E. Snyder, Glastonbury, CT (US);

Thomas N. Slavens, Vernon, CT (US);

Mosheshe Camara-Khary Blake, Manchester, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Hartford, CT (US);

Attorney:

Carlson, Gaskey & Olds, P.C.

Primary Examiner:

Woody Lee, Jr

Assistant Examiner:

Maxime Adjagbe

Int. Cl.
CPC ...
F01D 5/22 (2006.01); F01D 11/20 (2006.01); F01D 9/04 (2006.01); F01D 11/00 (2006.01); F01D 5/12 (2006.01); F01D 25/24 (2006.01); F16J 15/08 (2006.01);
U.S. Cl.
CPC ...
F01D 11/20 (2013.01); F01D 5/12 (2013.01); F01D 5/22 (2013.01); F01D 9/04 (2013.01); F01D 9/041 (2013.01); F01D 11/005 (2013.01); F01D 11/008 (2013.01); F01D 25/24 (2013.01); F16J 15/0887 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2240/11 (2013.01); F05D 2240/57 (2013.01); F05D 2250/71 (2013.01); F05D 2250/75 (2013.01); F05D 2270/303 (2013.01); F05D 2270/306 (2013.01);
Abstract

One exemplary embodiment of this disclosure relates to a gas turbine engine including a first engine component and a second engine component. The first engine component has a mate face adjacent a mate face of the second engine component. The engine further includes a seal between the mate face of the first engine component and the mate face of the second engine component. The seal establishes three points of contact with each mate face in at least one condition.

Find Patent Forward Citations

Quick Actions:

Snyder, Brooks. (2018). Seal for gas turbine engine (U.S. Patent No. 9988923). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9988923

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

Loading…