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.

Date of Patent:
Apr. 14, 2020

Filed:

Jul. 30, 2014
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Timothy M. Davis, Kennebunk, ME (US);

Jeffrey Vincent Anastas, Kennebunk, ME (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16J 15/34 (2006.01); F02C 7/28 (2006.01); F01D 11/08 (2006.01); F01D 11/12 (2006.01); F01D 11/22 (2006.01); F01D 11/00 (2006.01); F16J 15/44 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F16J 15/3496 (2013.01); F01D 9/02 (2013.01); F01D 11/001 (2013.01); F01D 11/003 (2013.01); F01D 11/08 (2013.01); F01D 11/12 (2013.01); F01D 11/122 (2013.01); F01D 11/125 (2013.01); F01D 11/127 (2013.01); F01D 11/22 (2013.01); F02C 7/28 (2013.01); F16J 15/3464 (2013.01); F16J 15/444 (2013.01); F05D 2220/32 (2013.01); F05D 2240/55 (2013.01); F05D 2250/283 (2013.01);
Abstract

A seal assembly includes an annular carrier defining a radially inward face, and an opposed radially outward face defining a plurality of spline slots. The spline slots are configured and adapted to receive corresponding spline tabs to center the carrier in a surrounding structure. A honeycomb seal is mounted to the radially inward face of the carrier. The honeycomb seal is configured for sealing engagement with a knife-edge seal rotating relative to the honeycomb seal. The seal assembly has a relatively low coefficient of thermal expansion in comparison to the static component or the knife-edge seal. For example, a gas turbine engine can include a seal assembly as described above, wherein the carrier is mounted to a static component and a rotor mounted for rotation relative to the carrier, and wherein the rotor includes the knife edge seal component sealingly engaged to the honeycomb seal.


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