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:
Mar. 02, 2021

Filed:

Apr. 15, 2015
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Allison Zywiak, Durham, CT (US);

Graham R. Philbrick, Vernon, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F01D 11/12 (2006.01); F01D 11/00 (2006.01); F02C 7/28 (2006.01); F16J 15/34 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); F01D 11/001 (2013.01); F01D 11/12 (2013.01); F01D 11/122 (2013.01); F01D 11/127 (2013.01); F02C 7/28 (2013.01); F16J 15/34 (2013.01); F05D 2220/32 (2013.01); F05D 2240/55 (2013.01);
Abstract

The present disclosure relates to gas turbine engine and seal configurations, and components for a gas turbine engine. In one embodiment, a seal for a gas turbine engine includes a rotary seal element, the rotary seal element configured to rotate during operation of a gas turbine engine, and a stationary seal element having an annular seal surface. The stationary seal element includes a first area of the annular seal surface configured to engage with the rotary seal element, and the stationary seal element includes a second area of the annular seal surface configured to provide reduced resistance to the rotary seal element during a flight windmilling event.


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