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:
Jun. 25, 2019

Filed:

Jul. 18, 2014
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Matthew Budnick, Hudson, NH (US);

Conway Chuong, Manchester, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2006.01); F02C 7/28 (2006.01); F01D 25/24 (2006.01); F01D 15/10 (2006.01);
U.S. Cl.
CPC ...
F01D 11/005 (2013.01); F01D 11/001 (2013.01); F01D 15/10 (2013.01); F01D 25/24 (2013.01); F02C 7/28 (2013.01); F05D 2220/30 (2013.01); F05D 2220/76 (2013.01); F05D 2240/55 (2013.01);
Abstract

A gas turbine engine includes an engine static structure. A fairing is supported relative to the engine static structure and configured to provide a flow path surface of a flow path extending in an axial direction. A seal plate has first and second ends radially spaced from one another with respect to the axial direction. The first end is operatively secured to the engine static structure. The second end is configured to seal relative to the fairing. The seal plate includes a portion between the first and second ends that extends substantially in the axial direction and configured to permit the second end to move away from the fairing in the axial direction relative to the first end in response to thermal growth.


Find Patent Forward Citations

Loading…