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:
Oct. 08, 2019

Filed:

Apr. 15, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Daniel S. Rogers, Springvale, ME (US);

Jeremy Drake, South Berwick, ME (US);

Brian C. McLaughlin, Kennebunk, ME (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/28 (2006.01); F01D 11/08 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 25/28 (2013.01); F01D 11/08 (2013.01); F01D 25/24 (2013.01); F01D 25/246 (2013.01); F05D 2220/32 (2013.01); F05D 2230/64 (2013.01); F05D 2230/70 (2013.01); F05D 2230/72 (2013.01); F05D 2230/80 (2013.01); F05D 2240/11 (2013.01); F05D 2260/30 (2013.01);
Abstract

A retention member for a component of a gas turbine engine and methods of using the same are provided. The retention member includes an annular body having a first side, a second side, a first end, and a second end, a retention element configured at the first end of the annular body and on the first side, the retention element configured to releasably engage with an interior surface of a case of the gas turbine engine, and a support element configured at the second end of the annular body, the support element configured to engage with a surface of at least one of a blade outer air seal or a blade outer air seal support.


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