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:
Dec. 10, 2019

Filed:

Mar. 17, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventor:

Edward Torres, Middletown, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 17/16 (2006.01); F01D 9/04 (2006.01); F04D 29/54 (2006.01); F04D 29/32 (2006.01); F02C 9/20 (2006.01);
U.S. Cl.
CPC ...
F01D 9/042 (2013.01); F01D 17/162 (2013.01); F02C 9/20 (2013.01); F04D 29/323 (2013.01); F04D 29/54 (2013.01); F05D 2220/32 (2013.01); F05D 2220/3217 (2013.01); F05D 2240/12 (2013.01); F05D 2240/14 (2013.01); F05D 2250/181 (2013.01); F05D 2250/182 (2013.01); F05D 2260/31 (2013.01);
Abstract

A vane retainer for a gas turbine engine includes a retainer body, an inner surface of the retainer body to engage complimentary threads of a mating component, and a plurality of castellations located at an end of the retainer body for engagement with complementary installation tool features during installation of the vane retainer to the mating component. A gas turbine engine includes a combustor and a plurality of vane assemblies in fluid communication with the combustor. Each vane assembly includes a vane having an airfoil portion and a vane stem extending from the airfoil portion. The vane stem is inserted into a bushing. A vane retainer is engaged with the bushing and includes a retainer body, an inner surface of the retainer body to engage complimentary threads of the bushing, and a plurality of castellations located at an end of the retainer body for engagement with complementary installation tool features.


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