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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.

Patent No.:

US 10415592 B1

PDFFull Text
Date of Patent:
Sep. 17, 2019

Filed:

Oct. 21, 2016

Shroud for gas turbine engine

Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Colin G. Amadon, Kennebunk, ME (US);

Kevin C. Eckland, Kennebunk, ME (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:

Cantor Colburn LLP

Primary Examiner:

Igor Kershteyn

Int. Cl.
CPC ...
F04D 29/54 (2006.01); F02C 3/04 (2006.01); F04D 29/08 (2006.01); F04D 29/64 (2006.01); F01D 9/04 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F04D 29/542 (2013.01); F01D 9/042 (2013.01); F02C 3/04 (2013.01); F04D 29/083 (2013.01); F04D 29/644 (2013.01); F02K 3/06 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2240/35 (2013.01); F05D 2240/80 (2013.01); F05D 2260/30 (2013.01); F05D 2300/431 (2013.01); Y02T 50/671 (2013.01);
Abstract

A stator assembly for a stator of a gas turbine engine is provided. The stator assembly having: a shroud defining a cavity; a plurality of inserts located within the cavity, each of the plurality of inserts defining a cavity; a plurality of vanes secured to the shroud, wherein each of the plurality of vanes has a tab portion located in the cavity of the shroud; and a rubber material disposed in the cavity of the shroud, the rubber material securing the tab portion of each of the plurality of vanes to the shroud.

Find Patent Forward Citations

Amadon, Colin. (2019). Shroud for gas turbine engine (U.S. Patent No. 10415592). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10415592

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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