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. 06, 2022

Filed:

Mar. 25, 2021
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Carson A. Roy Thill, South Berwick, ME (US);

Thomas E. Clark, Sanford, ME (US);

Danielle Mahoney, Dover, NH (US);

Andrew D. Keene, Portland, ME (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/02 (2006.01); F01D 11/08 (2006.01);
U.S. Cl.
CPC ...
F01D 11/02 (2013.01); F01D 11/08 (2013.01); F05D 2220/32 (2013.01); F05D 2240/55 (2013.01); F05D 2300/20 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A component for a gas turbine engine includes a component body formed of ceramic matrix composite lamina and has at least one hook. The at least one hook has an attachment region radially inward of the at least one hook. The attachment region is radially thinner from a hook end of the at least one hook to a remote end, and then becomes radially thicker. A slot is formed through a radial thickness of the at least one hook from the hook end in a remote direction, such that there are two sections of the attachment region. A gas turbine engine is also disclosed.


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