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. 29, 2019

Filed:

Jun. 17, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Colin J. Kling, Glastonbury, CT (US);

Darin S. Lussier, Guilford, CT (US);

James F. O'Brien, Glastonbury, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/52 (2006.01); F04D 29/66 (2006.01); F04D 29/02 (2006.01); B29C 70/72 (2006.01); B29C 70/02 (2006.01); F01D 21/04 (2006.01); F01D 5/28 (2006.01); F01D 25/24 (2006.01); B29C 70/86 (2006.01); B29C 70/88 (2006.01);
U.S. Cl.
CPC ...
F04D 29/526 (2013.01); B29C 70/023 (2013.01); B29C 70/72 (2013.01); B29C 70/86 (2013.01); B29C 70/885 (2013.01); F01D 5/282 (2013.01); F01D 21/045 (2013.01); F01D 25/24 (2013.01); F04D 29/023 (2013.01); F04D 29/664 (2013.01); F05D 2300/224 (2013.01); F05D 2300/603 (2013.01); F05D 2300/701 (2013.01); Y02T 50/672 (2013.01);
Abstract

A method of fabricating a fan case for a gas turbine engine defines a metallic ring including an outer surface and an inner surface. A first composite material is assembled about the outer surface of the metallic ring. A second composite material is assembled about the first composite material. The first composite material and the second material are cured about the metallic ring within a tool to form a first subassembly. The first subassembly is removed from the tool. A fan case assembly for a gas turbine engine and a gas turbine engine are also disclosed.


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