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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 10641287 B1

PDFFull Text
Date of Patent:
May. 05, 2020

Filed:

Sep. 06, 2016

Fan containment case for a gas turbine engine

Applicant:

Rolls-royce Corporation, Indianapolis, IN (US);

Inventors:

Matthew J. Kappes, Greenwood, IN (US);

Robert W. Heeter, Noblesville, IN (US);

Benedict N. Hodgson, Indianapolis, IN (US);

Assignee:

Rolls-Royce Corporation, Indianapolis, IN (US);

Attorney:

McCracken & Gillen LLC

Primary Examiner:

Justin D Seabe

Assistant Examiner:

Cameron A Corday

Int. Cl.
CPC ...
F04D 29/52 (2006.01); F01D 21/04 (2006.01); F04D 29/32 (2006.01); F04D 29/16 (2006.01); F02K 3/06 (2006.01); F04D 19/00 (2006.01);
U.S. Cl.
CPC ...
F04D 29/526 (2013.01); F01D 21/04 (2013.01); F02K 3/06 (2013.01); F04D 19/002 (2013.01); F04D 29/164 (2013.01); F04D 29/324 (2013.01); F05D 2220/32 (2013.01); F05D 2300/224 (2013.01); F05D 2300/603 (2013.01); Y02T 50/672 (2013.01);
Abstract

According to one aspect, a fan containment case for a gas turbine engine is provided which includes a barrel having a first band of material on an outside of the barrel. The first band is made of carbon fiber composite. The barrel further includes a second band of material inboard of the fan case and made of poly p-phenylene-2,6-benzobisoxazole (PBO) composite. The barrel also includes a third band of material made of carbon fiber composite inboard of the second band.

Find Patent Forward Citations

Kappes, Matthew. (2020). Fan containment case for a gas turbine engine (U.S. Patent No. 10641287). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10641287

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

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