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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 9297314 B1

PDFFull Text
Date of Patent:
Mar. 29, 2016

Filed:

Dec. 19, 2012

Gas turbine engine with accessory gear box

Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Thomas G. Cloft, Glastonbury, CT (US);

Robert L. Gukeisen, Middletown, CT (US);

Claude Mercier, South Windsor, CT (US);

Assignee:

United Technologies Corporation, Hartford, CT (US);

Attorney:

Carlson, Gaskey & Olds, PC

Primary Examiner:

Phutthiwat Wongwian

Assistant Examiner:

Alain Chau

Int. Cl.
CPC ...
F02C 7/32 (2006.01); F02C 7/36 (2006.01); F01D 25/28 (2006.01); F01D 25/20 (2006.01); F02C 7/268 (2006.01); F02C 7/275 (2006.01); F01D 25/24 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); F01D 25/28 (2013.01); F02C 7/36 (2013.01); F01D 25/20 (2013.01); F01D 25/24 (2013.01); F02C 7/268 (2013.01); F02C 7/275 (2013.01); F02K 3/06 (2013.01); Y02T 50/671 (2013.01);
Abstract

A nacelle for incorporation into a gas turbine engine has an inner wall defining a bypass duct, and an outer wall. At least one drive shaft extends through the inner wall. The at least one drive shaft is connected to a gas turbine engine receiving the nacelle. The at least one drive shaft is connected to drive at least two accessory gear boxes, with the at least two accessory gear boxes being received between the inner and outer walls of the nacelle. A gas turbine engine is also disclosed.

Find Patent Forward Citations

Cloft, Thomas. (2016). Gas turbine engine with accessory gear box (U.S. Patent No. 9297314). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9297314

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

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