logo

For the Inventor, By the Inventor

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 10634061 B1

PDFFull Text
Date of Patent:
Apr. 28, 2020

Filed:

Feb. 04, 2015

Gas turbine engine accessory architecture

Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Ryan K. Snyder, Glastonbury, CT (US);

Eric J. Heims, Avon, CT (US);

Mark W. Colebrook, Glastonbury, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:

Carlson, Gaskey & Olds, P.C.

Primary Examiner:

Craig Kim

Int. Cl.
CPC ...
F02C 7/32 (2006.01); F02C 7/14 (2006.01); F01D 25/28 (2006.01); F01D 25/20 (2006.01); F01D 25/26 (2006.01); F02K 3/06 (2006.01); B64C 7/02 (2006.01); B64D 29/06 (2006.01); B64D 27/10 (2006.01); B64D 29/08 (2006.01); F02C 3/04 (2006.01); H02K 7/18 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); B64C 7/02 (2013.01); B64D 27/10 (2013.01); B64D 29/06 (2013.01); B64D 29/08 (2013.01); F01D 25/20 (2013.01); F01D 25/265 (2013.01); F01D 25/28 (2013.01); F02C 3/04 (2013.01); F02C 7/14 (2013.01); F02K 3/06 (2013.01); H02K 7/1823 (2013.01); F05D 2220/327 (2013.01); F05D 2230/72 (2013.01); F05D 2250/30 (2013.01); F05D 2250/411 (2013.01); Y02T 50/671 (2013.01);
Abstract

A gas turbine engine comprises a compressor, a combustor and a turbine. A housing for the gas turbine engine includes a mount member to define a vertically upper location. Sides of the engine are defined on opposed sides of the mount, with a fuel filter, a fuel pump and a fuel flow meter being positioned on a first side and an oil pump, an oil filter and an oil tank positioned on a second of the sides.

Find Patent Forward Citations

Quick Actions:

Snyder, Ryan. (2020). Gas turbine engine accessory architecture (U.S. Patent No. 10634061). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10634061

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

Loading…