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 9814101 B1

PDFFull Text
Date of Patent:
Nov. 07, 2017

Filed:

Dec. 09, 2013

Heated rigid electrical harness for a gas turbine engine

Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Paul Broughton, Leicester, GB;

Michael Christopher Willmot, Sheffield, GB;

Justin Sean Dalton, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:

Oliff PLC

Primary Examiner:

Steven Sutherland

Assistant Examiner:

Eric Linderman

Int. Cl.
CPC ...
F02C 7/12 (2006.01); F02C 7/20 (2006.01); F02C 7/32 (2006.01); H05B 3/28 (2006.01); B23P 6/00 (2006.01); H02G 3/04 (2006.01); H01R 12/00 (2006.01); H02G 3/32 (2006.01); B60R 16/02 (2006.01); B64C 3/34 (2006.01); F02C 7/141 (2006.01); B60R 16/08 (2006.01); F02C 7/16 (2006.01); H01R 12/57 (2011.01); H01R 12/59 (2011.01); H01R 12/51 (2011.01); H01R 12/61 (2011.01); H02G 3/00 (2006.01); B60R 16/00 (2006.01); B64D 29/08 (2006.01); F02C 7/00 (2006.01); H02G 1/00 (2006.01); H02G 3/02 (2006.01); F02C 7/047 (2006.01); F02C 7/224 (2006.01); F24H 1/10 (2006.01); H05B 1/02 (2006.01); H05K 7/20 (2006.01);
U.S. Cl.
CPC ...
H05B 3/28 (2013.01); B23P 6/005 (2013.01); B60R 16/00 (2013.01); B60R 16/02 (2013.01); B60R 16/0207 (2013.01); B60R 16/0215 (2013.01); B60R 16/08 (2013.01); B64C 3/34 (2013.01); B64D 29/08 (2013.01); F02C 7/00 (2013.01); F02C 7/047 (2013.01); F02C 7/12 (2013.01); F02C 7/141 (2013.01); F02C 7/16 (2013.01); F02C 7/20 (2013.01); F02C 7/224 (2013.01); F02C 7/32 (2013.01); F24H 1/105 (2013.01); H01R 12/00 (2013.01); H01R 12/51 (2013.01); H01R 12/515 (2013.01); H01R 12/57 (2013.01); H01R 12/59 (2013.01); H01R 12/592 (2013.01); H01R 12/61 (2013.01); H02G 1/00 (2013.01); H02G 3/00 (2013.01); H02G 3/02 (2013.01); H02G 3/04 (2013.01); H02G 3/32 (2013.01); H05B 1/0236 (2013.01); H05K 7/20 (2013.01); F05D 2260/30 (2013.01); Y02T 50/672 (2013.01); Y10T 29/49002 (2015.01); Y10T 29/49117 (2015.01); Y10T 29/49234 (2015.01); Y10T 29/49236 (2015.01); Y10T 29/49238 (2015.01); Y10T 156/10 (2015.01);
Abstract

A rigid electrical raft has electrical conductors embedded in a rigid material. The electrical conductors transmit electrical signals through the rigid electrical raft, which may form part of an electrical system of a gas turbine engine. The rigid electrical raft also has electrical heating elements embedded therein. The electrical heating elements provide heat which may be used, for example, to prevent condensation and/or ice build-up and/or to raise the temperature of electrical components to be within a desired range.

Find Patent Forward Citations

Broughton, Paul. (2017). Heated rigid electrical harness for a gas turbine engine (U.S. Patent No. 9814101). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9814101

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

Loading…