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:
Apr. 03, 2018

Filed:

Dec. 17, 2012
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Paul Broughton, Leicester, GB;

Robin Charles Kennea, Nottingham, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H01B 7/00 (2006.01); H01B 7/17 (2006.01); H01B 7/282 (2006.01); H05K 1/00 (2006.01); H05K 1/18 (2006.01); F02C 7/32 (2006.01); F02C 7/00 (2006.01); H01R 12/78 (2011.01); H01R 12/61 (2011.01); H05K 1/14 (2006.01);
U.S. Cl.
CPC ...
H01B 7/0045 (2013.01); F02C 7/00 (2013.01); F02C 7/32 (2013.01); H01B 7/17 (2013.01); H01B 7/282 (2013.01); H05K 1/00 (2013.01); H05K 1/18 (2013.01); H01R 12/61 (2013.01); H01R 12/78 (2013.01); H05K 1/144 (2013.01); H05K 1/147 (2013.01); H05K 2201/058 (2013.01); H05K 2201/10295 (2013.01); Y02T 50/672 (2013.01);
Abstract

A gas turbine engineis provided with electrical harness raftscomprising electrical conductors embedded in a rigid composite material. The raftsare used to transport electrical signals (which may be, for example power and/or control signals) around a gas turbine engine. Raftsmay be connected together and to other components using flexible cables, that may help to accommodate relative movement of the rafts, for example through vibration. The raftsare lighter, more compact, and more convenient to handle than conventional electrical harnesses. The raftsmay provide a convenient and secure mounting surface for other components/systems of a gas turbine engine, such as EECs and/or fluid pipes.


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