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:
Aug. 08, 2017

Filed:

Dec. 17, 2012
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Paul Broughton, Leicester, GB;

Richard Peace, Derby, GB;

Gary Alan Skinner, Nottingham, GB;

Robin Charles Kennea, Nottingham, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/12 (2006.01); H05B 3/28 (2006.01); F02C 7/20 (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); F02C 7/32 (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 gas turbine enginecomprises at least one rigid raft assembly that has a fluid passagewayat least partially embedded therein. The fluid passagewayis at least a part of a fluid system. In addition to the fluid passageway, the rigid raft assemblyalso has at least a part of another system. For example, the rigid raft assembly may also include electrical conductors, which are part of an electrical system. The rigid raft assemblymay be lighter, easier to assemble, more robust and more compact than conventional solutions for providing systems to gas turbine engines.


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