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.:
Date of Patent:
Jul. 18, 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); F02C 7/20 (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); 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
The present invention provides a gas turbine engine part which has a primary purpose in the engine which is structural and/or aerodynamic. The part is formed of rigid composite material, and has an electrical system comprising electrical conductors permanently embedded in the composite material. This provides advantages in terms of weight, complexity, and build time.