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:
Nov. 15, 2016
Filed:
Aug. 06, 2013
Applicant:
Safran Power Uk Ltd., Buckinghamshire, GB;
Inventor:
Neil Dudley, Chelmsford, GB;
Assignee:
SAFRAN POWER UK LTD., Buckinghamshire, GB;
Primary Examiner:
Int. Cl.
CPC ...
F02N 11/00 (2006.01); H02P 9/04 (2006.01); F02N 11/08 (2006.01); F01D 19/00 (2006.01); H02P 27/04 (2016.01); H02P 1/46 (2006.01); H02P 1/52 (2006.01); H02P 6/20 (2016.01); F02C 7/268 (2006.01); H02K 23/52 (2006.01); H02P 9/08 (2006.01);
U.S. Cl.
CPC ...
F02N 11/0866 (2013.01); F01D 19/00 (2013.01); F02C 7/268 (2013.01); H02P 1/46 (2013.01); H02P 1/52 (2013.01); H02P 6/20 (2013.01); H02P 27/04 (2013.01); F02N 2011/0896 (2013.01); H02P 9/08 (2013.01); Y02T 50/671 (2013.01);
Abstract
An aircraft electrical apparatus includes an engine starter motor control unit configured to provide an AC input voltage to a transformer rectifier unit. The apparatus includes a transformer rectifier unit for supplying power to an aircraft DC supply bus. The engine starter motor control unit provides the AC input voltage to the transformer rectifier unit.