Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
ELECTRICAL APPARATUS
Document Type and Number:
WIPO Patent Application WO/2014/023726
Kind Code:
A3
Abstract:
An aircraft electrical apparatus comprises an engine starter motor control unit (1) configured to provide an AC input voltage to a transformer rectifier unit (2). Preferably, the apparatus comprises a transformer rectifier unit (2) for supplying power to an aircraft DC supply bus (4), wherein the engine starter motor control unit (1) provides the AC input voltage to the transformer rectifier unit (2).

Inventors:
DUDLEY NEIL (GB)
Application Number:
PCT/EP2013/066472
Publication Date:
April 10, 2014
Filing Date:
August 06, 2013
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
SAFRAN POWER UK LTD (GB)
International Classes:
F02C7/266; F01D19/00; F02N11/08; H02M3/22; H02P1/16; H02P1/46; H02P1/52; H02P6/20; H02P9/08; H02P27/04
Foreign References:
EP0377328A21990-07-11
EP0605780A21994-07-13
US20040080164A12004-04-29
US6128204A2000-10-03
Attorney, Agent or Firm:
REGIMBEAU (Paris Cedex 17, Paris Cedex 17, FR)
Download PDF:
View/Download PDF      PDF Help



 
Previous Patent: HOUSING FOR A BATTERY CELL WITH A HOUSING COVER HAVING A MONITORING ELECTRONICS UNIT, BATTERY CELL, ...

Next Patent: METHOD AND APPARATUS PROVIDING INTER-TRANSMISSION POINT PHASE RELATIONSHIP FEEDBACK FOR JOINT TRANSM...