EP 1654442 A1 20060510 - AIRCRAFT ENGINE
Title (en)
AIRCRAFT ENGINE
Title (de)
FLUGTRIEBWERK
Title (fr)
GROUPE MOTOPROPULSEUR
Publication
Application
Priority
- DE 2005000750 W 20050423
- DE 102004023569 A 20040513
Abstract (en)
[origin: WO2005111381A1] The invention relates to an aircraft engine, particularly a gas turbine engine, comprising at least one fan (11) and a central engine (12). The fan (11) is provided with a fan housing (13) that defines a fan duct and at least one fan wheel (15) while the central engine (12) is provided with at least one compressor (15, 16), at least one combustion chamber (17), and at least one turbine (18, 19). The inventive aircraft engine further comprises at least one generator (24) for producing electrical power, the or each generator (24) producing electrical power from shaft power tapped from the central engine (12). According to the invention, in order to produce electrical power, the or each generator (24) is integrated in a strut (21) which extends in a radial direction of the fan duct and is thus placed within the fan duct.
IPC 1-7
IPC 8 full level
F01D 15/10 (2006.01); F02K 3/06 (2006.01)
CPC (source: EP US)
F01D 15/10 (2013.01 - EP US); F02K 3/06 (2013.01 - EP US); F05D 2220/36 (2013.01 - EP US); F05D 2220/76 (2013.01 - EP US); F05D 2260/20 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US)
Citation (search report)
See references of WO 2005111381A1
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
WO 2005111381 A1 20051124; DE 102004023569 A1 20051208; EP 1654442 A1 20060510; US 2007157597 A1 20070712
DOCDB simple family (application)
DE 2005000750 W 20050423; DE 102004023569 A 20040513; EP 05748042 A 20050423; US 58734605 A 20050423