EP 1697623 A1 20060906 - GAS TURBINE, IN PARTICULAR AIRCRAFT ENGINE AND METHOD FOR GENERATING ELECTRICAL ENERGY IN A GAS TURBINE
Title (en)
GAS TURBINE, IN PARTICULAR AIRCRAFT ENGINE AND METHOD FOR GENERATING ELECTRICAL ENERGY IN A GAS TURBINE
Title (de)
GASTURBINE, INSBESONDERE FLUGTRIEBWERK, UND VERFAHREN ZUR ERZEUGUNG ELEKTRISCHER ENERGIE BEI EINER GASTURBINE
Title (fr)
TURBINE A GAZ, NOTAMMENT GROUPE MOTOPROPULSEUR, ET PROCEDE POUR PRODUIRE DE L'ENERGIE ELECTRIQUE DANS UNE TURBINE A GAZ
Publication
Application
Priority
- DE 2004002444 W 20041105
- DE 10355917 A 20031129
Abstract (en)
[origin: WO2005054645A1] The invention relates to a gas turbine, in particular an aircraft engine and to a method for generating electrical energy in a gas turbine. The gas turbine comprises at least one engine core (18), in which a shaft (19) produces a shaft output. The inventive turbine is equipped with means that generate electrical energy both from the shaft output produced by the engine core (18) and from the compressed air that is dissipated by the engine core (18).
IPC 8 full level
F02C 7/32 (2006.01); B64D 13/06 (2006.01); F01D 15/10 (2006.01); F02C 6/08 (2006.01); F02C 7/277 (2006.01); F02C 7/36 (2006.01); F04D 27/02 (2006.01)
CPC (source: EP US)
B64D 13/06 (2013.01 - EP US); F02C 6/08 (2013.01 - EP US); F02C 7/277 (2013.01 - EP US); F02C 7/32 (2013.01 - EP US); F02C 7/36 (2013.01 - EP US); F04D 27/0207 (2013.01 - EP US); B64D 2013/0644 (2013.01 - EP US); F05D 2220/323 (2013.01 - EP US); F05D 2220/76 (2013.01 - EP US); F05D 2260/4031 (2013.01 - EP US); Y02T 50/50 (2013.01 - EP US)
Citation (search report)
See references of WO 2005054645A1
Designated contracting state (EPC)
DE FR GB SE
DOCDB simple family (publication)
WO 2005054645 A1 20050616; DE 10355917 A1 20050630; EP 1697623 A1 20060906; US 2007089420 A1 20070426; US 7584600 B2 20090908
DOCDB simple family (application)
DE 2004002444 W 20041105; DE 10355917 A 20031129; EP 04819575 A 20041105; US 58074304 A 20041105