EP 2440852 A1 20120418 - DRIVE FOR A TURBINE AND DRIVE METHOD
Title (en)
DRIVE FOR A TURBINE AND DRIVE METHOD
Title (de)
ANTRIEB FÜR EINE TURBINE NEBST ANTRIEBSVERFAHREN
Title (fr)
ENTRAÎNEMENT POUR UNE TURBINE ET PROCÉDÉ D'ENTRAÎNEMENT
Publication
Application
Priority
- EP 2010058050 W 20100609
- DE 102009026881 A 20090610
Abstract (en)
[origin: WO2010142709A1] The invention relates to a drive for a turbine, in particular an aircraft turbine, and a method for operating such a turbine. According to the invention, a drive for a turbine is provided with a compressor (1) for compressing air, a nozzle (14) for injecting a first fuel into the compressed air, and a combustion chamber (16) for igniting the air-fuel mixture. The drive also comprises a further nozzle (7) for injecting a second fuel. The nozzle for injecting a first fuel is used to start the drive. Therefore, the first fuel is a conventional fuel, in particular kerosene. The second nozzle is used to inject a novel fuel, which at least initially is a liquefied gas. In particular, a mixture and bio-LNG having a high calorific value is used as the liquefied gas.
IPC 8 full level
CPC (source: EP US)
F02C 7/22 (2013.01 - US); F23R 3/32 (2013.01 - EP US); F23R 3/343 (2013.01 - EP US)
Citation (search report)
See references of WO 2010142709A1
Citation (examination)
US 2004118121 A1 20040624 - PARKMAN KENNETH [CA], et al
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR
DOCDB simple family (publication)
WO 2010142709 A1 20101216; DE 102009026881 A1 20101216; EP 2440852 A1 20120418; US 2013199199 A1 20130808
DOCDB simple family (application)
EP 2010058050 W 20100609; DE 102009026881 A 20090610; EP 10722135 A 20100609; US 201013518439 A 20100609