EP 2092163 A1 20090826 - VANE ASSEMBLY CONFIGURED FOR TURNING A FLOW IN A GAS TURBINE ENGINE, A STATOR COMPONENT COMPRISING THE VANE ASSEMBLY, A GAS TURBINE AND AN AIRCRAFT JET ENGINE
Title (en)
VANE ASSEMBLY CONFIGURED FOR TURNING A FLOW IN A GAS TURBINE ENGINE, A STATOR COMPONENT COMPRISING THE VANE ASSEMBLY, A GAS TURBINE AND AN AIRCRAFT JET ENGINE
Title (de)
LEITSCHAUFELANORDNUNG, DIE ZUM DREHEN EINES STROMS IN EINEM GASTURBINENTRIEBWERK KONFIGURIERT IST, STATORKOMPONENTE MIT DER LEITSCHAUFELANORDNUNG, GASTURBINE UND FLUGZEUGSTRAHLTRIEBWERK
Title (fr)
ENSEMBLE D'AUBES CONFIGURÉES POUR FAIRE TOURNER UN ÉCOULEMENT DANS UN MOTEUR DE TURBINE À GAZ, UN COMPOSANT DE STATOR COMPRENANT L'ENSEMBLE D'AUBES, UNE TURBINE À GAZ ET UN MOTEUR À RÉACTION D'AVION
Publication
Application
Priority
SE 2006001292 W 20061114
Abstract (en)
[origin: WO2008060195A1] The invention relates to a vane assembly configured for turning a flow in a gas turbine engine comprising a stationary main guide vane (208) and an additional guide vane (210), wherein a leading edge (318) of the additional guide vane (210) is positioned upstream of a leading edge (310) of the main guide vane (208) and wherein the additional guide vane (210) extends a distance along the main guide vane (208) towards a trailing edge (312) of the main guide vane (208) forming a passageway (322) between the additional guide vane (210) and the main guide vane (208).
IPC 8 full level
CPC (source: EP US)
F01D 5/146 (2013.01 - EP US); F01D 9/041 (2013.01 - EP US); F01D 9/065 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US)
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 LV MC NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
WO 2008060195 A1 20080522; EP 2092163 A1 20090826; EP 2092163 A4 20130417; US 2010158684 A1 20100624
DOCDB simple family (application)
SE 2006001292 W 20061114; EP 06813013 A 20061114; US 51480009 A 20091201