EP 1705339 B1 20161130 - Rotor shaft, in particular for a gas turbine
Title (en)
Rotor shaft, in particular for a gas turbine
Title (de)
Rotorwelle, insbesondere für eine Gasturbine
Title (fr)
Arbre de rotor, particulièrement pour une turbine à gaz
Publication
Application
Priority
CH 5042005 A 20050323
Abstract (en)
[origin: EP1705339A2] Cooling air channels (14) are formed within the turbine section (12) of a drive shaft (10) and between turbine disks (13) around the turbine section. Each of the cooling air channels radiates outward from a cavity (15) around the cooling air supply channel (16) within the drive shaft and is of an elliptical cross-section. The major and minor axes of each cooling air channel runs perpendicular and parallel to the drive shaft axis, respectively.
IPC 8 full level
F01D 5/08 (2006.01)
CPC (source: EP US)
F01D 5/081 (2013.01 - EP US); F05D 2250/14 (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)
EP 1705339 A2 20060927; EP 1705339 A3 20131106; EP 1705339 B1 20161130; US 2007086884 A1 20070419; US 7329086 B2 20080212
DOCDB simple family (application)
EP 06110741 A 20060307; US 38649706 A 20060322