EP 1690011 A1 20060816 - ROTOR FOR A COMPRESSOR
Title (en)
ROTOR FOR A COMPRESSOR
Title (de)
ROTOR FÜR EINEN VERDICHTER
Title (fr)
ROTOR POUR UN COMPRESSEUR
Publication
Application
Priority
- EP 2004053114 W 20041126
- DE 10357134 A 20031206
Abstract (en)
[origin: WO2005054682A1] The invention relates to a rotor (20) for a compressor, in particular a gas turbine, comprising a plurality of moving blades (25), which are arranged in the form of a ring about the rotation axis of the rotor (20) and which are each maintained in a peripheral turned groove (21) on the rotor (21) by means of a blade root (26), whereby a widening lower part (27) of said blade root (26) engages behind two shoulders (24), formed on the lateral walls of said turned groove (21). The aim of said invention is to extend the lifetime of such a rotor. Said aim is achieved, whereby the depth (T) of the turned groove (21) is substantially greater than a minimal groove depth (Tmin), a strength of rotor (20), which is sufficient for start-up, being thus obtained in the area of the blade mounting, according to the predetermined material characteristics of the rotor (20) and operating conditions of the compressor.
IPC 8 full level
F04D 29/32 (2006.01); F01D 5/30 (2006.01)
CPC (source: EP US)
F01D 5/3038 (2013.01 - EP US); F04D 29/322 (2013.01 - EP US); F05D 2250/29 (2013.01 - EP US); F05D 2250/291 (2013.01 - EP US)
Citation (search report)
See references of WO 2005054682A1
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LU MC NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
WO 2005054682 A1 20050616; CA 2548642 A1 20050616; CA 2548642 C 20110419; DE 10357134 A1 20050630; EP 1690011 A1 20060816; EP 1690011 B1 20170426; EP 1690011 B8 20170802; US 2006228216 A1 20061012; US 7513747 B2 20090407
DOCDB simple family (application)
EP 2004053114 W 20041126; CA 2548642 A 20041126; DE 10357134 A 20031206; EP 04804578 A 20041126; US 41903106 A 20060518