EP 1828616 A1 20070905 - METHOD FOR IMPROVING THE FLOW STABILITY OF A TURBO COMPRESSOR
Title (en)
METHOD FOR IMPROVING THE FLOW STABILITY OF A TURBO COMPRESSOR
Title (de)
VERFAHREN ZUR MODIFIZIERUNG EINES TURBOKOMPRESSORS
Title (fr)
MÉTHODE D' AMÉLIORATION DE LA STABILITÉ DE COURANT D' UNE TURBOMACHINE
Publication
Application
Priority
- EP 2005056294 W 20051129
- EP 04106808 A 20041221
- EP 05815881 A 20051129
Abstract (en)
[origin: EP1674734A1] The method is for the individual modifying of a turbocompressor for the purpose of adapting to specific framework conditions during operation, whereby blades (232) installed in a blade ring are installed by their roots (231) in a circumferentially extending slot in the rotor shaft or casing. In an axial blade cascade of the compressor the number of blades installed in a blade ring can be increased. At least one distance piece (24) installed in the circumferential direction (U) between two blade roots can be removed and at least one additional blade fitted. Independent claims are included for the following: (A) a rotor of a turbocompressor with at least blade row which can be modified in accordance with the proposed method; (B) a stator of a turbocompressor with at least blade row which can be modified in accordance with the proposed method; (C) a turbocompressor comprising at least one rotor or stator according to the invention; and (D) a gas turbine unit including a turbocompressor with at least one modifiable rotor or stator according to the invention.
IPC 8 full level
F04D 29/66 (2006.01); F01D 5/30 (2006.01); F04D 29/32 (2006.01); F04D 29/54 (2006.01)
CPC (source: EP US)
F04D 29/541 (2013.01 - EP US)
Citation (search report)
See references of WO 2006067025A1
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 1674734 A1 20060628; EP 1828616 A1 20070905; EP 1828616 B1 20141001; US 2008003098 A1 20080103; WO 2006067025 A1 20060629
DOCDB simple family (application)
EP 04106808 A 20041221; EP 05815881 A 20051129; EP 2005056294 W 20051129; US 81202907 A 20070614