EP 2394026 A2 20111214 - GAS TURBINE BLADE FOR A TURBOMACHINE
Title (en)
GAS TURBINE BLADE FOR A TURBOMACHINE
Title (de)
GASTURBINENSCHAUFEL FÜR EINE STRÖMUNGSMASCHINE
Title (fr)
AUBE DE TURBINE À GAZ POUR TURBOMACHINE
Publication
Application
Priority
- DE 2010001334 W 20101112
- DE 102009052881 A 20091113
Abstract (en)
[origin: WO2011057622A2] The invention relates to a gas turbine blade (10), in particular a compressor blade and/or turbine blade, for a turbomachine, wherein the gas turbine blade (10) comprises at least one receptacle (18) for arranging a connecting element in a form-closed manner, by means of which connecting element a mechanical load can be applied to the gas turbine blade (10). The invention further relates to an shrouding band segment (16) for arrangement on a gas turbine blade (10), a connection system having a gas turbine blade (10) and having a connecting element, a method for connecting a gas turbine blade (10) to a connecting element, and a rotor for a turbomachine having a rotor disk (12) joined to a blade ring or having a rotor ring joined to a blade ring.
IPC 8 full level
CPC (source: EP US)
F01D 5/225 (2013.01 - EP US); F01D 5/34 (2013.01 - EP US); F05D 2250/183 (2013.01 - EP US); F05D 2260/36 (2013.01 - EP US)
Citation (search report)
See references of WO 2011057622A2
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 RS SE SI SK SM TR
DOCDB simple family (publication)
WO 2011057622 A2 20110519; WO 2011057622 A3 20111013; DE 102009052881 A1 20110526; EP 2394026 A2 20111214; EP 2394026 B1 20130717; US 2012230825 A1 20120913; US 8622704 B2 20140107
DOCDB simple family (application)
DE 2010001334 W 20101112; DE 102009052881 A 20091113; EP 10798489 A 20101112; US 201013508875 A 20101112