EP 2462320 A2 20120613 - BLADE
Title (en)
BLADE
Title (de)
SCHAUFELBLATT
Title (fr)
AUBE
Publication
Application
Priority
- DE 102009036406 A 20090806
- DE 2010000920 W 20100805
Abstract (en)
[origin: WO2011015193A2] The present invention relates to a blade of a turbomachine, in particular an adjustable guide blade of a gas turbine, comprising at least one thickened area (18) on a pressure side (D) of the blade profile (P), wherein the thickened area (18) is arranged in a radially outer, housing-side area of the blade (10), wherein the thickened area (18) is designed at a distance from a front edge (12) and a rear edge (14) of the blade (10).
IPC 8 full level
F01D 5/14 (2006.01)
CPC (source: EP US)
F01D 5/141 (2013.01 - EP US); F01D 5/145 (2013.01 - EP US); F01D 5/20 (2013.01 - EP US); F01D 17/162 (2013.01 - EP US); F04D 29/544 (2013.01 - EP US); F04D 29/563 (2013.01 - EP US); F04D 29/681 (2013.01 - EP US); F05D 2250/711 (2013.01 - EP US); F05D 2250/713 (2013.01 - EP US)
Citation (search report)
See references of WO 2011015193A2
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 SE SI SK SM TR
DOCDB simple family (publication)
DE 102009036406 A1 20110210; CN 102472111 A 20120523; CN 102472111 B 20170301; EP 2462320 A2 20120613; EP 2462320 B1 20161012; US 2012128480 A1 20120524; US 9011081 B2 20150421; WO 2011015193 A2 20110210; WO 2011015193 A3 20110915
DOCDB simple family (application)
DE 102009036406 A 20090806; CN 201080034389 A 20100805; DE 2010000920 W 20100805; EP 10754675 A 20100805; US 201013388367 A 20100805