EP 2815083 A1 20141224 - COMPONENT FOR A THERMAL MACHINE, IN PARTICULAR A GAS TURBINE
Title (en)
COMPONENT FOR A THERMAL MACHINE, IN PARTICULAR A GAS TURBINE
Title (de)
BAUTEIL FÜR EINE THERMISCHE MASCHINE, INSBESONDERE EINE GASTURBINE
Title (fr)
ÉLÉMENT POUR UNE MACHINE THERMIQUE, EN PARTICULIER UNE TURBINE À GAZ
Publication
Application
Priority
- CH 2102012 A 20120217
- EP 2013053116 W 20130215
Abstract (en)
[origin: WO2013121016A1] The invention relates to a component for a thermal machine, in particular a gas turbine, said component having a corner and/or edge (22) subjected to a thermally high load. The cooling of the component is improved in a manner such that at least one cooling channel (25) is countersunk into the surface of the component in the immediate vicinity of the corner and/or edge (22) in order to cool the corner and/or edge (22).
IPC 8 full level
F01D 25/12 (2006.01)
CPC (source: EP US)
F01D 5/081 (2013.01 - US); F01D 5/085 (2013.01 - US); F01D 5/186 (2013.01 - US); F01D 5/187 (2013.01 - US); F01D 25/12 (2013.01 - EP US); F05D 2230/10 (2013.01 - EP US); F05D 2240/81 (2013.01 - EP US); F05D 2260/20 (2013.01 - US); F05D 2260/208 (2013.01 - US)
Citation (search report)
See references of WO 2013121016A1
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
Designated extension state (EPC)
BA ME
DOCDB simple family (publication)
WO 2013121016 A1 20130822; CH 706107 A1 20130830; CN 104114818 A 20141022; CN 104114818 B 20170623; EP 2815083 A1 20141224; EP 2815083 B1 20170628; JP 2015508141 A 20150316; US 2014334914 A1 20141113; US 9777577 B2 20171003
DOCDB simple family (application)
EP 2013053116 W 20130215; CH 2102012 A 20120217; CN 201380009850 A 20130215; EP 13704137 A 20130215; JP 2014557058 A 20130215; US 201414445346 A 20140729