EP 2725194 B1 20200219 - Turbine rotor blade of a gas turbine
Title (en)
Turbine rotor blade of a gas turbine
Title (de)
Turbinenrotorschaufel einer Gasturbine
Title (fr)
Aube de rotor d'une turbine à gaz
Publication
Application
Priority
- GB 201219267 A 20121026
- DE 102012021400 A 20121031
Abstract (en)
[origin: EP2725194A1] The turbine blade has a root portion, a platform and an aerofoil that is mounted on platform and is formed by a pressure side wall and a suction side wall and has an outer surface. The pressure side wall and suction side wall meet at a leading edge and a trailing edge. The suction side wall defines portion of radially outward surface of aerofoil and overhang at aerofoil tip that has maximum overhang length that is between 5% and 20% of axial chord length of blade and is located between 15% and 40% of suction surface length from leading edge. An independent claim is included for a rotor stage of turbine.
IPC 8 full level
F01D 5/20 (2006.01)
CPC (source: EP US)
F01D 5/141 (2013.01 - US); F01D 5/20 (2013.01 - EP US); F01D 11/08 (2013.01 - US); F05D 2240/307 (2013.01 - US)
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)
EP 2725194 A1 20140430; EP 2725194 B1 20200219; EP 2725195 A1 20140430; EP 2725195 B1 20190925; US 10641107 B2 20200505; US 2014119920 A1 20140501; US 2014119942 A1 20140501; US 9593584 B2 20170314
DOCDB simple family (application)
EP 13190022 A 20131024; EP 13190039 A 20131024; US 201314061971 A 20131024; US 201314062230 A 20131024