Global Patent Index - EP 3412867 A1

EP 3412867 A1 20181212 - COOLED GAS TURBINE BLADE

Title (en)

COOLED GAS TURBINE BLADE

Title (de)

GEKÜHLTE GASTURBINENSCHAUFEL

Title (fr)

AUBE REFROIDIE DE TURBINE À GAZ

Publication

EP 3412867 A1 20181212 (EN)

Application

EP 17174866 A 20170607

Priority

EP 17174866 A 20170607

Abstract (en)

A blade for a gas turbine (5) is provided with an airfoil (18) having a leading edge (27), a trailing edge (28), a pressure side (24) and a suction side (25); the airfoil (18) comprising an outer wall (30) and an inner wall (31) substantially enclosed by the outer wall (30); and with a cooling arrangement (29) which comprises a suction side cooling path (31a) defined at least partially along the suction side (25) between the outer wall (30) and the inner wall (31); the suction side cooling path (31a) having at least one suction side inlet (40) and at least one suction side discharge arrangement (41); the suction side inlet (40) being arranged closer to the trailing edge (28) than the suction side discharge arrangement (41).

IPC 8 full level

F01D 5/18 (2006.01)

CPC (source: CN EP)

F01D 5/186 (2013.01 - CN); F01D 5/187 (2013.01 - EP); F01D 5/186 (2013.01 - EP); F05D 2260/22141 (2013.01 - EP)

Citation (applicant)

Citation (search report)

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)

EP 3412867 A1 20181212; EP 3412867 B1 20240103; EP 3412867 B8 20240214; CN 108999646 A 20181214

DOCDB simple family (application)

EP 17174866 A 20170607; CN 201810580811 A 20180607