Global Patent Index - EP 2083148 A3

EP 2083148 A3 20120606 - Gas turbine with a compressor with run-in coating and method of lapping the free extremities of compressor blades in a gas turbine

Title (en)

Gas turbine with a compressor with run-in coating and method of lapping the free extremities of compressor blades in a gas turbine

Title (de)

Gasturbine mit einem Verdichter mit Einlaufschicht und Verfahren zum Einlaufen von freien Endbereichen von Schaufeln eines Verdichters einer Gasturbine

Title (fr)

Turbine à gaz dotée d'un compresseur muni d'un revêtement de rodage et procédé de rodage des extrémités libres des aubes d'un compresseur de turbine à gaz

Publication

EP 2083148 A3 20120606 (DE)

Application

EP 09000952 A 20090123

Priority

  • DE 102008005482 A 20080123
  • DE 102008005480 A 20080123
  • DE 102008005479 A 20080123

Abstract (en)

[origin: EP2083148A2] The gas turbine has a compressor with a set of blades, where the blades are provided with a free end in each case. An adjacent intake layer (6) is formed on the free end of the blade at a circular housing area. The intake layer is connected with a fluid supplying device (9) and is provided with liquid passage opening. An independent claim is included for a method for running free end area of blades of a compressor of a gas turbine.

IPC 8 full level

F01D 11/08 (2006.01); F01D 11/10 (2006.01)

CPC (source: EP US)

F01D 11/10 (2013.01 - EP US); F01D 11/122 (2013.01 - EP US); F04D 27/0238 (2013.01 - EP US); F04D 29/164 (2013.01 - EP US); F05D 2300/222 (2013.01 - EP US); F05D 2300/50 (2013.01 - EP US)

Citation (search report)

Designated contracting state (EPC)

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 TR

Designated extension state (EPC)

AL BA RS

DOCDB simple family (publication)

EP 2083148 A2 20090729; EP 2083148 A3 20120606; US 2009196730 A1 20090806; US 8257016 B2 20120904

DOCDB simple family (application)

EP 09000952 A 20090123; US 32036809 A 20090123