Title:
熱的なターボ機械
Document Type and Number:
Japanese Patent JP2006522894
Kind Code:
A
Abstract:
A thermal turbomachine is disclosed having at least one row of rotor blades. At least one first rotor blade has a greater radial length than the others and at the blade tip is equipped with a first abrasive layer. At least one rotor blade which has a shorter radial length than the first rotor blade is equipped with a second abrasive layer at the blade tip. The first abrasive layer has a better cutting capacity and a lower thermal stability than the second abrasive layer. During commissioning of the thermal turbomachine, the first abrasive layer is in contact with the abradable layer of the stator, and during continuous operation of the thermal turbomachine the second abrasive layer is in contact with the abradable layer of the stator.
More Like This:
Inventors:
Nicholas Campino Johnson
Matthias Hebel
Jonas Hooter
Christoph Niederberger
Matthias Hebel
Jonas Hooter
Christoph Niederberger
Application Number:
JP2006505554A
Publication Date:
October 05, 2006
Filing Date:
April 13, 2004
Export Citation:
Assignee:
ALSTOM Technology Ltd
International Classes:
F01D5/20; F01D11/08; F01D21/04
Attorney, Agent or Firm:
Toshio Yano
Toshiomi Yamazaki
Takuya Kuno
Einzel Felix-Reinhard
Toshiomi Yamazaki
Takuya Kuno
Einzel Felix-Reinhard