METHOD FOR MANUFACTURING TURBINE ROTOR BLADE

Title:

METHOD FOR MANUFACTURING TURBINE ROTOR BLADE

Document Type and Number:

WIPO Patent Application WO/2014/098151

Kind Code:

A1

Abstract:

The present invention addresses the problem of providing a method for manufacturing a turbine rotor blade wherein warping, bending and twisting of the entire rotor blade, which is provided with an excess thickness portion after a forging step, can be suppressed. In the forging step in a process for manufacturing a rotor blade (23), the forging is hot-forged such that the distance (the excess thickness amount) from the blade surface of the blade section (23) to the surface of the excess thickness section is substantially uniform along the entire periphery of a cross section of the blade section (23) and the excess thickness section (31) perpendicular to the blade length direction, and such that the amount of the excess thickness in the blade length direction, which is the thickness of the excess thickness section (31), gradually increases toward the blade tip from a prescribed position.

Inventors:

HATANO KOHEI (JP)
OYAMA HIROHARU (JP)
MACHIDA MOTONARI (JP)
HARAGUCHI HIDETAKA (JP)
ISHII KEN (JP)
KAMITANI KEISUKE (JP)
MATSUMURA TAKUMI (JP)
OTA TAKAHIRO (JP)

Application Number:

PCT/JP2013/083954

Publication Date:

June 26, 2014

Filing Date:

December 18, 2013

Export Citation:

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Assignee:

MITSUBISHI HEAVY IND LTD (JP)

International Classes:

F01D25/00; B21K3/04; F01D5/14

Foreign References:

JPS63112039A	1988-05-17
JP3531677B2	2004-05-31
JP3531677B2	2004-05-31

Other References: