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Patent Searching and Data


Title:
TURBINE BLADE AND GAS TURBINE
Document Type and Number:
WIPO Patent Application WO/2019/003590
Kind Code:
A1
Abstract:
This turbine blade comprises: a blade part which has a hollow part extending along a blade height direction, and in which is formed a plurality of film-cooling holes aligned along the blade height direction; and an insert which is provided inside the hollow part along the blade height direction, and in which a plurality of impingement cooling holes is formed. The insert includes a high-density opening area in which the opening density of the impingement cooling holes is higher than in the rest of the surface area of the insert, a shape center of the high-density opening area is positioned on a negative-pressure-surface side of the blade part in the front edge-rear edge direction, the shape center of the high-density opening area is positioned farther radially outward than a center position of the blade part in the blade height direction, and the plurality of film-cooling holes include a plurality of upstream-side film-cooling holes provided in a position corresponding to the high-density opening area or toward the front edge side from said position on the negative pressure surface of the blade part.

Inventors:
FUJII TAKASHI (JP)
KOYABU HIDEMICHI (JP)
TORII SHUNSUKE (JP)
HADA SATOSHI (JP)
Application Number:
PCT/JP2018/015832
Publication Date:
January 03, 2019
Filing Date:
April 17, 2018
Export Citation:
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Assignee:
MITSUBISHI HITACHI POWER SYS (JP)
International Classes:
F01D9/02; F01D5/18; F02C7/18
Foreign References:
JP2001317302A2001-11-16
EP3054113A12016-08-10
JPH0392504A1991-04-17
JP2007239756A2007-09-20
JP2017089633A2017-05-25
Attorney, Agent or Firm:
SEISHIN IP PATENT FIRM, P.C. (JP)
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