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Patent Searching and Data


Title:
FILM COOLING STRUCTURE, AND TURBINE BLADE FOR GAS TURBINE ENGINE
Document Type and Number:
WIPO Patent Application WO/2020/246494
Kind Code:
A1
Abstract:
This film cooling structure comprises a wall part 20, and a cooling hole 30 that is inclined such that an outlet 32 is located further rearward than an inlet 31. The cooling hole 30 includes a straight pipe part 30 and a diffuser part 34. The diffuser part 34 includes: a flat surface 37; a curved surface 38 that is curved rearward and, together with the flat surface 37, forms a semi-circular or semi-elliptical flow path cross-section larger than that of the straight pipe part 33; a first section 40 in which the area of the flow path cross-section increases toward the outlet 32 of the cooling hole 30; and a second section 41 that extends from the first section 40 to the outlet 32 of the cooling hole 30, and in which the area of the flow path cross-section increases, toward the outlet of the cooling hole, at a rate of increase smaller than that of the first section 40 or in which the area of the flow path cross-section is constant. The width of the diffuser part 34 has a value at least twice the depth of the diffuser part 34.

Inventors:
IKEHARA RYO (JP)
FUJIMOTO SHU (JP)
OKITA YOJI (JP)
KUBO SEIJI (JP)
HATTORI HITOSHI (JP)
Application Number:
PCT/JP2020/021896
Publication Date:
December 10, 2020
Filing Date:
June 03, 2020
Export Citation:
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Assignee:
IHI CORP (JP)
International Classes:
F01D9/02; F01D5/18; F02C7/18
Foreign References:
JP2000087701A2000-03-28
JP2000064806A2000-02-29
JP2017198199A2017-11-02
JPS56449B11981-01-08
JP2013124612A2013-06-24
Other References:
See also references of EP 3981954A4
Attorney, Agent or Firm:
MIYOSHI Hidekazu et al. (JP)
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