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Patent Searching and Data


Title:
STATIONARY BLADE AND GAS TURBINE PROVIDED WITH SAME
Document Type and Number:
WIPO Patent Application WO/2017/026314
Kind Code:
A1
Abstract:
A shroud of a stationary blade (50) has formed therein a plurality of circumferential ejection passages (95) that connect with a cavity (69) into which cooling air (Ac) flows and that open on a circumferential end surface (63). Of a central region (91) in the circumferential end surface (63), an upstream-side region (92) in the circumferential end surface (63), and a downstream-side region (93) in the circumferential end surface (63), openings of the plurality of circumferential ejection passages (95) are formed in at least the central region (91). The density, being the number of openings of the circumferential ejection passages (95) per unit length in the axial direction (Da), is highest in the central region (91).

Inventors:
OTOMO HIROYUKI (JP)
HADA SATOSHI (JP)
Application Number:
PCT/JP2016/072500
Publication Date:
February 16, 2017
Filing Date:
August 01, 2016
Export Citation:
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Assignee:
MITSUBISHI HITACHI POWER SYS (JP)
International Classes:
F01D9/04; F01D11/00; F02C7/18
Domestic Patent References:
WO2011132217A12011-10-27
WO2012144242A12012-10-26
Foreign References:
JP5606648B12014-10-15
JP2004060638A2004-02-26
US5609466A1997-03-11
Other References:
See also references of EP 3336316A4
Attorney, Agent or Firm:
MORI Ryuichirou et al. (JP)
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