Invention Grant
- Patent Title: Gas turbine blade with cooling passages
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Application No.: US14893677Application Date: 2015-06-05
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Publication No.: US09644485B2Publication Date: 2017-05-09
- Inventor: Hiroyuki Otomo , Masamitsu Kuwabara
- Applicant: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- Applicant Address: JP Kanagawa
- Assignee: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- Current Assignee: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- Current Assignee Address: JP Kanagawa
- Agency: Wenderoth, Lind & Ponack, L.L.P.
- Priority: JP2014-132866 20140627
- International Application: PCT/JP2015/066367 WO 20150605
- International Announcement: WO2015/198840 WO 20151230
- Main IPC: F01D25/12
- IPC: F01D25/12 ; F01D5/30 ; F01D5/18 ; F01D5/02 ; F02C7/18 ; F02C3/04

Abstract:
A blade is formed with blade air passages connecting the inside of a blade body of the blade and the inside of a platform of the blade. The platform is formed with pressure side passages that extend from the blade air passages toward a circumferential pressure side, are open at a pressure side end face, and are arranged in an axial direction. Further, the platform is formed with a suction side main passage into which cooling air flows, and a suction side passage that communicates with the suction side main passage and extends from the suction side main passage along a suction side end face.
Public/Granted literature
- US20160177751A1 BLADE AND GAS TURBINE PROVIDED WITH THE SAME Public/Granted day:2016-06-23
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