发明申请
- 专利标题: GAS TURBINE
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申请号: US15327442申请日: 2015-08-19
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公开(公告)号: US20180209282A1公开(公告)日: 2018-07-26
- 发明人: Yasuro SAKAMOTO , Satoshi MIZUKAMI , Keisuke MATSUYAMA , Satoshi TANIMURA , Masanori YURI , Shunsuke TORII , Hiroaki KISHIDA
- 申请人: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- 优先权: JP2014-166922 20140819
- 国际申请: PCT/JP2015/073256 WO 20150819
- 主分类号: F01D9/02
- IPC分类号: F01D9/02 ; F23R3/46 ; F01D9/04 ; F01D25/12
摘要:
A gas turbine combustor and a gas turbine; wherein inclined surfaces are provided on inner surfaces of side walls neighboring in a circumferential direction at downstream end portions of transition pieces of combustors, the inclined surfaces being configured to increase a passage area of the transition pieces, a ratio (S/P) is from 0 to 0.2, where (P) is a pitch dimension of first stage vanes, and (S) is a circumferential dimension from an intermediate point between neighboring transition pieces to an upstream end of a first stage vane closest in the circumferential direction; and a ratio (L/P) is from 0.3 to 0.55, where (P) is the pitch dimension, and (L) is an axial dimension from a downstream end of the transition piece to the upstream end of the first stage vane.