- 专利标题: NOZZLE, BURNER, COMBUSTOR, GAS TURBINE, AND GAS TURBINE SYSTEM
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申请号: US15115431申请日: 2015-03-12
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公开(公告)号: US20170130962A1公开(公告)日: 2017-05-11
- 发明人: Kei INOUE , Satoshi TAKIGUCHI , Shinji AKAMATSU , Kenta TANIGUCHI , Naoki ABE
- 申请人: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- 申请人地址: JP Kanagawa
- 专利权人: Mitsubishi Hitachi Power Systems, Ltd.
- 当前专利权人: Mitsubishi Hitachi Power Systems, Ltd.
- 当前专利权人地址: JP Kanagawa
- 优先权: JP2014-059127 20140320
- 国际申请: PCT/JP2015/057378 WO 20150312
- 主分类号: F23R3/16
- IPC分类号: F23R3/16 ; F23R3/28 ; F02C7/232
摘要:
A combustor (10) is provided with: a nozzle (25) having formed therein an air jet section (51) that causes air to be jetted from a nozzle section (25s); a cylindrical part (26) covering the nozzle (25) from the outer peripheral side thereof and forming an air flow path between the cylindrical part (26) and the nozzle (25); and a pressure loss section (27) provided to the air flow path, the pressure loss section (27) causing a loss of pressure in the air that flows through the air flow path. The nozzle (25) is provided with: at least one air inlet section (52) that takes in air from an outer peripheral surface that is an upstream side from the pressure loss section (27); and a flow path-forming section (50) forming a discharge air flow path (R2) that guides air that is taken in from the at least one air inlet section (52) to the air jet section (51).
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