- 专利标题: Arrangement for a gas turbine combustion engine
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申请号: US15509987申请日: 2014-10-07
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公开(公告)号: US10132175B2公开(公告)日: 2018-11-20
- 发明人: David A. Little
- 申请人: Siemens Energy, Inc.
- 申请人地址: US FL Orlando
- 专利权人: SIEMENS ENERGY, INC.
- 当前专利权人: SIEMENS ENERGY, INC.
- 当前专利权人地址: US FL Orlando
- 国际申请: PCT/US2014/059381 WO 20141007
- 国际公布: WO2016/057020 WO 20160414
- 主分类号: F01D9/02
- IPC分类号: F01D9/02 ; F23R3/42 ; F23R3/46 ; F02C7/12
摘要:
An arrangement (10) for delivering gases from combustors (15) to a first row of blades. The arrangement (10) includes at least an upstream flow path (60) including an aft first side wall (64) and a downstream flow path (62) including a forward second side wall (66). A convergence junction trailing edge (40) is defined at a downstream terminal edge (41) of the first side wall (64), and the second side wall (66) converges toward the first side wall (64) in the direction of the convergence junction trailing edge (40). An impingement sheet structure (78) is located between and provides impingement cooling air to the first and second side walls (64, 66). Openings (88) provide a cooling air passage between the first and second side walls (64, 66) and provide a flow of post impingement air into the gas path at the convergence junction trailing edge (40).
公开/授权文献
- US20180230835A1 ARRANGEMENT FOR A GAS TURBINE COMBUSTION ENGINE 公开/授权日:2018-08-16
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