发明名称 ARRANGEMENT FOR A GAS TURBINE COMBUSTION ENGINE
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).
申请公布号 WO2016057020(A1) 申请公布日期 2016.04.14
申请号 WO2014US59381 申请日期 2014.10.07
申请人 SIEMENS ENERGY, INC. 发明人 LITTLE, DAVID A.
分类号 F01D9/02 主分类号 F01D9/02
代理机构 代理人
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