发明名称 HYBRID VENTURI COOLING SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide a venturi device for a turbine combustor. SOLUTION: The venturi device (42) includes a substantially annular outer liner (48); a substantially annular inner liner (46); a venturi channel (50) located between the substantially annular outer and inner liners (48 and 46); the substantially annular outer and inner liners (48 and 46) being substantially V-shaped in axial cross-section, thereby defining a throat region (60); the substantially annular outer liner (48) formed with an array of impingement cooling holes (76) and the substantially annular inner liner (46) formed with a plurality of vortex generators (78) facing the substantially annular outer liner (48). COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2011179495(A) 申请公布日期 2011.09.15
申请号 JP20110037747 申请日期 2011.02.24
申请人 GENERAL ELECTRIC CO 发明人 SHERSHNYOV BORYS;GINESSIN LEONID;KAMILEVICH ALMAZ VALEEV
分类号 F02C7/18;F23R3/42 主分类号 F02C7/18
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