发明名称 Hybrid venturi cooling system
摘要 <p>A venturi device (42) for a turbine combustor 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; the substantially annular outer and inner liners being substantially V-shaped in axial cross-section, thereby defining a throat region (60); the substantially annular outer liner formed with an array of impingement holes (76) and the substantially annular inner liner formed with a plurality of vortex generators (78) facing the substantially annular outer liner. </p>
申请公布号 EP2363644(A3) 申请公布日期 2014.10.29
申请号 EP20110156488 申请日期 2011.03.01
申请人 GENERAL ELECTRIC COMPANY 发明人 SHERSHNYOV, BORYS;GINESSIN, LEONID;KAMILEVICH, ALMAZ VALEEV
分类号 F23R3/06 主分类号 F23R3/06
代理机构 代理人
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