发明名称 Combustor cooling hole pattern
摘要 A combustor assembly (10) includes an inner and outer liner (16,18) defining a combustion chamber (22). The inner and outer liners (16,18) include a plurality of cooling holes (36) spaced a specified distance apart. The cooling holes (36) include first, second and third groups (44,46,48). The first group (44) of cooling holes (36) is the most densely spaced, followed by the second group (46) and then the third group (48). The first group (44) of cooling holes (36) begin upstream of a leading edge (50) of a large opening (50) and terminates downstream of the leading edge (50). The increased density of cooling holes (36) adjacent the large openings (38) provide increased cooling airflow in areas where cooling may be affected by local disturbances in cooling airflow.
申请公布号 EP1705426(A1) 申请公布日期 2006.09.27
申请号 EP20060251068 申请日期 2006.02.28
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BURD, STEVEN W.;CHEUNG, ALBERT K.
分类号 F23R3/00;F23R3/06 主分类号 F23R3/00
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