发明名称 Combustor cooling hole pattern
摘要 A combustor assembly includes an inner and outer liner defining a combustion chamber. The inner and outer liners include a plurality of cooling holes spaced a specified distance apart. The cooling holes include first, second and third groups. The first group of cooling holes is the most densely spaced, followed by the second group and then the third group. The first group of cooling holes begin upstream of a leading edge of a large opening and terminates downstream of the leading edge. The increased density of cooling holes adjacent the large openings provide increased cooling airflow in areas where cooling may be affected by local disturbances in cooling airflow.
申请公布号 US2006196188(A1) 申请公布日期 2006.09.07
申请号 US20050069095 申请日期 2005.03.01
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BURD STEVEN W.;CHEUNG ALBERT K.
分类号 F23R3/04 主分类号 F23R3/04
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