发明名称 COMBUSTOR FOR A GAS TURBINE ENGINE
摘要 In an embodiment of the invention, a dual-wall casing for a combustor comprises an outer wall and an inner wall defining a channel therebetween. The walls are fastened together by a bolt which extends from the inner wall and across the channel. In use, the inner wall is exposed to combustion products. Cooling is provided by a primary inlet hole extending through the outer wall and arranged upstream (with respect to the direction of flow of coolant in the channel) of the bolt and an array of effusion holes extending through the inner wall and positioned with their inlet in line of sight of the primary inlet hole. The primary inlet hole is sized with respect to the array of effusion holes such that it has a flow area which causes locally negligible flow restriction.
申请公布号 US2017108219(A1) 申请公布日期 2017.04.20
申请号 US201615273243 申请日期 2016.09.22
申请人 ROLLS-ROYCE plc 发明人 RIMMER John E. T.;BROWN Nicholas M.
分类号 F23R3/00 主分类号 F23R3/00
代理机构 代理人
主权项 1. A dual-wall component configured for use in a high temperature environment, the component comprising; an outer wall and an inner wall defining a channel therebetween, the inner wall, in use, exposed to the high temperature, a primary inlet hole extending through the outer wall, an array of effusion holes extending through the inner wall and positioned with their entire inlet in direct line of sight of the primary inlet hole, the primary inlet hole sized with respect to the array of effusion holes such that it has a flow area which causes locally negligible flow restriction.
地址 London GB