发明名称 CONICAL-FLAT HEAT SHIELD FOR GAS TURBINE ENGINE COMBUSTOR DOME
摘要 A gas turbine engine combustor conical-flat heat shield includes an annular conical section extending upstream from and being integral with a flat section with a flat downstream facing surface which may be generally perpendicular to or canted with respect to a centerline. The flat section includes radially outer and inner edges at least one of which is circular and circumscribed about a centerline and circumferentially spaced apart clockwise and counter-clockwise radial edges having an origin on the centerline. A gas turbine engine combustor includes conical-flat heat shields in one or more circular rows arranged in a non-symmetrical or asymmetrical pattern. Two or more groups (A, B, C) of the conical-flat heat shields in the circular rows may be mounted on a domeplate and one or more of the conical-flat heat shields is different in one or more of the groups (A, B, C).
申请公布号 US2015377488(A1) 申请公布日期 2015.12.31
申请号 US201514750543 申请日期 2015.06.25
申请人 GENERAL ELECTRIC COMPANY 发明人 ELKADY Ahmed Mostafa;DANIS Allen Michael;ROBERSON Eric Matthew;MUELLER Mark Anthony;MOERTLE George;LI Shui-Chi
分类号 F23R3/00 主分类号 F23R3/00
代理机构 代理人
主权项 1. A conical-flat heat shield for a gas turbine engine combustor, the conical-flat heat shield comprising: an annular conical section extending upstream or forward from and being integral with a substantially annular flat section of the conical-flat heat shield, the flat section including radially outer and inner edges, at least one of the outer and inner edges being circular and circumscribed about a centerline, and the flat section including circumferentially spaced apart clockwise and counter-clockwise radial edges having an origin on the centerline.
地址 Schenectady NY US