发明名称 ADDITIVE MANUFACTURED GAS TURBINE ENGINE COMBUSTOR LINER PANEL
摘要 A combustor of a gas turbine engine includes an additively manufactured liner panel with a heat transfer augmentation feature.
申请公布号 US2016033129(A1) 申请公布日期 2016.02.04
申请号 US201414775290 申请日期 2014.03.14
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Burd Steven W.
分类号 F23R3/00;B23P15/00;F02C7/18 主分类号 F23R3/00
代理机构 代理人
主权项 1. A combustor of a gas turbine engine comprising: an additively manufactured liner panel.
地址 Hartford CT US