发明名称 GAS TURBINE ENGINE COMBUSTOR WITH INTEGRATED COMBUSTOR VANE
摘要 A combustor section for a gas turbine engine includes a combustor vane which extends at least partially into a combustion chamber.
申请公布号 US2014338336(A1) 申请公布日期 2014.11.20
申请号 US201213627722 申请日期 2012.09.26
申请人 Cunha Frank J.;Erbas-Sen Nurhak 发明人 Cunha Frank J.;Erbas-Sen Nurhak
分类号 F23R3/28 主分类号 F23R3/28
代理机构 代理人
主权项 1. A combustor section for a gas turbine engine comprising: a combustion chamber; and a combustor vane which extends at least partially into said combustion chamber.
地址 Avon CT US