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发明名称
GAS TURBINE ENGINE COMBUSTOR LINER
摘要
<p>A liner for a combustor of a turbine engine includes a cooling feature which projects from a backside and an effusion hole that communicates through the liner</p>
申请公布号
EP2904236(A2)
申请公布日期
2015.08.12
申请号
EP20130843296
申请日期
2013.10.04
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
BANGERTER, JAMES, P.;WILLIAMS, ALEXANDER, W.;MULE, NICHOLAS;PACHECO-TOUGAS, MONICA
分类号
F23R3/06;F23R3/10;F23R3/50
主分类号
F23R3/06
代理机构
代理人
主权项
地址
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