发明名称 |
CONDUCTIVE PANEL SURFACE COOLING AUGMENTATION FOR GAS TURBINE ENGINE COMBUSTOR |
摘要 |
A liner panel for use in a combustor of a gas turbine engine includes a substrate with a hot side and a cold side; a bond coat on at least one of the hot side and the cold side of the substrate; and a convective feature on the cold side of the substrate of a material different than a material of the substrate. A wall assembly for use in a combustor of a gas turbine engine includes a shell with a multiple of impingement flow passages; and a liner panel mounted to the shell, where the panel includes a convective feature which faces the shell. A method of cooling a liner panel for a combustor section of a gas turbine engine includes directing an impingement flow towards a convective feature of a liner panel; and directing an effusion flow though the liner panel. |
申请公布号 |
WO2015047472(A2) |
申请公布日期 |
2015.04.02 |
申请号 |
WO2014US42284 |
申请日期 |
2014.06.13 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DRAKE, CHRISTOPHER;KOSTKA, JR., STANISLAV |
分类号 |
F23M5/00;F02C7/12;F23M5/08;F23R3/42 |
主分类号 |
F23M5/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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