发明名称 |
ANGLED COMBUSTOR LINER COOLING HOLES THROUGH TRANSVERSE STRUCTURE WITHIN A GAS TURBINE ENGINE COMBUSTOR |
摘要 |
A wall assembly for use in a combustor of a gas turbine engine includes a transverse structure with at least one effusion passage that extends at an angle a therethrough. The effusion passage includes an inlet in an outer periphery of a wall. A wall assembly within a gas turbine engine include a liner panel generally parallel to a support shell and a transverse structure with at least one effusion passage that extends at an angle a therethrough. The effusion passage includes an inlet in an outer periphery of a wall that is transverse to the liner panel and the support shell. |
申请公布号 |
EP3047127(A4) |
申请公布日期 |
2017.01.18 |
申请号 |
EP20140843603 |
申请日期 |
2014.09.16 |
申请人 |
United Technologies Corporation |
发明人 |
BOULDIN, Lee E.;MOURA, Dennis M.;EASTWOOD, Jonathan J.;PACHECO-TOUGAS, Monica |
分类号 |
F02C7/12;F02C7/18;F23M5/04;F23R3/00;F23R3/06;F23R3/42;F23R3/60 |
主分类号 |
F02C7/12 |
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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