发明名称 |
COOLING SYSTEMS FOR GAS TURBINE ENGINE COMPONENTS |
摘要 |
A transfer tube (110; 210) includes a conduit (108) with an inlet (106; 204) and an opposed outlet (104; 206). The transfer tube also includes a retention tab (230) extending from the inlet and a locking spring tab (240) extending from the outlet. The locking spring tab includes a claw portion (242) extending radially from the locking spring tab of the transfer tube. |
申请公布号 |
EP2955330(A3) |
申请公布日期 |
2016.04.20 |
申请号 |
EP20150167758 |
申请日期 |
2015.05.14 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DAVIS, TIMOTHY M.;DRAKE, JEREMY |
分类号 |
F01D9/06;F01D25/24;F16L21/02;F16L37/086 |
主分类号 |
F01D9/06 |
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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