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(A2) 申请公布日期 2015.12.16
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
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