发明名称 Sequential cooling insert for turbine stator vane
摘要 A sequential impingement cooling insert for a turbine stator vane that forms a double impingement for the pressure and suction sides of the vane or a triple impingement. The insert is formed from a sheet metal formed in a zigzag shape that forms a series of alternating impingement cooling channels with return air channels, where pressure side and suction side impingement cooling plates are secured over the zigzag shaped main piece. Another embodiment includes the insert formed from one or two blocks of material in which the impingement channels and return air channels are machined into each block.
申请公布号 US8684668(B1) 申请公布日期 2014.04.01
申请号 US201213685053 申请日期 2012.11.26
申请人 JONES RUSSELL B;KRUEGER JUDSON J;PLANK WILLIAM L;FLORIDA TURBINE TECHNOLOGIES, INC. 发明人 JONES RUSSELL B;KRUEGER JUDSON J;PLANK WILLIAM L
分类号 F01D9/04 主分类号 F01D9/04
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