Invention Grant
US07524163B2 Nozzle guide vanes 有权
喷嘴导叶

Nozzle guide vanes
Abstract:
A turbine nozzle guide vane 10 with passages 28 leading from a hollow core 32 to respective seal strip slots 20, to deliver cooling air to abutment faces 18 on each end of the vane 10.
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