Invention Grant
US08092159B2 Feeding film cooling holes from seal slots 有权
从密封槽进料薄膜冷却孔

Feeding film cooling holes from seal slots
Abstract:
A cooling arrangement for a first stage nozzle of a turbine includes a slot formed in a forward face of the first stage nozzle, the slot opening in a direction facing a combustor transition piece and adapted to receive a flange portion of a seal extending between the first stage nozzle and the transition piece. The slot has a closed end formed with at least one cooling cavity provided with at least one cooling passageway extending between the cavity and an external surface of the first stage nozzle.
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