Invention Grant
US07766615B2 Local indented trailing edge heat transfer devices 有权
局部缩进后缘传热装置

Local indented trailing edge heat transfer devices
Abstract:
A turbine engine component has an airfoil portion having a pressure side and a suction side, a trailing edge discharge slot, and a suction side lip downstream of an exit of the trailing edge slot. The suction side lip is provided with negative features for increasing local heat transfer coefficient in the region of the suction side lip.
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