发明申请
US20080056909A1 Multi-peripheral serpentine microcircuits for high aspect ratio blades 有权
用于高纵横比刀片的多外围蛇形微电路

Multi-peripheral serpentine microcircuits for high aspect ratio blades
摘要:
A cooling arrangement for a pressure side of an airfoil portion of a turbine engine component is provided. The cooling arrangement comprises a pair of cooling circuits embedded within a wall forming the pressure side. The pair of cooling circuits includes a first serpentine cooling circuit and a second circuit offset from the first serpentine cooling circuit.
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