发明申请
US20090317234A1 CROSSFLOW TURBINE AIRFOIL 有权
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CROSSFLOW TURBINE AIRFOIL
摘要:
A turbine airfoil includes pressure and suction sidewalls extending axially in chord between opposite leading and trailing edges. The sidewalls are spaced transversely apart to define flow channels extending longitudinally and separated chordally by partitions bridging the sidewalls. A perforate partition includes a row of crossover holes extending obliquely therethrough.
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