发明授权
US08647066B2 Blade with non-axisymmetric platform: recess and boss on the extrados 有权
具有非轴对称平台的刀片:外壳上的凹槽和凸台

Blade with non-axisymmetric platform: recess and boss on the extrados
摘要:
A blade for a turbomachine impeller including an airfoil, and at least one platform at one of the ends of the airfoil, the blade configured to be arranged with a plurality of substantially identical blades so as to form a ring around a ring axis. In the blade, a suction surface profile at the surface of the platform and along the suction surface has a first recessed part located axially in an upstream half of the airfoil and a first boss-like part located axially downstream of the first recessed part. Due to this configuration, efficiency of the blade is improved.
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