Invention Grant
US08192168B2 Airfoil shape for a compressor blade 有权
用于压缩机叶片的翼型

Airfoil shape for a compressor blade
Abstract:
An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE A. X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances can be joined smoothly with one another to form a complete airfoil shape.
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