发明名称 BLADE FOR AXIAL COMPRESSOR ROTOR
摘要 <p>A blade for a compressor rotor comprises a blade root at a first end of the blade extending from a rotor body of the compressor, and a blade tip at a second end of the blade. The first end and the second end are disposed on a span of the blade. The blade root and the blade tip define a face of the blade between them. The blade tip comprises a first extremity and a second extremity. The blade tip is disposed such that a first segment of the blade tip defines a positive dihedral angle with the face of the blade. The first segment extends from a first point in the blade tip to the first extremity of the blade tip. A second segment of the blade tip defines a negative dihedral angle with the face of the blade. The second segment extends from a second point in the blade tip to the second extremity of the blade tip.</p>
申请公布号 CA2856264(A1) 申请公布日期 2015.08.03
申请号 CA20142856264 申请日期 2014.07.07
申请人 PRATT & WHITNEY CANADA CORP.;INDIAN INSTITUTE OF TECHNOLOGY, BOMBAY 发明人 ROY, BHASKAR;AMBOOR, PRADEEP M.;HALBE, CHAITANYA V.;YU, HONG;TOWNSEND, PETER
分类号 F01D5/14;F01D5/30 主分类号 F01D5/14
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