发明名称 STATOR BLADE FOR AXIAL COMPRESSOR
摘要 PROBLEM TO BE SOLVED: To prevent loss caused by secondary flow and downsize the whole device by twisting a blade near the end wall surface so as to coincide with the direction of boundary layer flow generated near the end wall surface part of the blade. SOLUTION: One end of a stator blade 1 is fixed onto the end wall surface 3 formed at a part of a shroud. In this case, the stator blade 1 is twisted near the contact parts with the end wall surface 3 at one end and the end wall surface at the other end so as to coincide with the direction of boundary layer flow 4. As a result, the parts near the end wall surface contact parts of the blade 1 are twisted large with different twist angles from a twist angle at a center part opposed to main flow from the view of a plurality of longitudinal sections of the stator blade 1. The boundary layer flow 4 thereby flows along the blade profile, so that the development and growth of secondary flow are suppressed, and the increase of loss is prevented to attain high efficiency while realizing a compact device.
申请公布号 JPH0925897(A) 申请公布日期 1997.01.28
申请号 JP19950174884 申请日期 1995.07.11
申请人 MITSUBISHI HEAVY IND LTD 发明人 KOBAYASHI KAZUYA
分类号 F04D19/00;F01D5/14;F04D29/54 主分类号 F04D19/00
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