发明名称 Wall contour for an axial turbomachine
摘要 <p>The rotor-sided and/or stator-sided flow-defining wall (10,11) of the channel is angled at the discharge end of the rotor blades (La1,La2,La3). The angle is dimensioned, so that total pressure and outflow angle of the flow coming from the rotor blades are homogenised. The wall has an additional counter angle (B,BB) approx. near the intake area of the guide blades (Le2,Le3,Le4) of the following stage. On the stator side, the wall is formed by the foot plates (13) of these guide blades, which face the flow channel. Behind the angle, the wall extends mainly in the plane of the rotor blade intake, so that it has a common point (P) with the original straight outer channel contour (51).</p>
申请公布号 EP0799973(B1) 申请公布日期 2002.07.03
申请号 EP19960810199 申请日期 1996.04.01
申请人 ALSTOM 发明人 KREITMEIER, FRANZ
分类号 F01D9/04;F01D5/14;(IPC1-7):F01D9/04 主分类号 F01D9/04
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