首页> 外国专利> Moving blade for axial turbomachine has flow duct formed so that discharge openings lie radially further outside intake openings whereby driving pressure gradient at relevant operating points is large enough to permit suction and discharge

Moving blade for axial turbomachine has flow duct formed so that discharge openings lie radially further outside intake openings whereby driving pressure gradient at relevant operating points is large enough to permit suction and discharge

机译:用于轴向涡轮机的动叶片具有流道,流道形成为使得排放孔径向位于进气孔的外侧,从而在相关工作点处的驱动压力梯度足够大以允许吸入和排放

摘要

Moving blade (1) has an internal flow duct (2) which connects radially spaced-apart intake openings (8) and discharge openings (9) to each other. The flow duct is formed in such a way that the discharge openings lie radially further outside the intake openings. The difference in radius between intake and discharge point is selected so that the driving pressure gradient at all relevant operating points is large enough to permit suction and discharge. An INDEPENDENDENT CLAIM is also included for the application of moving blade.
机译:动叶片(1)具有内部流道(2),该内部流道将径向间隔开的进气口(8)和排气口(9)彼此连接。流动通道形成为使得排放孔径向地位于进气孔的外侧。选择进气点和排气点之间的半径差,以使所有相关工作点的驱动压力梯度都足够大,以允许吸气和排气。还包括独立权利要求,适用于移动刀片的应用。

著录项

  • 公开/公告号DE102005047016A1

    专利类型

  • 公开/公告日2007-04-05

    原文格式PDF

  • 申请/专利权人 MTU AERO ENGINES GMBH;

    申请/专利号DE20051047016

  • 发明设计人 KLINGELS HERMANN;SELMEIER RUDOLF;

    申请日2005-09-30

  • 分类号F01D5/18;

  • 国家 DE

  • 入库时间 2022-08-21 20:29:43

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