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    • 1. 发明申请
    • Annular Flow Duct for a Turbomachine Through which a Main Flow can Flow in the Axial Direction
    • 一个涡轮机的环形流道,主流通过该流道可以在轴向流动
    • US20090290974A1
    • 2009-11-26
    • US12227928
    • 2007-05-29
    • Romain BayereMalte BlomeyerChristian CorneliusTorsten MatthiasUwe Sieber
    • Romain BayereMalte BlomeyerChristian CorneliusTorsten MatthiasUwe Sieber
    • F04D27/02F04D29/68
    • F01D5/145F01D5/143F04D29/526F04D29/685
    • Disclosed is an annular flow duct for a turbomachine, the flow duct arranged concentrically about a machine axis running in the axial direction and defined by a boundary wall of circular cross section for directing a main flow, wherein the boundary wall has a plurality of return flow passages distributed over its circumference and through which in each case a partial flow is detached from the main flow at a bleed position and returned to the main flow at a feed position situated upstream of the bleed position, and having aerofoils, arranged radically in the flow duct, of a blade ring, the aerofoil tips of which lie opposite the boundary wall, with a gap formed in each case, wherein the aerofoils are movable in a predetermined rotation direction along the circumference of the boundary wall. Furthermore, a compressor which is insensitive to pumping and flow separations, as viewed in rotation direction, the bleed position of each return flow passage lies upstream of the corresponding feed position.
    • 公开了一种用于涡轮机的环形流动管道,该流动管道围绕沿着轴向运动的机器轴线同心地布置并且由用于引导主流量的圆形横截面的边界壁限定,其中边界壁具有多个回流 分布在其圆周上的通道,并且在每种情况下,部分流动在出口位置处与主流体分离,并且在位于排放位置上游的进给位置处返回到主流体,并且具有从根本上排列在流体中的机翼 一个叶片环的管道,其机翼尖头与边界壁相对,在每种情况下形成间隙,其中翼型件可沿着边界壁的圆周沿预定的旋转方向移动。 此外,从旋转方向观察对泵送和流动分离不敏感的压缩机,每个返回流动通道的排放位置位于相应进给位置的上游。
    • 2. 发明授权
    • Annular flow duct for a turbomachine through which a main flow can flow in the axial direction
    • 用于涡轮机的环形流道,主流通过该流道可沿轴向流动
    • US08066471B2
    • 2011-11-29
    • US12227928
    • 2007-05-29
    • Romain BayereMalte BlomeyerChristian CorneliusTorsten MatthiasUwe Sieber
    • Romain BayereMalte BlomeyerChristian CorneliusTorsten MatthiasUwe Sieber
    • F04D27/02
    • F01D5/145F01D5/143F04D29/526F04D29/685
    • Disclosed is an annular flow duct for a turbomachine, the flow duct arranged concentrically about a machine axis running in the axial direction and defined by a boundary wall of circular cross section for directing a main flow, wherein the boundary wall has a plurality of return flow passages distributed over its circumference and through which in each case a partial flow is detached from the main flow at a bleed position and returned to the main flow at a feed position situated upstream of the bleed position, and having aerofoils, arranged radically in the flow duct, of a blade ring, the aerofoil tips of which lie opposite the boundary wall, with a gap formed in each case, wherein the aerofoils are movable in a predetermined rotation direction along the circumference of the boundary wall. Furthermore, a compressor which is insensitive to pumping and flow separations, as viewed in rotation direction, the bleed position of each return flow passage lies upstream of the corresponding feed position.
    • 公开了一种用于涡轮机的环形流动管道,该流动管道围绕沿着轴向运动的机器轴线同心地布置并且由用于引导主流量的圆形横截面的边界壁限定,其中边界壁具有多个回流 分布在其圆周上的通道,并且在每种情况下,部分流动在出口位置处与主流体分离,并且在位于排放位置上游的进给位置处返回到主流体,并且具有从根本上排列在流体中的机翼 一个叶片环的管道,其机翼尖头与边界壁相对,在每种情况下形成间隙,其中翼型件可沿着边界壁的圆周沿预定的旋转方向移动。 此外,从旋转方向观察对泵送和流动分离不敏感的压缩机,每个返回流动通道的排放位置位于相应进给位置的上游。