发明名称 |
ANNULAR FLOW DUCT FOR A TURBOMACHINE THROUGH WHICH A MAIN FLOW CAN FLOW IN THE AXIAL DIRECTION |
摘要 |
The invention relates to an annular flow duct (18) for a turbomachine, said flow duct (18) being arranged concentrically about a machine axis (2) running in the axial direction and being defined by a boundary wall (22, 24) of circular cross section for directing a main flow (26), wherein the boundary wall (22, 24) has a plurality of return flow passages (46) which are distributed over its circumference and through which in each case a partial flow (49) which can be detached from the main flow (26) at a bleed position (50) can be returned to the main flow (26) at a feed position (52) situated upstream of the bleed position (50), and having aerofoils (32), arrranged radially in the flow duct (18), of a blade ring, the aerofoil tips (42) of which lie opposite the boundary wall (22, 24), with a gap being formed in each case, wherein the aerofoils (32) are movable in a predetermined rotation direction (U) along the circumference of the boundary wall (22 ,24). In order to specify a compressor which is insensitive to pumping and flow separations, it is proposed that - as viewed in rotation direction (U) - the bleed position (50) of each return flow passage lie upstream of the corresponding feed position (52). |
申请公布号 |
WO2007141160(A1) |
申请公布日期 |
2007.12.13 |
申请号 |
WO2007EP55183 |
申请日期 |
2007.05.29 |
申请人 |
SIEMENS AKTIENGESELLSCHAFT;BAYERE, ROMAIN;BLOMEYER, MALTE;CORNELIUS, CHRISTIAN;MATTHIAS, TORSTEN;SIEBER, UWE |
发明人 |
BAYERE, ROMAIN;BLOMEYER, MALTE;CORNELIUS, CHRISTIAN;MATTHIAS, TORSTEN;SIEBER, UWE |
分类号 |
F01D5/14;F04D27/02;F04D29/68 |
主分类号 |
F01D5/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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