发明名称 TURBO-MACHINE STAGE HAVING REDUCED SECONDARY LOSSES
摘要 A turbine stage comprising a set of fixed vanes (1) fixed to the stator (3) of the turbine and supporting a diaphragm, followed by a set of moving vanes (8) mounted on a disk (9) which is fixed to the rotor (6) of the turbine, the periphery of the set of moving vanes (8) having seals (10) constituted by a plurality of chambers (11). The disk (9) includes suction orifices (16) opening out into the space between the diaphragm (4) and the disk (9) and disposed in the vicinty of the peripheral portion of the disk (9). The suction orifices (15) are connected by ducts (17) passing through at least some of the moving vanes (8) to outlet orifices (18) which open out in the tips of the vanes (8) downstream from the seals (10) within a chamber (11) thereof. The disturbed flow at the roots of the fixed vanes (2) and the leakage flow between the diaphragm (4) and the rotor (6) are sucked into the orifices (16), thereby improving efficiency.
申请公布号 US5167486(A) 申请公布日期 1992.12.01
申请号 US19910699126 申请日期 1991.05.13
申请人 GEC ALSTHOM SA 发明人 DETANNE, FRANCOIS
分类号 F01D5/18;F01D1/02;F01D1/04;F01D5/14;F01D11/00;F01D11/02;F01D11/10 主分类号 F01D5/18
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