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    • 2. 发明授权
    • Valve with a crenellated seat
    • 带阀座的阀门
    • US5318270A
    • 1994-06-07
    • US977890
    • 1992-11-18
    • Francois DetanneMichel Vincent de Paul
    • Francois DetanneMichel Vincent de Paul
    • F16K1/42F01D17/14F01L3/06F16K47/02F16K47/08
    • F16K47/08F01D17/145F05D2250/182Y10T137/86759
    • The present invention relates to a valve including a valve member co-operating with a seat provided with a crenellated portion disposed around the portion of the seat on which the valve member rests, said crenellated portion being constituted by teeth separated by gaps, the inside walls of the teeth being portions of a vertical axis cylinder, the width l of the gaps being less than the width b of the inside walls of the teeth, wherein the end wall of the valve member facing the crenellated portion when the valve member is in its closed position is convex in shape, co-operating with the inside wall of each tooth to form a channel that flares from top to bottom of the tooth, the point of contact C between the valve member and the seat being at a distance d from the base B of the crenellated portion lying in the range 0.25 times to 0.5 times the width l of the gap. Vibrations are eliminated at partial load and pressure fluctuations downstream from the valve are reduced.
    • 本发明涉及一种阀,其包括与座椅配合的阀门构件,所述座椅设置有围绕所述阀构件所在的所述座椅部分周围设置的锯齿状部分,所述锯齿形部分由被间隙分开的齿构成,所述内壁 所述齿是垂直轴圆柱体的一部分,所述间隙的宽度l小于所述齿的内壁的宽度b,其中当所述阀构件处于其中时所述阀构件的所述端壁面向所述锯齿状部分 闭合位置是凸形的,与每个齿的内壁协作以形成从牙齿的顶部到底部的弹道的通道,阀构件和座椅之间的接触点C距离 锯齿状部分的基底B位于间隙宽度l的0.25倍至0.5倍的范围内。 在部分负载下消除振动,减小阀门下游的压力波动。
    • 4. 发明授权
    • Turbo-machine stage having reduced secondary losses
    • 具有减少次级损失的涡轮机阶段
    • US5167486A
    • 1992-12-01
    • US699126
    • 1991-05-13
    • Francois Detanne
    • Francois Detanne
    • F01D5/18F01D1/02F01D1/04F01D5/14F01D11/00F01D11/02F01D11/10
    • F01D5/145F01D1/02Y10S415/914
    • 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.
    • 一种涡轮级,包括固定在涡轮机的定子(3)上的一组固定叶片(1),并支撑一个隔膜,其后是安装在盘(9)上的一组移动叶片(8),该盘片固定在转子 (6),所述一组移动叶片(8)的周边具有由多个室(11)构成的密封件(10)。 盘(9)包括通向隔膜(4)和盘(9)之间的空间的吸入孔(16),并设置在盘(9)的周边部分附近。 抽吸孔(15)由通过至少一些运动叶片(8)的管道(17)连接到在密封件(10)下游的叶片(8)的顶部开口的出口孔口(18) 在其室(11)内。 固定叶片(2)根部的扰动流动和隔膜(4)和转子(6)之间的泄漏流被吸入孔16中,从而提高了效率。
    • 5. 发明授权
    • Impulse turbine stage with reduced secondary losses
    • 具有减少二次损失的脉冲涡轮机阶段
    • US5125794A
    • 1992-06-30
    • US699127
    • 1991-05-13
    • Francois Detanne
    • Francois Detanne
    • F01D1/02F01D5/06F01D5/14F01D11/00
    • F01D1/02F01D11/001F01D5/145Y10S415/914
    • An impulse turbine stage comprising a set (1) of fixed vanes (2) fixed to the stator (3) of the turbine and supporting a diaphragm (4), followed by a set (7) of moving vanes (8) mounted on a disc (9) fixed to the rotor (6) of the turbine, the stage being characterized in that said disk (9) is provided with through ducts (12) parallel to the axis of the rotor (6) and in that the inlets to the ducts (12) opening out into the gap between the diaphragm (6) and the disk (9) are provided with scoops (15) open sideways in the direction of rotation to direct fluid into the ducts (12). The invention serves to reduce the secondary losses of an impulse turbine.
    • 一种脉冲涡轮机级,包括固定在涡轮机的定子(3)上并固定有隔膜(4)的固定叶片(2)的组(1),其后是安装在其上的一组移动叶片(8) 固定在涡轮机的转子(6)上的盘(9),其特征在于,所述盘(9)设置有平行于转子(6)的轴线的通孔(12),并且入口 在隔膜(6)和盘(9)之间的间隙中打开的管道(12)设置有沿旋转方向侧向开放以将流体引导到管道(12)中的勺子(15)。 本发明用于减少脉冲涡轮机的二次损失。