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    • 23. 发明申请
    • PRESSURE REGULATING VALVE FOR AIRCRAFT ENGINE
    • 用于飞机发动机的压力调节阀
    • US20140033730A1
    • 2014-02-06
    • US14050721
    • 2013-10-10
    • PRATT & WHITNEY CANADA CORP.
    • Johnny VinskiDaniel BlaisStephane Fortier
    • F02C7/00
    • F02C7/00F02C7/232F05D2260/85F16K11/0716G05D16/106Y10T137/2574Y10T137/2605Y10T137/2612Y10T137/2622Y10T137/2625Y10T137/2627Y10T137/2642Y10T137/8671Y10T137/86879Y10T137/86887
    • The fluid pressure regulating valve is for use in an aircraft engine. The valve has at least a first fluid inlet, a first fluid outlet and a second fluid outlet. The valve comprises: a valve housing having a first valve spool interior cavity; a first fluid path within the valve housing from the fluid inlet to the first fluid outlet; a second fluid path within the valve housing from the fluid inlet to the second fluid outlet; a first valve spool mounted for reciprocal motion within the first valve spool cavity between a first position and a second position, the first valve spool having a second valve spool interior cavity and being spring-biased to its first position; and a second valve spool mounted for reciprocal motion within the second valve spool cavity between a first position and a second position, the second valve spool being spring-biased to its first position, the second valve spool closing the first fluid path at its second position when the first valve spool is substantially at its first position.
    • 流体压力调节阀用于飞机发动机。 阀具有至少第一流体入口,第一流体出口和第二流体出口。 该阀包括:具有第一阀芯内腔的阀壳; 所述阀壳体内的从所述流体入口到所述第一流体出口的第一流体路径; 所述阀壳体内的从所述流体入口到所述第二流体出口的第二流体路径; 第一阀芯,其安装成在第一阀芯腔内在第一位置和第二位置之间往复运动,第一阀芯具有第二阀芯内腔,并被弹簧偏置到其第一位置; 以及第二阀芯,其安装成在第二阀芯腔内在第一位置和第二位置之间往复运动,所述第二阀芯被弹簧偏置到其第一位置,所述第二阀芯在其第二位置处关闭所述第一流体路径 当第一阀芯基本处于其第一位置时。
    • 24. 发明申请
    • PRESSURE REGULATING VALVE FOR AIRCRAFT ENGINE
    • 用于飞机发动机的压力调节阀
    • US20100187451A1
    • 2010-07-29
    • US12361771
    • 2009-01-29
    • JOHNNY VINSKIDaniel BLAISStephane FORTIER
    • JOHNNY VINSKIDaniel BLAISStephane FORTIER
    • F16K31/12
    • F02C7/00F02C7/232F05D2260/85F16K11/0716G05D16/106Y10T137/2574Y10T137/2605Y10T137/2612Y10T137/2622Y10T137/2625Y10T137/2627Y10T137/2642Y10T137/8671Y10T137/86879Y10T137/86887
    • The fluid pressure regulating valve is for use in an aircraft engine. The valve has at least a first fluid inlet, a first fluid outlet and a second fluid outlet. The valve comprises: a valve housing having a first valve spool interior cavity; a first fluid path within the valve housing from the fluid inlet to the first fluid outlet; a second fluid path within the valve housing from the fluid inlet to the second fluid outlet; a first valve spool mounted for reciprocal motion within the first valve spool cavity between a first position and a second position, the first valve spool having a second valve spool interior cavity and being spring-biased to its first position; and a second valve spool mounted for reciprocal motion within the second valve spool cavity between a first position and a second position, the second valve spool being spring-biased to its first position, the second valve spool closing the first fluid path at its second position when the first valve spool is substantially at its first position.
    • 流体压力调节阀用于飞机发动机。 阀具有至少第一流体入口,第一流体出口和第二流体出口。 该阀包括:具有第一阀芯内腔的阀壳; 所述阀壳体内的从所述流体入口到所述第一流体出口的第一流体路径; 所述阀壳体内的从所述流体入口到所述第二流体出口的第二流体路径; 第一阀芯,其安装成在第一阀芯腔内在第一位置和第二位置之间往复运动,第一阀芯具有第二阀芯内腔,并被弹簧偏置到其第一位置; 以及第二阀芯,其安装成在第二阀芯腔内在第一位置和第二位置之间往复运动,所述第二阀芯被弹簧偏置到其第一位置,所述第二阀芯在其第二位置处关闭所述第一流体路径 当第一阀芯基本处于其第一位置时。
    • 27. 发明授权
    • Compressor control valve
    • 压缩机控制阀
    • US3329154A
    • 1967-07-04
    • US26798663
    • 1963-03-26
    • BENDIX WESTINGHOUSE AUTOMOTIVE
    • MORSE ROBERT JVALENTINE HARRY M
    • G05D16/10
    • F04B49/03F04B39/1006F04B49/035Y10T137/2627Y10T137/7738
    • 1,043,806. Valves. BENDIX-WESTING- HOUSE AUTOMOTIVE AIR BRAKE CO. March 20, 1964 [March 26, 1963], No. 11963/64. Heading F2V. [Also in Division G3] A valve suitable for insertion in the line between a compressor and a receiver comprises an inlet chamber 12, a delivery chamber 14 and a check valve 60 allowing flow from the inlet to the delivery chamber. The check valve forms part of a piston 46 slidable in bore 47 and co-operating with a stop 48 carried by a spindle 42. The latter also carries an exhaust valve 36 loaded by a spring 54. When the pressure in the inlet chamber reaches a predetermined value it unseats the exhaust valve with a snap-action and the lowered pressure in the inlet chamber then allows the piston 60 to be driven downwardly by the receiver pressure until it engages stop 48, whereby the exhaust valve is retained open until the receiver pressure drops to a second, lower, predetermined value. In modifications, the piston and exhaust valve are rigidly interconnected, or the spindle 42 is rigid with the piston and the exhaust valve is slidable on the spindle with its loading spring in exhaust chamber 35. A filter may be provided in the inlet chamber upstream of the check valve. The latter comprises an annular gasket supported on a plate 64 retained by a snap-ring 66.