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    • 71. 发明授权
    • Laminar fluidic devices
    • 层压流体装置
    • US3662772A
    • 1972-05-16
    • US3662772D
    • 1969-11-21
    • GEN ELECTRIC
    • READER TREVOR D
    • G01P3/26F15C1/06F15C1/08F15C1/14F15C1/00
    • F15C1/14F15C1/08Y10T137/2251Y10T137/2256
    • Fluidic devices wherein the fluid stream or streams acting therein are always in the laminar state. The important elements of each fluidic device, which include one or more supply passageways, one or more receiver passageways, vents, a cavity and possibly one or more control passageways, are of a configuration and location such that fluid flowing through each supply passageway forms a laminar fluid stream which is capable of being received by one or more of the receiver passageways in a laminar state. The Reynolds number of the fluid forming the laminar fluid stream is preferably within the range of 200-1,500. The subject invention is applicable to a wide variety of fluidic devices including proportional and digital amplifiers, OR and AND gates, and rate sensors wherein the signal-to-noise ratio is substantially lower than that of conventional turbulent flow fluidic devices.
    • 其中在其中作用的流体流或流总是处于层流状态的流体装置。 每个流体装置的重要元件,其包括一个或多个供应通道,一个或多个接收器通道,通风口,空腔以及可能的一个或多个控制通道,其结构和位置使得流过每个供应通道的流体形成 能够由层流状态的一个或多个接收器通道接收的层流体流。 形成层流体流的流体的雷诺数优选在200-1,500的范围内。 本发明可应用于包括比例和数字放大器,OR和AND门以及速率传感器的各种流体装置,其中信噪比基本上低于常规湍流流体装置。
    • 73. 发明授权
    • Fluidic amplifiers with adaptive gain and/or frequency responses
    • 具有自适应增益和/或频率响应的流体放大器
    • US3621861A
    • 1971-11-23
    • US3621861D
    • 1969-11-12
    • BOWLES FLUIDICS CORP
    • BOWLES ROMALD E
    • F15C1/04F15C1/14F15C3/00
    • F15C1/04F15C1/14Y10T137/2076Y10T137/218Y10T137/2251Y10T137/2256
    • TECHNIQUES ARE DISCLOSED WHEREIN SYMMETRY OF OPERATION, GAIN AND/OR FREQUENCY RESPONSE CHARACTERISTICS OF FLUIDIC AMPLIFIERS MAY BE SELECTIVELY VARIED. IN ONE TECHNIQUE AN AMPLIFIER VENT PASSAGE IS PROVIDED WITH ONE OR MORE INSERTS WHICH CHANGE IN SIZE AND SHAPE IN RESPONSE TO TEMPERATURE AND/OR QUALITATIVE COMPOSITION OF THE WORKING FLUID, THE LATTER TWO PARAMETERS BEING SELECTIVELY VARIABLE TO CHANGE THE FLOW IMPEDANCE OF THE VENT PASSAGE. ANOTHER TECHNIQUE EMPLOYS A SIMILAR INSET IN A FLUIDIC CAPACITOR CONNECTED TO THE AMPLIFIER OUTPUT PASSAGE, WHEREBY THE CAPACITY OF THE OUTPUT PASSAGE, AND HENCE THE FREQUENCY RESPONSE OF THE AMPLIFIER, IS SELECTIVELY VARIABLE WITH EITHER WORKING FLUID TEMPERATURE OR WORKING FLUID QUALITATIVE COMPOSITION. IN STILL ANOTHER TECHNIQUE THE REYNOLDS NUMBER OF A POWER STREAM IN A TURBULENCE AMPLIFIER IS SELECTIVELY VARIED BY VARYING FLUID TEMPERATURE, PRESSURE AND/OR QUALITATIVE COMPOSITION, WHEREBY TO VARY THE SENSITIVITY OF THE POWER STREAM TO TURBULENCE IN RESPONSE TO DIFFERENT INPUT SIGNAL FREQUENCIES. IN ANOTHER TECHNIQUE FLUIDIC CAPACITORS, CONNECTED TO THE INPUT AND/OR OUTPUT PASSAGES OF A FLUIDIC AMPLIFIER, ARE SELECTIVELY VARIED BY INTRODUCING VARIABLE QUANTITIES OF CONTROL FLUID INTO THE CAPACITORS, THE VARIABLE CAPACITY PROVIDES CORRESPONDING VARIABLE AMPLIFIER FREQUENCY RESPONSE CHARACTERISTICS. IN ANOTHER TECHNIQUE, THE POWER STREAM PRESSURE IN A FLUIDIC AMPLIFIER IS AUTOMATICALLY VERIED TO MAINTAIN THE MINIMUM POWER STREAM PRESSURE NECESSARY TO PROVIDE A LINEAR AMPLIFIER GAIN CHARACTERISTICS FOR VARYING INPUT SIGNAL RANGES.
    • 80. 发明授权
    • Pressure ratio control system for a gas turbine engine
    • 一种气体涡轮发动机的压力比控制系统
    • US3564844A
    • 1971-02-23
    • US3564844D
    • 1969-07-18
    • DOWTY FUEL SYST LTD
    • RIMMER RONALD
    • F02C9/32F02C9/10F15C1/14
    • F02C9/32Y10T137/2093
    • A PRESSURE RATIO CONTROL SYSTEM FOR A GAS TURBINE ENGINE HAVING A FUEL PUMP TOGETHER WITH MEANS REGULATING FUEL FLOW TO THE ENGINE BURNERS, COMPRISING A PRESSURE RATIOSENSING DEVICE HAVING A DISCHARGE NOZZLE AND A RECEIVER NOZZLE CO-AXIALLY SPACED THEREFROM, THE DIAMETERS AND SPACING OF THE NOZZLES BEING SUCH THAT IN THE REGION OF A PREDETERMINED CRITICAL RATIO OF INLET PRESSURE TO OUTLET PRESSURE OF THE DISCHARGE NOZZLE, THE RATE OF CHANGE OF PRESSURE IN THE RECEIVE NOZZLE, OCCURRING WITH A CHANGE IN THE DISCHARGE NOZZLE PRESSURE RATIO, PROVIDES A CONTROLLING PARAMETER RESTRICTOR MEANS FOR SUPPLYING THE INLET AND OUTLET RESPECTIVELY OF THE DISCHARGE NOZZLE WITH HIGHER AND LOWER FLUID PRESSURES DERIVED FROM TWO DIFFERENT PRESSURE SOURCES IN THE ENGINE COMPRESSOR, CONTROL MEANS OPERABLE ON THE RESTRICTOR MEANS TO SELECT A DISCHARGE NOZZLE PRESSURE RATIO AS A SELECTED PROPORTION OF THE COMPRESSOR PRESSURE RATIO OF THE TWO SOURCES, AND FLUID-OPERATED MEANS ARRANGED TO CONTROL THE FUEL FLOW REGULATING MEANS IN RESPONSE TO A CHANGE IN THE PRESSURE IN THE RECEIVER NOZZLE, WHEREBY THE RATE OF COMBUSTION OF FUEL REGULATES THE ENGINE SPEED AND THEREFORE THE SAID COMPRESSOR PRESSURE RATIO SUCH THAT THE DISCHARGE NOZZLE PRESSURE RATIO TENDS TOWARDS THE PREDETERMINED CRITICAL VALUE.