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1. 发明授权

US4467984A Angular rate sensing apparatus and methods 失效
标题翻译：角速率检测装置及方法
公开(公告)号：US4467984A
公开(公告)日：1984-08-28
申请号：US206195
申请日：1980-11-12
申请人： Thomas B. Tippetts
发明人： Thomas B. Tippetts
IPC分类号： G01C19/00 , G01C19/58 , G01P3/26 , G01P9/00 , B64C13/16 , F15C1/04 , F15C1/06 , F15C3/00
CPC分类号： G01C19/58 , G01P3/266 , Y10T137/212 , Y10T137/218 , Y10T137/2202 , Y10T137/2224
摘要： A three-axis navigational guidance system utilizes three specially designed internal jet-type fluidic angular rate sensors which simultaneously sense the rotational rate of a guided body relative to three mutually perpendicular control axes. Fluidic output signals from the sensors are converted to electrical signals which are used to maintain the body in a preselected attitude relative to each of the three axes. The sensors are rendered extremely accurate by means of unique calibration mechanisms associated therewith which compensate for or correct for fabricational inaccuracies in the sensors. The operation of the rate sensing portion of the guidance system is environmentally stabilized by a novel jet-control system which automatically maintains the Reynolds number of each sensor jet within a predetermined range to thereby substantially eliminate jet drift.
摘要翻译：三轴导航引导系统采用三个专门设计的内部喷射型流体角速度传感器，它同时感测导向体相对于三个相互垂直的控制轴的旋转速度。来自传感器的流体输出信号被转换成电信号，其用于将主体相对于三个轴中的每一个保持在预选的姿态。传感器通过与之相关的独特的校准机构变得非常精确，这些校准机制可补偿或纠正传感器中的制造不准确。引导系统的速率感测部分的操作通过新颖的喷射控制系统进行环境稳定，该喷射控制系统将每个传感器喷嘴的雷诺数自动维持在预定范围内，从而基本上消除喷射漂移。

2. 发明授权

US4256015A Fluidic stabilization control 失效
标题翻译：流体稳定控制
公开(公告)号：US4256015A
公开(公告)日：1981-03-17
申请号：US967812
申请日：1978-12-08
申请人： Thomas B. Tippetts , Francis M. Manion
发明人： Thomas B. Tippetts , Francis M. Manion
IPC分类号： F15C4/00 , F41G5/14 , F41G5/24 , F15B13/16
CPC分类号： F41G5/24 , F15C4/00 , F41G5/14 , Y10T137/212 , Y10T137/2202
摘要： A fluidic system for stabilizing movement of a body subject to oscillation at its natural frequency, such as a tank-mounted gun, with appropriate circuitry and controls for notch filtering control output signals at the natural frequency.
摘要翻译：一种流体系统，用于在固有频率下稳定受到固有频率振荡的物体的运动，例如油箱安装的枪，具有适当的电路和控制，用于陷波滤波，以固有频率控制输出信号。

3. 发明授权

US4648807A Compact piezoelectric fluidic air supply pump 失效
标题翻译：紧凑型压电流体供气泵
公开(公告)号：US4648807A
公开(公告)日：1987-03-10
申请号：US734003
申请日：1987-05-14
申请人： Thomas B. Tippetts , Michael F. Cycon, Jr.
发明人： Thomas B. Tippetts , Michael F. Cycon, Jr.
IPC分类号： F04B9/00 , F04B43/00 , F04B43/04 , F04B45/047 , F04B35/04 , F04B45/04
CPC分类号： F04B43/0027 , F04B43/046
摘要： The piezoelectrically driven diaphragm of an air pump is extended through a chamber and commmunicating outlet passage of the pump's housing. During vibration of the diaphragm, air pulses are alternately expelled through the outlet passage portions positioned on opposite sides of the diaphragm. The air pulses are collected in a rectifying device, carried by the housing, for delivery to a fluidic device or system.
摘要翻译：空气泵的压电驱动隔膜通过泵的壳体的通道出口通道延伸。在隔膜的振动期间，空气脉冲通过位于隔膜相对侧的出口通道部分交替排出。空气脉冲被收集在由壳体承载的整流装置中，用于输送到流体装置或系统。

4. 发明授权

US4441525A Fluidic stabilization control 失效
标题翻译：流体稳定控制
公开(公告)号：US4441525A
公开(公告)日：1984-04-10
申请号：US171764
申请日：1980-07-24
申请人： Thomas B. Tippetts , Francis M. Manion
发明人： Thomas B. Tippetts , Francis M. Manion
IPC分类号： F15C4/00 , F41G5/14 , F41G5/24 , F15C1/12 , F15C3/00
CPC分类号： F41G5/14 , F15C4/00 , F41G5/24 , Y10T137/212 , Y10T137/2202 , Y10T137/2322
摘要： A fluidic system for stabilizing movement of a body subject to oscillation at its natural frequency, such as a tank-mounted gun, with appropriate circuitry and controls for notch filtering control output signals at the natural frequency.
摘要翻译：一种流体系统，用于在固有频率下稳定受到固有频率振荡的物体的运动，例如油箱安装的枪，具有适当的电路和控制，用于陷波滤波，以固有频率控制输出信号。

5. 发明授权

US3993101A Tristable fluidic device 失效
标题翻译：三重流体装置
公开(公告)号：US3993101A
公开(公告)日：1976-11-23
申请号：US607529
申请日：1975-08-25
申请人： Thomas B. Tippetts , Donald W. Chapin
发明人： Thomas B. Tippetts , Donald W. Chapin
IPC分类号： F15C1/04 , F15C3/14 , F15C4/00 , F15C1/10 , F15C3/00
CPC分类号： F15C4/00 , F15C1/04 , F15C3/14 , Y10T137/2213 , Y10T137/2322
摘要： An electrofluidic transducer which utilizes an electromagnetic device that is energizable by electric currents of opposite polarity to shift a fluid beam in opposite directions away from a central position. In its central position the beam deflector is between a pair of fluid nozzles, and shifts to deflect respective fluid beam from the two nozzles upon opposite energization of the electromagnet, so that three different pressure differential signals may be selectively impressed upon a pair of fluid output ports registering with the pair of fluid nozzles.
摘要翻译：一种电流换能器，其利用可由相反极性的电流激励的电磁装置，以使流体束在相对方向上偏离中心位置。在其中心位置，光束偏转器位于一对流体喷嘴之间，并且在电磁体相反通电时偏移来自两个喷嘴的各个流体束，从而可以将三个不同的压差信号选择性地压入一对流体输出端口与一对流体喷嘴对准。

6. 发明授权

US4445377A Pressure-to-electric output system for an angular rate sensor or the like 失效
标题翻译：用于角速率传感器等的压力 - 电力输出系统
公开(公告)号：US4445377A
公开(公告)日：1984-05-01
申请号：US206199
申请日：1980-11-12
申请人： Thomas B. Tippetts
发明人： Thomas B. Tippetts
IPC分类号： G01C19/00 , G01C19/58 , G01P3/26 , G01P9/00 , G01P15/00
CPC分类号： G01P3/263 , G01C19/58 , Y10T137/2065
摘要： A pressure-to-electric output system is used to convert the dual outlet pressure signals of a fluidic angular rate sensor to a pair of oscillating electrical signals whose relative frequency differential is very accurately indicative of the sensor outlet pressure differential. The sensor outlets are fluidically coupled to the control ports of the first amplifier in a cascaded series of fluidic proportional amplifiers. The outlet ports of the terminal amplifier are coupled to the inlet ports of a pair of fluidic oscillators. A pair of microphone type pressure-to-electric transducers are driven by the oscillators to produce the oscillating electrical signals.
摘要翻译：压力 - 电力输出系统用于将流体角速度传感器的双出口压力信号转换成一对振荡电信号，其相对频率差异非常精确地指示传感器出口压力差。传感器出口流体耦合到级联的一系列流体比例放大器中的第一放大器的控制端口。端子放大器的出口连接到一对流体振荡器的入口端口。一对麦克风型压电换能器由振荡器驱动以产生振荡电信号。

7. 发明授权

US4019697A Fluidic approach power compensator control system 失效
标题翻译：流体动力补偿器控制系统
公开(公告)号：US4019697A
公开(公告)日：1977-04-26
申请号：US607530
申请日：1975-08-25
申请人： Thomas B. Tippetts
发明人： Thomas B. Tippetts
IPC分类号： B64D37/00 , F15C1/00 , G05D1/06
CPC分类号： G05D1/063 , B64D37/00 , F15C1/006 , Y10T137/2071 , Y10T137/2147
摘要： A fluidic control system which automatically schedules and controls power developed by an aircraft during landing approach operation. Fluidic signals are generated in relation to sensed aircraft flight parameters, and these signals are combined in a preselected manner which includes integration of one of the signals by a series feedback capacitance fluidic integrator, to produce a single input signal indicative of a desired rate of fuel flow to schedule aircraft power to the desired level. The single input signal is temperature compensated, then discretely selectively modified in relation to ambient conditions by selectively varying the impedance of fluidic resistive networks to alter the gain of a fluidic amplifier driven by the single input signal. An error signal is then generated and amplified to produce a power output signal which drives a fuel control servo actuator in proportion to the error signal when the latter is small, and drives the servo in a digital manner when the error is large.
摘要翻译：一种流体控制系统，可在着陆过程中自动调度和控制飞机开发的功率。关于感测到的飞行器飞行参数产生流体信号，并且这些信号以预选的方式组合，其包括通过串联反馈电容流体积分器对信号中的一个进行积分，以产生指示所需燃料速率的单个输入信号流量将飞机功率调至所需水平。单个输入信号经过温度补偿，然后通过选择性地改变流体电阻网络的阻抗以改变由单个输入信号驱动的流体放大器的增益而相对于环境条件离散地选择性地修改。然后产生并放大误差信号以产生功率输出信号，当功率输出信号较小时驱动燃料控制伺服致动器与误差信号成比例，并且当误差较大时以数字方式驱动伺服。

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