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    • 11. 发明授权
    • Quarter turn quick connect fitting
    • 四分之一圈快速连接配件
    • US06361687B1
    • 2002-03-26
    • US09542667
    • 2000-04-04
    • Douglas W. FordDerrick S. LevanenJohn T. Martin
    • Douglas W. FordDerrick S. LevanenJohn T. Martin
    • B01D1508
    • F16L37/248F16L37/107G01N30/6026G01N30/6039
    • A quarter turn quick connect fitting assembly (10) for connecting miniature fluid conduits, such as tubing, includes a first fitting (12) having radially projecting pins (28) and a second fitting (14) located within a rotatable quarter turn nut (16) having spiral grooves (48) which receive the pins. The first fitting defines a central passage (26) and the second fitting defines a central passage (42) which may each be configured to slidably receive a hollow tube set (104), or to threadably receive an externally threaded mating fitting. The quarter turn quick connect fitting can be configured to attach to the end of a column, and can include an adapter (158), which houses a guard column (160), or a frit (188) for filtering the fluid passing through the quarter turn quick connect fitting assembly. The quarter turn quick connect fitting is assembled by sliding the pins of the first fitting into the grooves of the quarter turn nut and rotating the quarter turn nut through approximately 90° with respect to the first fitting, thereby securely seating the pins within angled areas defined at the ends of the grooves.
    • 用于连接微型流体管道(例如管道)的四分之一转的快速连接配件组件(10)包括具有径向突出销(28)的第一配件(12)和位于可旋转四分之一转动螺母(16)内的第二配件 )具有接收销的螺旋槽(48)。 第一配件限定中央通道(26),并且第二配件限定中央通道(42),其可以被构造成可滑动地容纳中空管组件(104),或者螺纹接纳外螺纹配合配件。 四分之一圈快速连接配件可以被配置为附接到柱的端部,并且可以包括容纳保护柱(160)的适配器(158)或用于过滤通过四分之一的流体的玻璃料(188) 转快速连接配件组件。 通过将第一配件的销滑动到四分之一转动螺母的凹槽中并将四分之一旋转螺母相对于第一配件旋转大约90°来组装四分之一转弯快速连接配件,从而将销牢固地固定在限定的成角度的区域内 在槽的端部。
    • 12. 发明授权
    • Integral fitting and filter
    • 整体配件和过滤器
    • US5911954A
    • 1999-06-15
    • US965626
    • 1997-11-06
    • Douglas W. FordKerry D. Nugent
    • Douglas W. FordKerry D. Nugent
    • B01D15/08B01L3/00G01N1/28G01N1/34G01N30/14G01N30/60B01L11/00
    • G01N1/4077B01D15/08B01D15/125B01L3/565G01N1/405G01N30/6039G01N30/14G01N30/6004G01N30/6034
    • An integral fitting and filter assembly includes a tubular body (119) having a integral proximal fitting piece (121) and an integral distal fitting piece (122). A central passage (125) extends through the proximal fitting piece and the distal fitting piece of the body. A tubular filter assembly sleeve including a filter sub-assembly (142) and tubular extension sleeve (140) is slidably received within the central passage of the body. The filter sub-assembly includes two end caps (144, 145) and a center piece (146). The center piece is packed with a selective chemical-absorbent packing material (26), that is retained within the center piece by first and second porous plugs (148) secured within opposite ends of the center piece of the end caps. The filter assembly is slidably inserted into the body, and is automatically adjustably positioned longitudinally to provide a pre-column filter that may be used to mate with differently configured mating fittings, such as high-performance liquid chromatography instrument inlet fittings.
    • 整体装配和过滤器组件包括具有一体的近侧配件件(121)和一体的远端配件件(122)的管状主体(119)。 中心通道(125)延伸穿过身体的近侧安装件和远端配件件。 包括过滤器子组件(142)和管状延伸套筒(140)的管状过滤器组件套筒可滑动地容纳在主体的中心通道内。 过滤器子组件包括两个端盖(144,145)和中心件(146)。 中心件装有选择性化学吸收性包装材料(26),其通过固定在端盖的中心件的相对端内的第一和第二多孔塞(148)保持在中心件内。 过滤器组件可滑动地插入到主体中,并且可纵向自动调节地定位,以提供可用于与不同配置的配合配件(例如高效液相色谱仪入口配件)配合的预柱过滤器。
    • 13. 发明授权
    • Small watercraft automatic steering apparatus and method
    • 小型船舶自动转向装置及方法
    • US5509369A
    • 1996-04-23
    • US320533
    • 1994-10-11
    • Douglas W. FordEric K. Juve
    • Douglas W. FordEric K. Juve
    • B63H25/04B63H25/22F02B61/04
    • B63H25/04B63H21/265F02B61/045
    • An automatic steering system (10) has a control subsystem (14) that employs a yaw rate control loop (90) and a steering control loop (92) to drive a hydraulic subsystem (12) in which the deflection rate of a steering actuator (16) is controlled without need for either a steering actuator angle sensor or an electronic steering bias integrator. Rather, the control subsystem employs a proportional rate servosystem to control the steering actuator deflection rate and a double-acting hydraulic cylinder (34) to provide the steering bias integral action. The control subsystem employs an electric compass (96) to generate heading data that are stored in a heading command register (102). A heading error is formed by calculating a difference between a desired heading and the current heading. A rate taker (94) generates a yaw rate feedback signal by differentiating changes in the current heading. The heading error and yaw rate feedback signal are processed to generate a steering rate command to which the steering control loop responds by pumping hydraulic fluid at a rate proportional to the steering rate command into the hydraulic cylinder to deflect the steering actuator of an outboard motor (18).
    • 自动转向系统(10)具有控制子系统(14),其采用横摆速度控制回路(90)和转向控制回路(92)来驱动液压子系统(12),其中转向致动器 16)被控制而不需要转向致动器角度传感器或电子转向偏置积分器。 相反,控制子系统使用比例速率伺服系统来控制转向致动器偏转速率和双作用液压缸(34)以提供转向偏压积分作用。 控制子系统使用电罗盘(96)产生存储在航向命令寄存器(102)中的航向数据。 通过计算期望的标题与当前的标题之间的差异来形成标题错误。 速率接收器(94)通过区分当前航向的变化来产生横摆率反馈信号。 航向误差和偏航率反馈信号被处理以产生转向速度命令,转向控制回路通过以与转向速率指令成比例的速率将液压流体泵送到液压缸中来使得舷外马达的转向致动器偏转, 18)。
    • 14. 发明授权
    • Windshear flight recovery command system
    • 风切变飞行恢复指挥系统
    • US4841448A
    • 1989-06-20
    • US92089
    • 1987-09-01
    • Douglas W. Ford
    • Douglas W. Ford
    • G05D1/06
    • G05D1/0623
    • The present invention constitutes a system for generating an elevator command signal for directing a pilot in guiding his aircraft along a path effective for recovering from hazardous windshear conditions. The system includes a descending mode guidance subsystem (10), an ascending mode guidance subsystem (12) and a switching mechanism (14) for shifting between the two subsystems. The descending mode subsystem includes an acceleration generator (20), a flight path command generator (22), a flight path error generator (24), a descending mode pitch error generator (26), an airspeed control device (28) and a descending mode signal controller (30). These components are connected serially together and operate to form an elevator command signal corresponding to the acceleration required to halt the descent of the aircraft by a fixed altitude level. They also function to control and condition this signal with respect to important flight parameters such as the aircraft's maximum safe angle of attack and the response capabilities of the pilot and aircraft.
    • 本发明构成一种用于产生电梯命令信号的系统,用于引导飞行员沿着有效从危险风切变条件恢复的路径引导他的飞行器。 该系统包括下行模式指导子系统(10),上行模式指导子系统(12)和用于在两个子系统之间移位的切换机构(14)。 下降模式子系统包括加速度发生器(20),飞行路径命令发生器(22),飞行路径误差发生器(24),下降模式螺距误差发生器(26),空速控制装置(28) 模式信号控制器(30)。 这些部件串联地连接在一起并且操作以形成对应于停止飞行器下降固定高度水平所需的加速度的电梯命令信号。 它们还用于控制和调节关于重要的飞行参数的信号,例如飞机的最大安全迎角和飞行员和飞机的响应能力。
    • 15. 发明授权
    • Method and apparatus for detecting control system data processing errors
    • 用于检测控制系统数据处理错误的方法和装置
    • US4698785A
    • 1987-10-06
    • US557631
    • 1983-12-02
    • John P. DesmondDouglas W. FordMichael E. FosseyMichael StanbroKenneth A. Zimmerman
    • John P. DesmondDouglas W. FordMichael E. FosseyMichael StanbroKenneth A. Zimmerman
    • G06F11/16G06F11/32
    • G06F11/1637G06F11/328G06F11/321
    • A digital-based control data processing system detects during system operation the occurrence of data processing errors. Data processing accuracy is verified by receiving output information developed from system input information in accordance with a first operational function, computing a derived version of the system input information in accordance with a second operational function, and comparing the derived version of the system input information to the actual system input information to determine whether they differ by a predetermined operational tolerance. This method for verifying processing accuracy is especially advantageous for detecting latent software errors which are unique to a particular computer program. The processing system includes display apparatus which develops from the output information a set of display symbols that convey the information on a monitor screen to the pilot. Assigned to each display symbol is an identifying tag which identifies in real time a display symbol that conveys erroneous information.
    • 基于数字的控制数据处理系统在系统操作期间检测数据处理错误的发生。 通过接收根据第一操作功能从系统输入信息开发的输出信息,根据第二操作功能计算系统输入信息的导出版本,并将系统输入信息的导出版本与 实际的系统输入信息,以确定它们是否因预定的运行公差而不同。 用于验证处理精度的该方法对于检测特定计算机程序唯一的潜在软件错误是特别有利的。 该处理系统包括显示装置,该显示装置根据输出信息显示将监视器屏幕上的信息传送给飞行员的一组显示符号。 分配给每个显示符号的是识别标签,其实时识别传达错误信息的显示符号。
    • 16. 发明授权
    • Integral fitting and filter of an analytical chemical instrument
    • 分析化学仪器的整体配件和过滤器
    • US5730943A
    • 1998-03-24
    • US659173
    • 1996-06-04
    • Douglas W. FordKerry D. Nugent
    • Douglas W. FordKerry D. Nugent
    • B01D15/08B01L3/00G01N1/28G01N1/34G01N30/14G01N30/60B01L11/00
    • G01N1/4077B01D15/08B01D15/125B01L3/565G01N1/405G01N30/6039G01N30/14G01N30/6004G01N30/6034
    • An integral fitting and filter assembly includes a tubular body (119) having a integral proximal fitting piece (121) and an integral distal fitting piece(122). A central passage (125) extends through the proximal fitting piece and the distal fitting piece of the body. A tubular filter assembly sleeve including a filter sub-assembly (142) and tubular extension sleeve (140) is slidably received within the central passage of the body. The filter sub-assembly includes two end caps (144, 145) and a center piece (146). The center piece is packed with a selective chemical-absorbent packing material (26), that is retained within the center piece by first and second porous plugs (148) secured within opposite ends of the center piece of the end caps. The filter assembly is slidably inserted into the body, and is automatically adjustably positioned longitudinally to provide a pre-column filter that may be used to mate with differently configured mating fittings, such as high-performance liquid chromatography instrument inlet fittings.
    • 整体装配和过滤器组件包括具有一体的近侧配件件(121)和一体的远端配件件(122)的管状主体(119)。 中心通道(125)延伸穿过身体的近侧安装件和远端配件件。 包括过滤器子组件(142)和管状延伸套筒(140)的管状过滤器组件套筒可滑动地容纳在主体的中心通道内。 过滤器子组件包括两个端盖(144,145)和中心件(146)。 中心件装有选择性化学吸收性包装材料(26),其通过固定在端盖的中心件的相对端内的第一和第二多孔塞(148)保持在中心件内。 过滤器组件可滑动地插入到主体中,并且可纵向自动调节地定位,以提供可用于与不同配置的配合配件(例如高效液相色谱仪入口配件)配合的预柱过滤器。
    • 19. 发明授权
    • Quarter turn quick connect fitting
    • 四分之一圈快速连接配件
    • US6095572A
    • 2000-08-01
    • US9647
    • 1998-01-20
    • Douglas W. FordDerrick S. LevanenJohn T. Martin
    • Douglas W. FordDerrick S. LevanenJohn T. Martin
    • F16L37/10F16L37/107F16L37/248F16L17/06
    • F16L37/248F16L37/107G01N30/6026G01N30/6039
    • A quarter turn quick connect fitting assembly (10) for connecting miniature fluid conduits, such as tubing, includes a first fitting (12) having radially projecting pins (28) and a second fitting (14) located within a rotatable quarter turn nut (16) having spiral grooves (48) which receive the pins. The first fitting defines a central passage (26) and the second fitting defines a central passage (42) which may each be configured to slidably receive a hollow tube set (104), or to threadably receive an externally threaded mating fitting. The quarter turn quick connect fitting can be configured to attach to the end of a column, and can include an adapter (158), which houses a guard column (160), or a frit (188) for filtering the fluid passing through the quarter turn quick connect fitting assembly. The quarter turn quick connect fitting is assembled by sliding the pins of the first fitting into the grooves of the quarter turn nut and rotating the quarter turn nut through approximately 90.degree. with respect to the first fitting, thereby securely seating the pins within angled areas defined at the ends of the grooves.
    • 用于连接微型流体管道(例如管道)的四分之一转的快速连接配件组件(10)包括具有径向突出销(28)的第一配件(12)和位于可旋转四分之一转动螺母(16)内的第二配件 )具有接收销的螺旋槽(48)。 第一配件限定中央通道(26),并且第二配件限定中央通道(42),其可以被构造成可滑动地容纳中空管组件(104),或者螺纹接纳外螺纹配合配件。 四分之一圈快速连接配件可以被配置为附接到柱的端部,并且可以包括容纳保护柱(160)的适配器(158)或用于过滤通过四分之一的流体的玻璃料(188) 转快速连接配件组件。 通过将第一配件的销滑动到四分之一转动螺母的凹槽中并将四分之一旋转螺母相对于第一配件旋转大约90°来组装四分之一转弯快速连接配件,从而将销牢固地固定在限定的成角度的区域内 在槽的端部。
    • 20. 发明授权
    • Automatic steering apparatus and method for small watercraft
    • 小型船舶自动转向装置及方法
    • US5632217A
    • 1997-05-27
    • US634116
    • 1996-04-17
    • Douglas W. FordEric K. Juve
    • Douglas W. FordEric K. Juve
    • B63H25/04B63H25/22F02B61/04
    • B63H25/04B63H21/265F02B61/045
    • An automatic steering system (10) has a control subsystem (14) that employs a yaw rate control loop (90) and a steering control loop (92) to drive a hydraulic subsystem (12) in which the deflection rate of a steering actuator (16) is controlled without need for either a steering actuator angle sensor or an electronic steering bias integrator. Rather, the control subsystem employs a proportional rate servosystem to control the steering actuator deflection rate and a double-acting hydraulic cylinder (34) to provide the steering bias integral action. The control subsystem employs an electric compass (96) to generate heading data that are stored in a heading command register (102). An heading error is formed by calculating a difference between a desired heading and the current heading. A rate taker (94) generates a yaw rate feedback signal by differentiating changes in the current heading, or alternatively, a rate sensor (302) generates the yaw rate feedback signal directly. The heading error and yaw rate feedback signal are processed to generate a steering rate command to which the steering control loop responds by pumping hydraulic fluid at a rate proportional to the steering rate command into the hydraulic cylinder to deflect a steering actuator (38) of an outboard motor (18).
    • 自动转向系统(10)具有控制子系统(14),其采用横摆速度控制回路(90)和转向控制回路(92)来驱动液压子系统(12),其中转向致动器 16)被控制而不需要转向致动器角度传感器或电子转向偏置积分器。 相反,控制子系统使用比例速率伺服系统来控制转向致动器偏转速率和双作用液压缸(34)以提供转向偏压积分作用。 控制子系统使用电罗盘(96)产生存储在航向命令寄存器(102)中的航向数据。 通过计算期望的航向和当前航向之间的差异来形成航向误差。 速率接收器(94)通过区分当前航向的变化产生偏航率反馈信号,或者,速率传感器(302)直接产生横摆率反馈信号。 处理航向误差和偏航率反馈信号以产生转向速率命令,转向控制回路通过以与转向速率命令成比例的速率泵送液压流体来对液压缸进行响应,以使液压缸的转向致动器(38)偏转 舷外马达(18)。