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1. 发明授权

US11026361B2 Linear/angular correction of pick-and-place held component and related optical subsystem 有权
公开(公告)号：US11026361B2
公开(公告)日：2021-06-01
申请号：US13838075
申请日：2013-03-15
申请人： John S. Youngquist
发明人： John S. Youngquist
IPC分类号： H05K13/04 , H05K13/08
摘要： A pick-and-place machine and method includes use of a passive component feeder cartridge including a feeder gear. Rotation of the feeder gear causes a component-bearing tape to be fed through the feeder cartridge. A pickup head includes a vacuum nozzle to pick up the components from the tape and a rack gear to engage and drive the feeder gear of the feeder cartridge via translational motion of the pickup head when operatively disposed with respect to a selected feeder cartridge.

2. 发明申请

US20140267682A1 LINEAR/ANGULAR CORRECTION OF PICK-AND-PLACE HELD COMPONENT AND RELATED OPTICAL SUBSYSTEM 审中-公开
标题翻译： PICK和放置组件的线性/角度校正和相关的光学子系统
公开(公告)号：US20140267682A1
公开(公告)日：2014-09-18
申请号：US13838075
申请日：2013-03-15
申请人： JOHN S. YOUNGQUIST
发明人： JOHN S. YOUNGQUIST
IPC分类号： H05K13/04 , H04N7/18
CPC分类号： H05K13/0417 , H05K13/0409 , H05K13/0419 , H05K13/0812
摘要： A pick-and-place machine and method includes use of a passive component feeder cartridge including a feeder gear. Rotation of the feeder gear causes a component-bearing tape to be fed through the feeder cartridge. A pickup head includes a vacuum nozzle to pick up the components from the tape and a rack gear to engage and drive the feeder gear of the feeder cartridge via translational motion of the pickup head when operatively disposed with respect to a selected feeder cartridge.
摘要翻译：拾取和放置机器和方法包括使用包括进给齿轮的无源元件供给盒。进给齿轮的旋转会使一个部件承载带通过进料盒进给。拾取头包括一个真空喷嘴，用于从胶带上拾取部件和一个齿条，用于在相对于选定的进料盒操作地设置时通过拾取头的平移运动来接合和驱动进给盒的进料器齿轮。

3. 发明授权

US5502371A Storm monitor 失效
公开(公告)号：US5502371A
公开(公告)日：1996-03-26
申请号：US404750
申请日：1995-03-15
申请人： John S. Youngquist
发明人： John S. Youngquist
IPC分类号： G01W1/16
CPC分类号： G01W1/16
摘要： A storm monitoring apparatus and method is described wherein two H-field antennas are oriented with respect to the heading axis of an aircraft or the like at an angle of 45.degree.. The signals developed by these two antennas are picked-up by small R-F transformers which serve the inherent function of integrating the signals and extracting the H-field current component. A printed circuit board structuring of the two antennas provides for consistency of fabrication and reliability as well as compactness. The monitoring apparatus exhibits broad band frequency response to evaluate lightning strike rate to determine storm range and intensity. A computer control test utilizing diagnostic coils at the antenna carries out periodic testing of the performance of the device and a component such as a gravity switch provides an indication to the control system as to the orientation of mounting of the antenna on an aircraft. The outputs of the antennas are digitized and evaluated at a high rate and range information is developed from these digitized data in consequence of the transfer function of the atmosphere. For example, range is developed by an analysis of the decay of various frequency components emanating from a lightning burst. Select memory retention of the data is continuously provided such that the operator can look to immediately preceding storm evaluations to determine whether the condition in which flight is being made is one into worsening or improving weather.

4. 发明授权

US5500602A Storm monitor 失效
公开(公告)号：US5500602A
公开(公告)日：1996-03-19
申请号：US404896
申请日：1995-03-15
申请人： John S. Youngquist
发明人： John S. Youngquist
IPC分类号： G01W1/16
CPC分类号： G01W1/16
摘要： A storm monitoring apparatus and method is described wherein two H-field antennas are oriented with respect to the heading axis of an aircraft or the like at an angle of 45.degree.. The signals developed by these two antennas are picked-up by small R-F transformers which serve the inherent function of integrating the signals and extracting the H-field current component. A printed circuit board structuring of the two antennas provides for consistency of fabrication and reliability as well as compactness. The monitoring apparatus exhibits broad band frequency response to evaluate lightning strike rate to determine storm range and intensity. A computer control test utilizing diagnostic coils at the antenna carries out periodic testing of the performance of the device and a component such as a gravity switch provides an indication to the control system as to the orientation of mounting of the antenna on an aircraft. The outputs of the antennas are digitized and evaluated at a high rate and range information is developed from these digitized data in consequence of the transfer function of the atmosphere. For example, range is developed by an analysis of the decay of various frequency components emanating from a lightning burst. Select memory retention of the data is continuously provided such that the operator can look to immediately preceding storm evaluations to determine whether the condition in which flight is being made is one into worsening or improving weather.

5. 发明授权

US09549493B2 Passive feeder cartridge driven by pickup head 有权
标题翻译：由拾音头驱动的被动馈线盒
公开(公告)号：US09549493B2
公开(公告)日：2017-01-17
申请号：US13837727
申请日：2013-03-15
申请人： John S. Youngquist
发明人： John S. Youngquist
IPC分类号： H05K13/02 , H05K13/04 , G01D5/28 , G01D5/347
CPC分类号： H05K13/0417 , B23K1/0016 , B23K3/0638 , B23K26/0876 , B23K26/352 , B23K26/361 , B23K37/0235 , B23K2101/42 , G01D5/285 , G01D5/3473 , G05B11/01 , H05K13/021 , H05K13/0408 , H05K13/0409 , H05K13/0419 , H05K13/0812 , H05K13/086 , Y10T156/11 , Y10T156/19
摘要： A pick-and-place machine and method includes use of a passive component feeder cartridge including a feeder gear. Rotation of the feeder gear causes a component-bearing tape to be fed through the feeder cartridge. A pickup head includes a vacuum nozzle to pick up the components from the tape and a rack gear to engage and drive the feeder gear of the feeder cartridge via translational motion of the pickup head when operatively disposed with respect to a selected feeder cartridge.
摘要翻译：拾取和放置机器和方法包括使用包括进给齿轮的无源元件供给盒。进给齿轮的旋转会使一个部件承载带通过进料盒进给。拾取头包括一个真空喷嘴，用于从胶带上拾取部件和一个齿条，用于在相对于选定的进料盒操作地设置时通过拾取头的平移运动来接合和驱动进给盒的进料器齿轮。

6. 发明申请

US20140270473A1 VIRTUAL ASSEMBLY AND PRODUCT INSPECTION CONTROL PROCESSES 审中-公开
标题翻译：虚拟装配和产品检验控制程序
公开(公告)号：US20140270473A1
公开(公告)日：2014-09-18
申请号：US13839239
申请日：2013-03-15
申请人： JOHN S. YOUNGQUIST
发明人： JOHN S. YOUNGQUIST
IPC分类号： G06T19/00 , G06K9/62 , G06K9/64 , G06T7/00
CPC分类号： G06T7/001 , G06T7/0004 , G06T11/00 , G06T2207/10016 , G06T2207/30141 , H01L24/75 , H01L2224/75745 , H01L2224/75753 , H01L2224/75901 , H01L2924/12042 , H01L2924/12043 , H05K13/0408 , H05K13/0409 , H05K13/0417 , H05K13/0419 , H05K13/08 , H05K13/0812 , H05K13/0815 , H05K13/085 , H01L2924/00
摘要： A pick-and-place machine and method includes use of a passive component feeder cartridge including a feeder gear. Rotation of the feeder gear causes a component-bearing tape to be fed through the feeder cartridge. A pickup head includes a vacuum nozzle to pick up the components from the tape and a rack gear to engage and drive the feeder gear of the feeder cartridge via translational motion of the pickup head when operatively disposed with respect to a selected feeder cartridge.
摘要翻译：拾取和放置机器和方法包括使用包括进给齿轮的无源元件供给盒。进给齿轮的旋转会使一个部件承载带通过进料盒进给。拾取头包括一个真空喷嘴，用于从胶带上拾取部件和一个齿条，用于在相对于选定的进料盒操作地设置时通过拾取头的平移运动来接合和驱动进给盒的进料器齿轮。

7. 发明申请

US20090306839A1 Aircraft monitoring equipment 有权
标题翻译：飞机监控设备
公开(公告)号：US20090306839A1
公开(公告)日：2009-12-10
申请号：US12385395
申请日：2009-04-07
申请人： John S. Youngquist , John W. Toulmin
发明人： John S. Youngquist , John W. Toulmin
IPC分类号： G06F19/00 , F02P17/00 , G01K7/02 , G01M15/06
CPC分类号： G01K7/021 , G01K15/00 , G09G2380/12
摘要： An aircraft monitoring system uses aircraft engine and system transducers to monitor critical engine and aircraft system parameters. Simple controls and graphical user interfaces facilitate the display of different kinds of critical information to the pilot. Such data may also be recorded for later downloading and analysis.
摘要翻译：飞机监控系统使用飞机发动机和系统换能器来监测关键发动机和飞机系统参数。简单的控件和图形用户界面便于向飞行员显示不同种类的关键信息。这些数据也可以记录下来进行下载和分析。

8. 发明授权

US07054760B2 Apparatus and method for generating and displaying fuel flow information in a GPS-equipped vehicle 有权
标题翻译：在配备GPS的车辆中生成和显示燃料流量信息的装置和方法
公开(公告)号：US07054760B2
公开(公告)日：2006-05-30
申请号：US10385568
申请日：2003-03-12
申请人： John S. Youngquist
发明人： John S. Youngquist
IPC分类号： G06F13/10
CPC分类号： G01F15/063 , G01F25/0007
摘要： Fuel flow information is generated in an engine compartment and transmitted for display on the fuel page(s) of a GPS signal receiver located in view of a vehicle operator. A fuel transducer coupled to a pre-programmed micro-controller are provided as an integrated single unit in the engine compartment of the vehicle (e.g., an aircraft). The integrated transducer/micro-controller unit outputs RS232 fuel flow signals to the GPS signal receiver without requiring any extra panel space. Since the transducer/micro-controller is already pre-programmed to compensate for the proportionality or “K” factor, no further calibration or compensation programming is needed at installation time (or when one composite transducer/computer unit is substituted for another). Separate transducer/micro-controller power supply and grounding connections suppress common mode noise. A blinking LED power/fuel flow visual display on the unit in the engine compartment helps trouble shoot power and/or transducer problems.
摘要翻译：燃料流量信息在发动机舱中产生并被发送以在位于车辆驾驶员的GPS信号接收器的燃料页面上显示。耦合到预编程的微控制器的燃料换能器作为车辆（例如，飞行器）的发动机室中的集成单个单元提供。集成的传感器/微控制器单元将RS232燃油流量信号输出到GPS信号接收器，而不需要任何额外的面板空间。由于传感器/微控制器已经被预先编程以补偿比例或“K”因子，所以在安装时（或者当一个复合传感器/计算机单元被另一个替代时）不需要进一步的校准或补偿编程。单独的传感器/微控制器电源和接地连接可以抑制共模噪声。发动机舱中的单元上的闪烁的LED电源/燃油流动视觉显示屏有助于解决电源和/或换能器问题。

9. 发明授权

US5408175A Storm monitor 失效
标题翻译：风暴监视器
公开(公告)号：US5408175A
公开(公告)日：1995-04-18
申请号：US115183
申请日：1993-08-31
申请人： John S. Youngquist
发明人： John S. Youngquist
IPC分类号： G01W1/16
CPC分类号： G01W1/16
摘要： A storm monitoring apparatus and method is described wherein two H-field antennas are oriented with respect to the heading axis of an aircraft or the like at an angle of 45.degree.. The signals developed by these two antennas are picked-up by small R-F transformers which serve the inherent function of integrating the signals and extracting the H-field current component. A printed circuit board structuring of the two antennas provides for consistency of fabrication and reliability as well as compactness. The monitoring apparatus exhibits broad band frequency response to evaluate lightning strike rate to determine storm range and intensity. A computer control test utilizing diagnostic coils at the antenna carries out periodic testing of the performance of the device and a component such as a gravity switch provides an indication to the control system as to the orientation of mounting of the antenna on an aircraft. The outputs of the antennas are digitized and evaluated at a high rate and range information is developed from these digitized data in consequence of the transfer function of the atmosphere. For example, range is developed by an analysis of the decay of various frequency components emanating from a lightning burst. Select memory retention of the data is continuously provided such that the operator can look to immediately preceding storm evaluations to determine whether the condition in which flight is being made is one into worsening or improving weather.
摘要翻译：描述了一种风暴监测装置和方法，其中两个H场天线相对于飞机等的45°的角度定向。由这两个天线开发的信号由小的R-F变压器拾取，其用于集成信号和提取H场电流分量的固有功能。构成两个天线的印刷电路板提供制造和可靠性以及紧凑性的一致性。监测装置展现出宽带频率响应，以评估雷击速率，以确定风暴范围和强度。在天线处利用诊断线圈的计算机控制测试执行对装置的性能的周期性测试，并且诸如重力开关的部件向控制系统提供关于在飞机上安装天线的方向的指示。天线的输出以高速数字化和评估，并且由于大气的传递函数，从这些数字化数据开发范围信息。例如，通过对从闪电发生的各种频率分量的衰减的分析来开发范围。选择持续提供数据的记忆保持，以便操作者可以查看紧接在前的风暴评估，以确定是否正在进行飞行的状况是恶化或改善天气之一。

10. 发明授权

US10269256B2 Aircraft landing aid with rangefinder 有权
公开(公告)号：US10269256B2
公开(公告)日：2019-04-23
申请号：US15220971
申请日：2016-07-27
申请人： John S. Youngquist
发明人： John S. Youngquist
IPC分类号： G05D1/06 , G08G5/02 , B64D45/08 , G01S17/02 , G01S17/10 , G01S17/32 , G01S17/93 , G01S7/481
摘要： A landing aid is removably attachable to an aircraft to provide precise measurements of distance and descent rate to ground which are conveyed to the pilot in real time via sound such that the pilot does not have to look away from the flight path ahead during the landing process. The landing aid may generate energy waves that pass from an interior portion of the aircraft to an area exterior of the aircraft through a window of the aircraft. A reflector may be positioned on an exterior portion of the aircraft to direct the energy waves toward the ground. The energy waves reflected back towards the aircraft by the ground permit a distance from the aircraft to the ground and a descent rate to be determined and concurrently output to a pilot via audible signals.

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