专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20070291427A1 AIRCRAFT APPLICABLE CIRCUIT IMBALANCE DETECTION AND CIRCUIT INTERRUPTER AND PACKAGING THEREOF 有权
公开(公告)号：US20070291427A1
公开(公告)日：2007-12-20
申请号：US11846962
申请日：2007-08-29
申请人： Ronald Bax , Rudy Rusali , Timothy King
发明人： Ronald Bax , Rudy Rusali , Timothy King
IPC分类号： H02H3/00
CPC分类号： H01H83/14 , H01H3/001 , H01H83/04 , H01H83/144 , H02H1/06 , H02H3/04 , H02H3/05 , H02H3/105 , H02H3/32 , H02H3/33 , H02H3/347 , H02H7/09
摘要： The aircraft applicable current imbalance detection and circuit interrupter interrupts an electrical circuit when a current imbalance is sensed. The current imbalance detection and circuit interrupter includes a housing, power supplies, a sensor system for sensing a current imbalance at the line side of the electrical circuit, a logic controller and a power controller including a power relay having contacts capable of surviving carry-break and make-carry-break types of ground fault conditions at anticipated current levels. At power up, the device performs a test to confirm that none of the relay contacts have failed in a closed position, and to check whether a switching FET which controls the relay coil has shorted.

2. 发明申请

US20070291428A1 AIRCRAFT APPLICABLE CIRCUIT IMBALANCE DETECTION AND CIRCUIT INTERRUPTER AND PACKAGING THEREOF 有权
标题翻译：飞机适用电路不平衡检测与电路中断及其包装
公开(公告)号：US20070291428A1
公开(公告)日：2007-12-20
申请号：US11847071
申请日：2007-08-29
申请人： Ronald Bax , Rudy Rusali , Timothy King
发明人： Ronald Bax , Rudy Rusali , Timothy King
IPC分类号： H02H3/00
CPC分类号： H01H83/14 , H01H3/001 , H01H83/04 , H01H83/144 , H02H1/06 , H02H3/04 , H02H3/05 , H02H3/105 , H02H3/32 , H02H3/33 , H02H3/347 , H02H7/09
摘要： The aircraft applicable current imbalance detection and circuit interrupter interrupts an electrical circuit when a current imbalance is sensed. The current imbalance detection and circuit interrupter includes a housing, power supplies, a sensor system for sensing a current imbalance at the line side of the electrical circuit, a logic controller and a power controller including a power relay having contacts capable of surviving carry-break and make-carry-break types of ground fault conditions at anticipated current levels. At power up, the device performs a test to confirm that none of the relay contacts have failed in a closed position, and to check whether a switching FET which controls the relay coil has shorted.
摘要翻译：当感测到电流不平衡时，飞机适用的电流不平衡检测和电路断路器中断电路。电流不平衡检测和电路断路器包括壳体，电源，用于感测电路线路侧的电流不平衡的传感器系统，逻辑控制器和功率控制器，其包括具有能够存活携带断点的触点的功率继电器以及预期目前水平的接地故障类型。上电时，器件进行测试以确认没有继电器触点在闭合位置发生故障，并检查控制继电器线圈的开关FET是否短路。

3. 发明申请

US20070139985A1 CURRENT FAULT DETECTOR AND CIRCUIT INTERRUPTER AND PACKAGING THEREOF 有权
标题翻译：电流故障检测器和电路中断器及其包装
公开(公告)号：US20070139985A1
公开(公告)日：2007-06-21
申请号：US11678496
申请日：2007-02-23
申请人： Ronald Bax , Rudy Rusali , Timothy King
发明人： Ronald Bax , Rudy Rusali , Timothy King
IPC分类号： H02M7/32
CPC分类号： H01H83/226 , H02H1/06 , H02H3/04 , H02H3/105 , H02H3/335 , H02H3/347
摘要： A power controller is positioned within a current path between the line side and the load side of an electrical circuit. The power controller closes the current path in the presence of a control supply and opens the current path in the absence of the control supply. A power supply electrically connected to the current path provides the control supply. A sensor system receives power from the power supply, monitors the current in the current path and outputs a sensor signal indicative of a current condition within the current path. A logic controller also receives power from the power supply, receives the sensor signal and removes the control supply from the power controller when the sensor signal does not satisfy an established criteria. The sensor system may include one or both of an imbalance sensor for monitoring the current balance among two or more electrical lines and over-current sensors for monitoring current in individual lines.
摘要翻译：功率控制器位于电路的线路侧和负载侧之间的电流路径内。功率控制器在存在控制电源时关闭电流通路，并在没有控制电源的情况下打开电流通路。电连接到电流路径的电源提供控制电源。传感器系统从电源接收电力，监视当前路径中的电流，并输出指示当前路径内的当前状态的传感器信号。当传感器信号不满足既定标准时，逻辑控制器还从电源接收电力，接收传感器信号并从功率控制器中去除控制电源。传感器系统可以包括不平衡传感器中的一个或两个，用于监测两个或更多个电线之间的电流平衡以及用于监视各个线路中的电流的过电流传感器。

4. 发明申请

US20060028779A1 Current fault detector and circuit interrupter and packaging thereof 有权
公开(公告)号：US20060028779A1
公开(公告)日：2006-02-09
申请号：US11242246
申请日：2005-10-03
申请人： Ronald Bax , Rudy Rusali , Timothy King
发明人： Ronald Bax , Rudy Rusali , Timothy King
IPC分类号： H02H3/08
CPC分类号： H01H83/226 , H02H1/06 , H02H3/04 , H02H3/105 , H02H3/335 , H02H3/347
摘要： A power controller is positioned within a current path between the line side and the load side of an electrical circuit. The power controller closes the current path in the presence of a control supply and opens the current path in the absence of the control supply. A power supply electrically connected to the current path provides the control supply. A sensor system receives power from the power supply, monitors the current in the current path and outputs a sensor signal indicative of a current condition within the current path. A logic controller also receives power from the power supply, receives the sensor signal and removes the control supply from the power controller when the sensor signal does not satisfy an established criteria. The sensor system may include one or both of an imbalance sensor for monitoring the current balance among two or more electrical lines and over-current sensors for monitoring current in individual lines.

5. 发明申请

US20050018369A1 Aircraft applicable circuit imbalance detection and circuit interrupter and packaging thereof 有权
标题翻译：飞机适用电路不平衡检测及电路断路器及其包装
公开(公告)号：US20050018369A1
公开(公告)日：2005-01-27
申请号：US10860387
申请日：2004-06-03
申请人： Ronald Bax , Rudy Rusali , Timothy King
发明人： Ronald Bax , Rudy Rusali , Timothy King
IPC分类号： H02H1/06 , H02H3/00 , H02H3/04 , H02H3/05 , H02H3/10 , H02H3/33 , H02H3/347
CPC分类号： H01H83/14 , H01H3/001 , H01H83/04 , H01H83/144 , H02H1/06 , H02H3/04 , H02H3/05 , H02H3/105 , H02H3/32 , H02H3/33 , H02H3/347 , H02H7/09
摘要： The aircraft applicable current imbalance detection and circuit interrupter interrupts an electrical circuit when a current imbalance is sensed. The current imbalance detection and circuit interrupter includes a housing, power supplies, a sensor system for sensing a current imbalance at the line side of the electrical circuit, a logic controller and a power controller including a power relay having contacts capable of surviving carry-break and make-carry-break types of ground fault conditions at anticipated current levels. At power up, the device performs a test to confirm that none of the relay contacts have failed in a closed position, and to check whether a switching FET which controls the relay coil has shorted.
摘要翻译：当感测到电流不平衡时，飞机适用的电流不平衡检测和电路断路器中断电路。电流不平衡检测和电路断路器包括壳体，电源，用于感测电路线路侧的电流不平衡的传感器系统，逻辑控制器和功率控制器，其包括具有能够存活携带断点的触点的功率继电器以及预期目前水平的接地故障类型。上电时，器件进行测试以确认没有继电器触点在闭合位置发生故障，并检查控制继电器线圈的开关FET是否短路。

6. 发明申请

US20080062592A1 AIRCRAFT APPLICABLE CURRENT IMBALANCE DETECTION AND CIRCUIT INTERRUPTER AND PACKAGING THEROF 有权
标题翻译：航空器适用的电流不平衡检测和电路中断器及其包装
公开(公告)号：US20080062592A1
公开(公告)日：2008-03-13
申请号：US11931803
申请日：2007-10-31
申请人： Ronald Bax
发明人： Ronald Bax
IPC分类号： H02H3/00
CPC分类号： H02H3/347 , H02H1/0007 , H02H1/06 , H02H3/04 , H02H3/105
摘要： The aircraft applicable current imbalance detection and circuit interrupter interrupts an electrical circuit when a current imbalance is sensed. The current imbalance detection and circuit interrupter includes a housing, power supplies, a sensor for sensing a current imbalance at the line side of the electrical circuit, a logic controller and a power controller. In a preferred embodiment, the invention can also include a fault indicator, a press to test switch and a reset switch. The power supplies provide power to the sensor, logic controller, and the power controller. The logic controller receives input from the sensor and the relay control signal, and the power controller receives input from the logic controller, and interrupts power to the load side of the electrical circuit when the sensor senses a current imbalance. Power interruption due to a sensed current imbalance is maintained until the line side power source is cycled. The circuit interrupter is preferably autonomous, requiring no additional signals, inputs, wiring or sources of power. The current imbalance detection and circuit interrupter is packaged in a configuration integral with the power controller, thus easing retrofit with the improved aircraft applicable current imbalance detection and circuit interrupter.
摘要翻译：当感测到电流不平衡时，飞机适用的电流不平衡检测和电路断路器中断电路。电流不平衡检测和断路器包括壳体，电源，用于感测电路线路侧的电流不平衡的传感器，逻辑控制器和功率控制器。在优选实施例中，本发明还可以包括故障指示器，按压测试开关和复位开关。电源为传感器，逻辑控制器和电源控制器提供电源。逻辑控制器接收来自传感器和继电器控制信号的输入，并且功率控制器接收来自逻辑控制器的输入，并且当传感器感测到电流不平衡时中断到电路的负载侧的电力。由于感测到的电流不平衡导致的电源中断被维持直到线路侧电源循环。电路断路器优选是自主的，不需要额外的信号，输入，布线或电源。目前的不平衡检测和电路断路器与功率控制器集成在一起，从而可以通过改进的飞机适用的电流不平衡检测和电路断路器进行改造。

7. 发明申请

US20050146818A1 Aircraft applicable current imbalance detection and circuit interrupter and packaging thereof 有权
标题翻译：飞机适用的电流不平衡检测和断路器及其包装
公开(公告)号：US20050146818A1
公开(公告)日：2005-07-07
申请号：US10967482
申请日：2004-10-18
申请人： Ronald Bax
发明人： Ronald Bax
IPC分类号： H01H83/02 , H01H83/14 , H02H1/06 , H02H3/04 , H02H3/10 , H02H3/347 , H02H7/26 , H02H3/00
CPC分类号： H02H3/347 , H02H1/0007 , H02H1/06 , H02H3/04 , H02H3/105
摘要： The aircraft applicable current imbalance detection and circuit interrupter interrupts an electrical circuit when a current imbalance is sensed. The current imbalance detection and circuit interrupter includes a housing, power supplies, a sensor for sensing a current imbalance at the line side of the electrical circuit, a logic controller and a power controller. In a preferred embodiment, the invention can also include a fault indicator, a press to test switch and a reset switch. The power supplies provide power to the sensor, logic controller, and the power controller. The logic controller receives input from the sensor and the relay control signal, and the power controller receives input from the logic controller, and interrupts power to the load side of the electrical circuit when the sensor senses a current imbalance. Power interruption due to a sensed current imbalance is maintained until the line side power source is cycled. The circuit interrupter is preferably autonomous, requiring no additional signals, inputs, wiring or sources of power. The current imbalance detection and circuit interrupter is packaged in a configuration integral with the power controller, thus easing retrofit with the improved aircraft applicable current imbalance detection and circuit interrupter.
摘要翻译：当感测到电流不平衡时，飞机适用的电流不平衡检测和电路断路器中断电路。电流不平衡检测和断路器包括壳体，电源，用于感测电路线路侧的电流不平衡的传感器，逻辑控制器和功率控制器。在优选实施例中，本发明还可以包括故障指示器，按压测试开关和复位开关。电源为传感器，逻辑控制器和电源控制器提供电源。逻辑控制器接收来自传感器和继电器控制信号的输入，并且功率控制器接收来自逻辑控制器的输入，并且当传感器感测到电流不平衡时中断到电路的负载侧的电力。由于感测到的电流不平衡导致的电源中断被维持直到线路侧电源循环。电路断路器优选是自主的，不需要额外的信号，输入，布线或电源。目前的不平衡检测和电路断路器与功率控制器集成在一起，从而可以通过改进的飞机适用的电流不平衡检测和电路断路器进行改造。

8. 发明申请

US20060250730A1 Aircraft applicable current imbalance detection and circuit interrupter and packaging thereof 有权
公开(公告)号：US20060250730A1
公开(公告)日：2006-11-09
申请号：US11413737
申请日：2006-04-28
申请人： Ronald Bax
发明人： Ronald Bax
IPC分类号： H02H3/00
CPC分类号： H02H3/347 , H02H1/0007 , H02H1/06 , H02H3/04 , H02H3/105
摘要： The aircraft applicable current imbalance detection and circuit interrupter interrupts an electrical circuit when a current imbalance is sensed. The current imbalance detection and circuit interrupter includes a housing, power supplies, a sensor for sensing a current imbalance at the line side of the electrical circuit, a logic controller and a power controller. In a preferred embodiment, the invention can also include a fault indicator, a press to test switch and a reset switch. The power supplies provide power to the sensor, logic controller, and the power controller. The logic controller receives input from the sensor and the relay control signal, and the power controller receives input from the logic controller, and interrupts power to the load side of the electrical circuit when the sensor senses a current imbalance. Power interruption due to a sensed current imbalance is maintained until the line side power source is cycled. The circuit interrupter is preferably autonomous, requiring no additional signals, inputs, wiring or sources of power. The current imbalance detection and circuit interrupter is packaged in a configuration integral with the power controller, thus easing retrofit with the improved aircraft applicable current imbalance detection and circuit interrupter.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式