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1. 发明申请

US20140082177A1 ASYNCHRONOUS REPORTING SYSTEM 有权
标题翻译：异常报告系统
公开(公告)号：US20140082177A1
公开(公告)日：2014-03-20
申请号：US13621093
申请日：2012-09-15
申请人： Patrick R. Lemire , Cherry Lv , Thomas Paul Schmit , Jeffrey Stuart , Bo Wang , James Kern , William R. Blum , Philip J. Ferro
发明人： Patrick R. Lemire , Cherry Lv , Thomas Paul Schmit , Jeffrey Stuart , Bo Wang , James Kern , William R. Blum , Philip J. Ferro
IPC分类号： G06F15/173
CPC分类号： F24F11/30 , F24F11/52 , F24F11/62 , F24F2110/50 , H04L12/2803 , H04L67/10 , H04L67/12 , H04L67/125
摘要： An asynchronous reporting mechanism for a remote device in a heating, ventilation and air conditioning environment. Using gateway information, such as a device address, report information may be sent to the user account, or using another approach, the information may be sent directly to the user. An asynchronous message may be sent without user intervention or request.
摘要翻译：用于加热，通风和空调环境中远程设备的异步报告机制。使用诸如设备地址的网关信息可以将报告信息发送到用户帐户，或者使用另一种方法，该信息可以直接发送给用户。可以发送异步消息而无需用户干预或请求。

2. 发明授权

US09705962B2 Asynchronous reporting system 有权
公开(公告)号：US09705962B2
公开(公告)日：2017-07-11
申请号：US13621093
申请日：2012-09-15
申请人： Patrick R. Lemire , Cherry Lv , Thomas Paul Schmit , Jeffrey Stuart , Bo Wang , James Kern , William R. Blum , Philip J. Ferro
发明人： Patrick R. Lemire , Cherry Lv , Thomas Paul Schmit , Jeffrey Stuart , Bo Wang , James Kern , William R. Blum , Philip J. Ferro
IPC分类号： G06F15/173 , H04L29/08 , F24F11/00
CPC分类号： F24F11/30 , F24F11/52 , F24F11/62 , F24F2110/50 , H04L12/2803 , H04L67/10 , H04L67/12 , H04L67/125
摘要： An asynchronous reporting mechanism for a remote device in a heating, ventilation and air conditioning environment. Using gateway information, such as a device address, report information may be sent to the user account, or using another approach, the information may be sent directly to the user. An asynchronous message may be sent without user intervention or request.

3. 发明申请

US20050127241A1 Flight control actuation system 失效
标题翻译：飞行控制驱动系统
公开(公告)号：US20050127241A1
公开(公告)日：2005-06-16
申请号：US10874729
申请日：2004-06-22
申请人： Paul Wingett , Louie Gaines , Paul Evans , James Kern
发明人： Paul Wingett , Louie Gaines , Paul Evans , James Kern
IPC分类号： B64C13/42 , B64C13/50 , B64C5/00
CPC分类号： B64C13/50 , B64C13/42
摘要： A flight control actuation system comprises a controller, electromechanical actuator and a pneumatic actuator. During normal operation, only the electromechanical actuator is needed to operate a flight control surface. When the electromechanical actuator load level exceeds 40 amps positive, the controller activates the pneumatic actuator to offset electromechanical actuator loads to assist the manipulation of flight control surfaces. The assistance from the pneumatic load assist actuator enables the use of an electromechanical actuator that is smaller in size and mass, requires less power, needs less cooling processes, achieves high output forces and adapts to electrical current variations. The flight control actuation system is adapted for aircraft, spacecraft, missiles, and other flight vehicles, especially flight vehicles that are large in size and travel at high velocities.
摘要翻译：飞行控制致动系统包括控制器，机电致动器和气动致动器。在正常操作期间，仅需要机电致动器来操作飞行控制表面。当机电致动器负载水平超过40安培正时，控制器激活气动执行器以抵消机电执行器负载，以帮助操纵飞行控制表面。来自气动负载辅助致动器的帮助使得能够使用尺寸和质量更小的机电致动器，需要更少的功率，更少的冷却过程，实现高输出力并适应于电流变化。飞行控制致动系统适用于飞机，航天器，导弹和其他飞行器，特别是大型飞行器和高速行驶的飞行器。

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