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41. 发明申请

US20100179595A1 Intervertebral Implant Devices and Methods for Insertion Thereof 有权
标题翻译：椎间植入装置及其插入方法
公开(公告)号：US20100179595A1
公开(公告)日：2010-07-15
申请号：US12685618
申请日：2010-01-11
申请人： Michael R. Jackson , Russell M. Pietila , Qi-Bin Bao , Wade DePas , Jeffrey L. Trudeau
发明人： Michael R. Jackson , Russell M. Pietila , Qi-Bin Bao , Wade DePas , Jeffrey L. Trudeau
IPC分类号： A61B17/70 , A61B17/56
CPC分类号： A61B17/7065 , A61B17/7053 , A61B17/7068 , A61B2017/0256
摘要： Implant apparatuses are provided for being inserted between adjacent vertebral bone portions and maintaining mechanical engagement with the vertebral bone portions. The implant apparatuses are generally constructed to be inserted in an insertion orientation and pivoted between the vertebral bone portions to an implanted orientation. The implant apparatuses are further secured in the implanted orientation to maintain engagement with the adjacent vertebral bone portions.
摘要翻译：提供植入装置用于插入在相邻的椎骨部分之间并保持与椎骨部分的机械接合。植入装置通常被构造成以插入方向插入并且在椎骨部分之间枢转到植入方向。植入装置进一步固定在植入方向上以保持与相邻的椎骨部分的接合。

42. 发明授权

US06507782B1 Aircraft control system for reaching a waypoint at a required time of arrival 有权
标题翻译：飞机控制系统，在达到所需的时间到达航点
公开(公告)号：US06507782B1
公开(公告)日：2003-01-14
申请号：US09855861
申请日：2001-05-14
申请人： Jim R. Rumbo , Michael R. Jackson , Brian E. O'Laughlin
发明人： Jim R. Rumbo , Michael R. Jackson , Brian E. O'Laughlin
IPC分类号： G06F1550
CPC分类号： G05D1/0202 , G05D1/0005
摘要： The instant invention provides a system and method for controlling the flight of an aircraft to meet an RTA. The system comprises a speed profile generator that communicates with a trajectory generator to produce a speed profile signal that enables the aircraft to reach a waypoint substantially at a predetermined time. In the system of the instant invention, the speed profile generator receives a nominal speed command signal, a time error signal and a sensitivity signal. Based on these inputs, the speed profile generator produces a speed profile signal. The trajectory generator receives the speed profile signal and a required time of arrival signal. Based on these signals, the trajectory generator produces a time error signal and a sensitivity signal. This sensitivity signal represents the sensitivity of the time error signal to changes in the speed profile signal.
摘要翻译：本发明提供了一种用于控制飞行器满足RTA的飞行的系统和方法。该系统包括与轨迹发生器通信以产生速度分布信号的速度曲线发生器，该速度曲线信号使飞机能够在预定时间内达到航点。在本发明的系统中，速度曲线发生器接收标称速度指令信号，时间误差信号和灵敏度信号。基于这些输入，速度曲线生成器产生速度曲线信号。轨迹发生器接收速度曲线信号和所需的到达时间信号。基于这些信号，轨迹发生器产生时间误差信号和灵敏度信号。该灵敏度信号表示时间误差信号对速度分布信号变化的灵敏度。

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