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1. 发明申请

WO2013169320A2 AUTOPILOT AND METHODS 审中-公开
标题翻译：自动化和方法
公开(公告)号：WO2013169320A2
公开(公告)日：2013-11-14
申请号：PCT/US2013025456
申请日：2013-02-08
申请人： MERLIN TECHNOLOGY INC
发明人： ALBION NICOLAS , BARTEL MARK , FEIFEL MARC , MARVIN MARK , MERCER JOHN
CPC分类号： B64C27/57 , B64C13/18 , B64C13/42 , B64C27/56 , B64C27/59 , B64C27/64 , B64C27/68 , G05D1/0077 , G05D1/0816 , G05D1/0858 , G05D1/102 , Y02T50/44
摘要： A helicopter autopilot system includes an inner loop for attitude hold for the flight of the helicopter including a given level of redundancy applied to the inner loop. An outer loop is configured for providing a navigation function with respect to the flight of the helicopter including a different level of redundancy than the inner loop. An actuator provides a braking force on a linkage that serves to stabilize the flight of the helicopter during a power failure. The actuator is electromechanical and receives electrical drive signals to provide automatic flight control of the helicopter without requiring a hydraulic assistance system in the helicopter. The autopilot can operate the helicopter in a failed mode of the hydraulic assistance system. A number of flight modes are described with associated sensor inputs including rate based and true attitude modes.
摘要翻译：直升机自动驾驶系统包括用于直升机飞行的姿态保持的内循环，包括施加到内循环的给定水平的冗余。外部环路被配置为提供关于直升机的飞行的导航功能，其包括与内部循环不同的冗余级别。致动器在联动装置上提供制动力，用于在停电期间稳定直升机的飞行。致动器是机电的并且接收电驱动信号以提供直升机的自动飞行控制，而不需要直升机中的液压辅助系统。自动驾驶仪可以在液压辅助系统的故障模式下操作直升机。使用相关的传感器输入描述多个飞行模式，包括基于速率和真实姿态模式。

2. 发明申请

WO2013172885A3 AUTOPILOT SYSTEM, COMPONENTS AND METHODS 审中-公开
标题翻译：自动化系统，组件和方法
公开(公告)号：WO2013172885A3
公开(公告)日：2014-02-13
申请号：PCT/US2013025458
申请日：2013-02-09
申请人： MERLIN TECHNOLOGY INC
发明人： ALBION NICOLAS , FEIFEL MARC , MARVIN MARK , MERCER JOHN
IPC分类号： B64C27/04 , G05D1/00
CPC分类号： B64C27/57 , B64C13/18 , B64C13/42 , B64C27/56 , B64C27/59 , B64C27/64 , B64C27/68 , G05D1/0077 , G05D1/0816 , G05D1/0858 , G05D1/102 , Y02T50/44
摘要： An autopilot actuator includes first and second motors each including a rotatable motor output shaft such that either one or both of the motors can drive an actuator output shaft. An autopilot main unit enclosure is removably mounted to the helicopter proximate to a cyclic control and commonly houses autopilot actuators as well as main autopilot electronics. A cyclic vibration isolator is removably supported by an actuator shaft for corotation and coupled to the cyclic control to attenuate a cyclic vibration frequency at the actuator shaft while output rotations of the actuator shaft below a resonant frequency are coupled to the cyclic control. A force limited link includes first and second ends and a variable length between. The force limited link having a relaxed length when less than an unseating force is applied and the variable length changes when an applied force exceeds the unseating force to permit pilot override.
摘要翻译：自动驾驶执行器包括第一和第二电动机，每个电动机包括可旋转的电动机输出轴，使得电动机中的一个或两个可以驱动致动器输出轴。自动驾驶仪主机壳体可拆卸地安装在靠近循环控制的直升机上，并且通常容纳自动驾驶执行器以及主要的自动驾驶仪电子装置。循环式隔振器由致动器轴可移除地支撑，用于共旋转并且耦合到循环控制以衰减致动器轴上的循环振动频率，而致动器轴的低于谐振频率的转速被耦合到循环控制。力限制连杆包括第一和第二端以及两者之间的可变长度。当施加小于放开力的力时，力限制连杆具有松弛的长度，并且当所施加的力超过转动力以允许引导超驰时，可变长度改变。

3. 发明专利

HK1202846A1 AUTOPILOT SYSTEM, COMPONENTS AND METHODS 未知
公开(公告)号：HK1202846A1
公开(公告)日：2015-10-09
申请号：HK15103393
申请日：2015-04-06
申请人： MERLIN TECHNOLOGY INC
发明人： ALBION NICOLAS , FEIFEL MARC , MARVIN MARK , MERCER JOHN
IPC分类号： B64C20060101 , G05D20060101
摘要： A helicopter autopilot system includes an inner loop for attitude hold for the flight of the helicopter including a given level of redundancy applied to the inner loop. An outer loop is configured for providing a navigation function with respect to the flight of the helicopter including a different level of redundancy than the inner loop. An actuator provides a braking force on a linkage that serves to stabilize the flight of the helicopter during a power failure. The actuator is electromechanical and receives electrical drive signals to provide automatic flight control of the helicopter without requiring a hydraulic assistance system in the helicopter. The autopilot can operate the helicopter in a failed mode of the hydraulic assistance system. A number of flight modes are described with associated sensor inputs including rate based and true attitude modes.

4. 发明专利

HK1254894A1 自動駕駛儀及其方法未知
公开(公告)号：HK1254894A1
公开(公告)日：2019-08-02
申请号：HK18113964
申请日：2015-06-05
申请人： MERLIN TECHNOLOGY INC
发明人： ALBION NICOLAS , BARTEL MARK , FEIFEL MARC , MARVIN MARK , MERCER JOHN
IPC分类号： G05D20060101 , B64C20060101

5. 发明公开

EP2812764A4 AUTOPILOT AND METHODS 有权
标题翻译： AUTO PILOT和程序
公开(公告)号：EP2812764A4
公开(公告)日：2016-07-06
申请号：EP13787117
申请日：2013-02-08
申请人： MERLIN TECHNOLOGY INC
发明人： ALBION NICOLAS , BARTEL MARK , FEIFEL MARC , MARVIN MARK , MERCER JOHN
IPC分类号： B64C13/18 , B64C13/42 , B64C27/04 , B64C27/56 , B64C27/57 , B64C27/64 , B64C27/68 , G05D1/08 , G05D1/10
CPC分类号： B64C27/57 , B64C13/18 , B64C13/42 , B64C27/56 , B64C27/59 , B64C27/64 , B64C27/68 , G05D1/0077 , G05D1/0816 , G05D1/0858 , G05D1/102 , Y02T50/44
摘要： A helicopter autopilot system includes an inner loop for attitude hold for the flight of the helicopter including a given level of redundancy applied to the inner loop. An outer loop is configured for providing a navigation function with respect to the flight of the helicopter including a different level of redundancy than the inner loop. An actuator provides a braking force on a linkage that serves to stabilize the flight of the helicopter during a power failure. The actuator is electromechanical and receives electrical drive signals to provide automatic flight control of the helicopter without requiring a hydraulic assistance system in the helicopter. The autopilot can operate the helicopter in a failed mode of the hydraulic assistance system. A number of flight modes are described with associated sensor inputs including rate based and true attitude modes.

6. 发明公开

EP2812245A4 AUTOPILOT SYSTEM, COMPONENTS AND METHODS 审中-公开
标题翻译：自动驾驶系统和组件及其方法
公开(公告)号：EP2812245A4
公开(公告)日：2015-10-07
申请号：EP13790956
申请日：2013-02-09
申请人： MERLIN TECHNOLOGY INC
发明人： ALBION NICOLAS , FEIFEL MARC , MARVIN MARK , MERCER JOHN
IPC分类号： B64C27/04 , G05D1/00
CPC分类号： B64C27/57 , B64C13/18 , B64C13/42 , B64C27/56 , B64C27/59 , B64C27/64 , B64C27/68 , G05D1/0077 , G05D1/0816 , G05D1/0858 , G05D1/102 , Y02T50/44

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