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1. 发明授权

US10106249B2 Method of operating aircraft drive to move an aircraft under adverse ground conditions 有权
公开(公告)号：US10106249B2
公开(公告)日：2018-10-23
申请号：US13983561
申请日：2012-02-03
申请人： Jonathan S. Edelson , Isaiah W. Cox , Neal Gilleran , Scott Perkins
发明人： Jonathan S. Edelson , Isaiah W. Cox , Neal Gilleran , Scott Perkins
IPC分类号： B64C25/40
摘要： A method is provided for restoring mobility to an aircraft equipped with at least one self-propelled drive wheel powered by a driver when the aircraft has been rendered immobile as a result of one or more wheel tires adhering to and becoming stuck to tarmac or another ground surface. The method uses forces generated by the cooperative action of the wheel driver, the aircraft steering, and the aircraft braking system to release adherent tires of each set of main wheels and/or nose gear wheels by applying differential force to one set of wheels at a time to release any adherent tires so that the aircraft is able to move on the ground surface and travel in a desired direction at a desired speed.

2. 发明授权

US09789957B2 Load transfer in a powered aircraft drive wheel 有权
公开(公告)号：US09789957B2
公开(公告)日：2017-10-17
申请号：US14449138
申请日：2014-07-31
申请人： Isaiah W. Cox , Scott Perkins
发明人： Isaiah W. Cox , Scott Perkins
IPC分类号： B64C25/50 , B64C25/40
CPC分类号： B64C25/405 , Y02T50/823 , Y10T29/49716
摘要： An efficient system and method are provided wherein aircraft may be retrofitted with non-engine drive means controllable to power landing gear wheels to move the aircraft autonomously during ground movement without engines or tow vehicles so that existing landing gear structures are employed to achieve force distribution and load transfer. Non-engine drive means capable of powering a landing gear wheel to move the aircraft during taxi are integrated into existing landing gear designs so that excess drive forces are transferred and distributed through previously evaluated and certificated landing gear structures, including tow fittings, determined to be capable of handling such forces, which eliminates changes to the landing gear and facilitates retrofit and certification. Engines-off taxi technology can be rapidly designed and developed to be retrofitted on existing aircraft nose and/or main landing gear and then efficiently certificated.

3. 发明申请

US20150151835A1 Load Transfer in a Powered Aircraft Drive Wheel 有权
标题翻译：在有功的飞机驱动轮中的负载传递
公开(公告)号：US20150151835A1
公开(公告)日：2015-06-04
申请号：US14449138
申请日：2014-07-31
申请人： Isaiah W. Cox , Scott Perkins
发明人： Isaiah W. Cox , Scott Perkins
IPC分类号： B64C25/40 , B64F5/00 , B64C25/34
CPC分类号： B64C25/405 , Y02T50/823 , Y10T29/49716
摘要： An efficient system and method are provided wherein aircraft may be retrofitted with non-engine drive means controllable to power landing gear wheels to move the aircraft autonomously during ground movement without engines or tow vehicles so that existing landing gear structures are employed to achieve force distribution and load transfer. Non-engine drive means capable of powering a landing gear wheel to move the aircraft during taxi are integrated into existing landing gear designs so that excess drive forces are transferred and distributed through previously evaluated and certificated landing gear structures, including tow fittings, determined to be capable of handling such forces, which eliminates changes to the landing gear and facilitates retrofit and certification. Engines-off taxi technology can be rapidly designed and developed to be retrofitted on existing aircraft nose and/or main landing gear and then efficiently certificated.
摘要翻译：提供了一种有效的系统和方法，其中可以使用非发动机驱动装置来改装飞行器，所述非发动机驱动装置可控制以驱动起落架齿轮，以在地面运动期间自主地移动飞行器，而不需要发动机或牵引车辆，从而采用现有的起落架结构来实现力分布，负载转移。非起动机驱动装置能够使着陆齿轮在出租车期间使飞机移动而被集成到现有的起落架设计中，以便通过先前评估和认证的起落架结构（包括牵引装置）将过量的驱动力传递和分配，确定为能够处理这种力，这消除了起落架的变化，并有助于改装和认证。引擎出租车技术可以快速设计和开发，以便在现有的飞机机头和/或主起落架上进行改装，然后进行有效的认证。

4. 发明授权

US09033273B2 Integrated aircraft ground navigation control system 有权
标题翻译：综合飞机地面导航控制系统
公开(公告)号：US09033273B2
公开(公告)日：2015-05-19
申请号：US13287115
申请日：2011-11-01
申请人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
发明人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
IPC分类号： B64C25/00 , B64C25/40 , G08G5/06
CPC分类号： B64C25/405 , G08G5/065 , Y02T50/823
摘要： An aircraft ground control system that moves an aircraft on the ground between landing and take off without external mechanical assistance from airport tugs or tow vehicles or reliance on thrust produced by the aircraft's engines is provided. The aircraft ground control system interfaces only with an aircraft auxiliary power unit or other aircraft power supply, but otherwise operates independently of aircraft systems. A system integrator and controller links cockpit controls designed to actuate the transmission of power to system components and to activate system components only under predetermined conditions with selectively activatable drivers in driving connection with one or more aircraft wheels to move the aircraft on the ground at selected torques and speeds.
摘要翻译：提供一种飞机地面控制系统，其在飞机着陆和起飞之间移动飞机，而不需要机场拖船或拖车的外部机械帮助，或依赖飞机发动机产生的推力。飞机地面控制系统只能与飞机辅助动力装置或其他飞机电源相连接，而与飞机系统无关。系统集成商和控制器连接驾驶舱控制器，其设计用于致动向系统组件传递电力，并且仅在预定条件下激活系统组件，其中选择性地激活驱动器与一个或多个飞行器轮驱动连接，以在选定的转矩下将飞机移动到地面上和速度。

5. 发明授权

US08833694B2 Split circumference aircraft wheel assembly with integrated drive motor assembly 有权
标题翻译：分体式飞轮组件与集成驱动电机组合
公开(公告)号：US08833694B2
公开(公告)日：2014-09-16
申请号：US13523865
申请日：2012-06-14
申请人： Neal Gilleran , Robert Sweet , Scott Perkins
发明人： Neal Gilleran , Robert Sweet , Scott Perkins
IPC分类号： B64C25/50
CPC分类号： B64C25/405 , Y02T50/823
摘要： A split circumference wheel assembly is provided for an aircraft landing gear wheel configured to maximize the space available within a landing gear wheel well to support a motor driver assembly with drive means that drives the aircraft wheel on the ground. The split circumference wheel assembly includes separable inboard and outboard support walls that are spaced axially apart a maximized distance so that the motor driver assembly is completely contained within the maximized space defined. A preferred wheel assembly employs a demountable flange and a locking ring to integrally and removably support the motor driver assembly within the maximized wheel volume to drive one or more aircraft wheels and move the aircraft independently on the ground. The wheel and motor driver assembly described herein are designed to be retrofitted in an existing aircraft wheel.
摘要翻译：为飞机着陆齿轮提供分体式圆周轮组件，其被配置为使起落架轮井内的空间最大化，以支撑具有驱动装置的马达驱动器组件，所述驱动装置驱动地面上的飞行器轮。分体式圆周轮组件包括可分离的内侧和外侧支撑壁，其间隔开最大距离的轴向间隔，使得电动机驱动器组件完全包含在限定的最大空间内。优选的车轮组件采用可拆卸的凸缘和锁定环，以将电动机驱动器组件整体地和可拆卸地支撑在最大化的车轮体积内以驱动一个或多个飞行器轮子并且独立地在地面上移动飞行器。这里描述的车轮和马达驱动器组件被设计成在现有飞行器轮中进行改装。

6. 发明授权

US06578722B2 Portable hoist assembly 失效
公开(公告)号：US06578722B2
公开(公告)日：2003-06-17
申请号：US09893930
申请日：2001-06-29
申请人： Scott Perkins , Don Hamilton
发明人： Scott Perkins , Don Hamilton
IPC分类号： B66C2344
CPC分类号： B66C23/44
摘要： The present invention is for a portable hoist assembly that includes a base member, an upright support member and a boom. A winch and line are attached to the hoist assembly with an engagement member for lifting objects. The base member attaches to a receiving member. The receiving member may be a trailer hitch on a vehicle. The boom and base member pivot with respect to the support member to a collapsed storage position. The boom and base member extend substantially parallel to the support member, and an end of the boom attaches to the base member. The engagement member is inserted within the base member for storage.

7. 发明申请

US20130056580A1 SPLIT CIRCUMFERENCE AIRCRAFT WHEEL ASSEMBLY WITH INTEGRATED DRIVE MOTOR ASSEMBLY 有权
标题翻译：具有集成驱动电机组件的分体循环飞行器车轮组件
公开(公告)号：US20130056580A1
公开(公告)日：2013-03-07
申请号：US13523865
申请日：2012-06-14
申请人： Neal Gilleran , Robert Sweet , Scott Perkins
发明人： Neal Gilleran , Robert Sweet , Scott Perkins
IPC分类号： B64C25/50 , B64C25/36
CPC分类号： B64C25/405 , Y02T50/823
摘要： A split circumference wheel assembly is provided for an aircraft landing gear wheel configured to maximize the space available within a landing gear wheel well to support a motor driver assembly with drive means that drives the aircraft wheel on the ground. The split circumference wheel assembly includes separable inboard and outboard support walls that are spaced axially apart a maximized distance so that the motor driver assembly is completely contained within the maximized space defined. A preferred wheel assembly employs a demountable flange and a locking ring to integrally and removably support the motor driver assembly within the maximized wheel volume to drive one or more aircraft wheels and move the aircraft independently on the ground. The wheel and motor driver assembly described herein are designed to be retrofitted in an existing aircraft wheel.
摘要翻译：为飞机着陆齿轮提供分体式圆周轮组件，其被配置为使起落架轮井内的空间最大化，以支撑具有驱动装置的马达驱动器组件，所述驱动装置驱动地面上的飞行器轮。分体式圆周轮组件包括可分离的内侧和外侧支撑壁，其间隔开最大距离的轴向间隔，使得电动机驱动器组件完全包含在限定的最大空间内。优选的车轮组件采用可拆卸的凸缘和锁定环，以将电动机驱动器组件整体地和可拆卸地支撑在最大化的车轮体积内以驱动一个或多个飞行器轮子并且独立地在地面上移动飞行器。这里描述的车轮和马达驱动器组件被设计成在现有飞行器轮中进行改装。

8. 发明申请

US20120168557A1 Integrated Aircraft Ground Navigation Control System 有权
标题翻译：综合飞机地面导航控制系统
公开(公告)号：US20120168557A1
公开(公告)日：2012-07-05
申请号：US13287115
申请日：2011-11-01
申请人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
发明人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
IPC分类号： B64C25/50
CPC分类号： B64C25/405 , G08G5/065 , Y02T50/823
摘要： An aircraft ground control system that moves an aircraft on the ground between landing and take off without external mechanical assistance from airport tugs or tow vehicles or reliance on thrust produced by the aircraft's engines is provided. The aircraft ground control system interfaces only with an aircraft auxiliary power unit or other aircraft power supply, but otherwise operates independently of aircraft systems. A system integrator and controller links cockpit controls designed to actuate the transmission of power to system components and to activate system components only under predetermined conditions with selectively activatable drivers in driving connection with one or more aircraft wheels to move the aircraft on the ground at selected torques and speeds.
摘要翻译：提供一种飞机地面控制系统，其在飞机着陆和起飞之间移动飞机，而不需要机场拖船或拖车的外部机械帮助，或依赖飞机发动机产生的推力。飞机地面控制系统只能与飞机辅助动力装置或其他飞机电源相连接，而与飞机系统无关。系统集成商和控制器连接驾驶舱控制器，其设计用于致动向系统组件传递电力，并且仅在预定条件下激活系统组件，其中选择性地激活驱动器与一个或多个飞行器轮驱动连接，以在选定的转矩下将飞机移动到地面上和速度。

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