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1. 发明申请

US20150203193A1 METHOD AND SYSTEM FOR THE POWERED SELF PUSH BACK OF AN AIRCRAFT 有权
标题翻译：用于飞机自动自推的方法和系统
公开(公告)号：US20150203193A1
公开(公告)日：2015-07-23
申请号：US14004158
申请日：2012-02-08
申请人： Isaiah W. Cox , Neal Gilleran , Joseph Goldman
发明人： Isaiah W. Cox , Neal Gilleran , Joseph Goldman
IPC分类号： B64C25/40 , B64C25/34
CPC分类号： B64C25/405 , B64C25/34 , B64D27/00 , Y02T50/823
摘要： A powered self push back method and system for an aircraft are provided to move an aircraft on the ground safely during push back without assistance from an external tug vehicle or the aircraft main engines. The method employs constant cooperative communication and signals between the pilot and the ground crew during the push back process to ensure that push back of the aircraft is safe, efficient, and reduces aircraft turnaround time. The powered self push back system used in conjunction with this method includes at least one powered self-propelled aircraft drive wheel powered by a wheel drive assembly that can be activated by pilot input controls or by remote control exteriorly of or interiorly to the aircraft in response to ground crew signals to activate the driver to rotate the drive wheel in a reverse, push back direction, causing the aircraft to move in the push back direction or in a forward direction for taxi and takeoff in accordance with activation of the controls.
摘要翻译：提供一种用于飞行器的动力自推回方法和系统，用于在没有来自外部拖拉车辆或飞机主发动机的帮助下在推回期间安全地移动飞机在地面上。该方法在推回过程中在飞行员和地勤人员之间采取持续的协作通信和信号，以确保飞机的推回是安全，有效的，并减少飞机周转时间。与该方法一起使用的动力自推回系统包括至少一个由车轮驱动组件供电的供电的自行式飞行器驱动轮，其可以由飞行员输入控制或者作为响应的外部或外部的遥控器来激活到地勤人员信号以激活驾驶员以相反的推回方向旋转驱动轮，使得飞机沿着推回方向或向前方向移动，以根据控制的激活而进行出租车和起飞。

2. 发明授权

US09334047B2 Method and system for the powered self push back of an aircraft 有权
标题翻译：飞机的自动推回方法和系统
公开(公告)号：US09334047B2
公开(公告)日：2016-05-10
申请号：US14004158
申请日：2012-02-08
申请人： Isaiah W. Cox , Neal Gilleran , Joseph Goldman
发明人： Isaiah W. Cox , Neal Gilleran , Joseph Goldman
IPC分类号： B64C25/50 , B64C25/40 , B64C25/34 , B64D27/00
CPC分类号： B64C25/405 , B64C25/34 , B64D27/00 , Y02T50/823
摘要： A powered self push back method and system for an aircraft are provided to move an aircraft on the ground safely during push back without assistance from an external tug vehicle or the aircraft main engines. The method employs constant cooperative communication and signals between the pilot and the ground crew during the push back process to ensure that push back of the aircraft is safe, efficient, and reduces aircraft turnaround time. The powered self push back system used in conjunction with this method includes at least one powered self-propelled aircraft drive wheel powered by a wheel drive assembly that can be activated by pilot input controls or by remote control exteriorly of or interiorly to the aircraft in response to ground crew signals to activate the driver to rotate the drive wheel in a reverse, push back direction, causing the aircraft to move in the push back direction or in a forward direction for taxi and takeoff in accordance with activation of the controls.
摘要翻译：提供一种用于飞行器的动力自推回方法和系统，用于在没有来自外部拖拉车辆或飞机主发动机的帮助下在推回期间安全地移动飞机在地面上。该方法在推回过程中在飞行员和地勤人员之间采取持续的协作通信和信号，以确保飞机的推回是安全，有效的，并减少飞机周转时间。与该方法一起使用的动力自推回系统包括至少一个由车轮驱动组件供电的供电的自行式飞行器驱动轮，其可以由飞行员输入控制或者作为响应的外部或外部的遥控器来激活到地勤人员信号以激活驾驶员以相反的推回方向旋转驱动轮，使得飞机沿着推回方向或向前方向移动，以根据控制的激活而进行出租车和起飞。

3. 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.

4. 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。

5. 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。

6. 发明授权

US09216819B2 Wheel structure for integrating an electric drive motor 有权
标题翻译：用于集成电动马达的车轮结构
公开(公告)号：US09216819B2
公开(公告)日：2015-12-22
申请号：US13074801
申请日：2011-03-29
申请人： Neal Gilleran , Robert M. Sweet , Jonathan Sidney Edelson , Rodney T. Cox , Isaiah Watas Cox
发明人： Neal Gilleran , Robert M. Sweet , Jonathan Sidney Edelson , Rodney T. Cox , Isaiah Watas Cox
IPC分类号： B64C25/40
CPC分类号： B64C25/405 , Y02T50/823
摘要： A wheel design is provided for an aircraft landing gear wheel that is configured to maximize the space available within a landing gear wheel well to support a motor driver assembly that drives the aircraft wheel when the aircraft is on the ground. The wheel includes inboard and outboard support walls that are spaced apart a selected distance along the wheel axle so that the motor driver assembly components are substantially completely contained within the wheel space defined by the support walls. The preferred motor driver assembly includes an electric motor and a gear and clutch assembly operatively connected to the wheel to drive the wheel and move the aircraft on the ground. The wheel and motor driver assembly described herein may be retrofitted in an existing aircraft wheel without changing existing landing gear components, including tires, piston, and axle.
摘要翻译：为飞机起落架齿轮提供轮设计，其被配置为使起落架轮井内的可用空间最大化，以支持在飞行器处于地面时驱动飞行器轮的马达驱动器组件。车轮包括沿着轮轴间隔开选定距离的内侧和外侧支撑壁，使得电动机驱动器组件部件基本上完全包含在由支撑壁限定的车轮空间内。优选的马达驱动器组件包括电动马达和可操作地连接到车轮的齿轮和离合器组件，以驱动车轮并使飞机在地面上移动。本文所述的车轮和马达驱动器组件可以在现有的飞机车轮中改装而不改变现有的起落架部件，包括轮胎，活塞和车轴。

7. 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。

8. 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。

9. 发明授权

US08714481B2 Integrated electric motor and gear in an aircraft wheel 失效
标题翻译：集成电动机和齿轮在飞轮上
公开(公告)号：US08714481B2
公开(公告)日：2014-05-06
申请号：US13082932
申请日：2011-04-08
申请人： Robert M. Sweet , Neal Gilleran , Jonathan Sidney Edelson , Isaiah Watas Cox , Rodney T. Cox
发明人： Robert M. Sweet , Neal Gilleran , Jonathan Sidney Edelson , Isaiah Watas Cox , Rodney T. Cox
IPC分类号： B64C25/50
CPC分类号： B64C25/405 , Y02T50/823
摘要： A wheel design is provided for an aircraft landing gear wheel that is configured to maximize the space available within a landing gear wheel well to support a geared motor assembly that drives the aircraft wheel when the aircraft is on the ground. The wheel includes inboard and outboard support walls that are spaced apart a selected distance along the wheel axle so that the geared motor assembly components are substantially completely contained within the wheel space defined by the support walls. The preferred motor driver assembly includes an electric motor and a gear and clutch assembly operatively connected to the wheel to drive the wheel and move the aircraft on the ground. The wheel and motor driver assembly described herein may be retrofitted in an existing aircraft wheel without changing existing landing gear components, including tires, piston, and axle.
摘要翻译：为飞机起落架齿轮提供轮设计，其被配置为使起落架轮井内的可用空间最大化，以支撑当飞机在地面上时驱动飞行器轮的齿轮传动马达组件。车轮包括沿着轮轴间隔开选定距离的内侧和外侧支撑壁，使得齿轮传动的马达组件部件基本上完全包含在由支撑壁限定的车轮空间内。优选的马达驱动器组件包括电动马达和可操作地连接到车轮的齿轮和离合器组件，以驱动车轮并使飞机在地面上移动。本文所述的车轮和马达驱动器组件可以在现有的飞机车轮中改装而不改变现有的起落架部件，包括轮胎，活塞和车轴。

10. 发明申请

US20110284685A1 Wheel Structure for Integrating an Electric Drive Motor 有权
标题翻译：用于集成电动驱动电机的车轮结构
公开(公告)号：US20110284685A1
公开(公告)日：2011-11-24
申请号：US13074801
申请日：2011-03-29
申请人： Neal Gilleran , Robert M. Sweet , Jonathan Sidney Edelson , Rodney T. Cox , Isaiah Watas Cox
发明人： Neal Gilleran , Robert M. Sweet , Jonathan Sidney Edelson , Rodney T. Cox , Isaiah Watas Cox
IPC分类号： B64C25/50
CPC分类号： B64C25/405 , Y02T50/823
摘要： A wheel design is provided for an aircraft landing gear wheel that is configured to maximize the space available within a landing gear wheel well to support a motor driver assembly that drives the aircraft wheel when the aircraft is on the ground. The wheel includes inboard and outboard support walls that are spaced apart a selected distance along the wheel axle so that the motor driver assembly components are substantially completely contained within the wheel space defined by the support walls. The preferred motor driver assembly includes an electric motor and a gear and clutch assembly operatively connected to the wheel to drive the wheel and move the aircraft on the ground. The wheel and motor driver assembly described herein may be retrofitted in an existing aircraft wheel without changing existing landing gear components, including tires, piston, and axle.
摘要翻译：为飞机起落架齿轮提供轮设计，其被配置为使起落架轮井内的可用空间最大化，以支持在飞行器处于地面时驱动飞行器轮的马达驱动器组件。车轮包括沿着轮轴间隔开选定距离的内侧和外侧支撑壁，使得电动机驱动器组件部件基本上完全包含在由支撑壁限定的车轮空间内。优选的马达驱动器组件包括电动马达和可操作地连接到车轮的齿轮和离合器组件，以驱动车轮并使飞机在地面上移动。本文所述的车轮和马达驱动器组件可以在现有的飞机车轮中改装而不改变现有的起落架部件，包括轮胎，活塞和车轴。

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