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1. 发明授权

US09475574B2 Heat dissipation system for aircraft drive wheel drive assembly 有权
标题翻译：飞机驱动轮驱动总成散热系统
公开(公告)号：US09475574B2
公开(公告)日：2016-10-25
申请号：US13615930
申请日：2012-09-14
申请人： Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
发明人： Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
IPC分类号： B64C25/40 , H02K9/19 , H02K7/14 , B60K7/00 , B60K1/00 , B60K11/02
CPC分类号： B64C25/405 , B60K7/0007 , B60K11/02 , B60K2001/006 , B60K2007/0038 , B60K2007/0092 , B60Y2200/50 , B60Y2200/51 , B60Y2306/03 , H02K7/14 , H02K9/19 , Y02T50/823
摘要： A system is provided for dissipating heat in an onboard non-engine powered aircraft wheel drive assembly with drive means that power one or more aircraft wheels to drive the aircraft autonomously on the ground without directly using the aircraft engines. The heat dissipation system is integral with a wheel drive assembly mounted substantially completely within a nose or main landing gear wheel. A reservoir mounted outboard or inboard of the wheel drive assembly increases thermal distribution mass and fluidically communicates with wheel drive assembly components to automatically circulate heat transfer fluid between the wheel drive assembly and the reservoir when the operating temperature exceeds a predetermined maximum temperature during aircraft ground travel. The heat dissipating system can be retrofitted in an existing aircraft to improve thermal distribution and prolong wheel drive assembly and drive means operation and useful life.
摘要翻译：提供了一种用于在车内非发动机动力的飞机车轮驱动组件上散热的系统，其具有驱动装置，所述驱动装置为一个或多个飞行器轮提供动力，以在地面上自主地驱动飞行器而不直接使用飞机发动机。散热系统与基本上完全安装在鼻子或主起落架轮内的轮驱动组件是一体的。安装在车轮驱动组件的外侧或内侧的储存器增加了热分配质量并且与车轮驱动组件部件流体连通，以便在飞行器地面行驶期间工作温度超过预定最大温度时，在轮驱动组件和储存器之间自动循环传热流体。散热系统可以在现有的飞机上进行改装，以改善热分配，延长轮驱装配和驱动装置的使用寿命。

2. 发明申请

US20150159968A1 HEAT DISSIPATION SYSTEM FOR AIRCRAFT DRIVE WHEEL DRIVE ASSEMBLY 有权
标题翻译：用于飞机驱动轮驱动装置的散热系统
公开(公告)号：US20150159968A1
公开(公告)日：2015-06-11
申请号：US13615930
申请日：2012-09-14
申请人： Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
发明人： Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
IPC分类号： F28F13/00 , B64C25/40
CPC分类号： B64C25/405 , B60K7/0007 , B60K11/02 , B60K2001/006 , B60K2007/0038 , B60K2007/0092 , B60Y2200/50 , B60Y2200/51 , B60Y2306/03 , H02K7/14 , H02K9/19 , Y02T50/823
摘要： A system is provided for dissipating heat in an onboard non-engine powered aircraft wheel drive assembly with drive means that power one or more aircraft wheels to drive the aircraft autonomously on the ground without directly using the aircraft engines. The heat dissipation system is integral with a wheel drive assembly mounted substantially completely within a nose or main landing gear wheel. A reservoir mounted outboard or inboard of the wheel drive assembly increases thermal distribution mass and fluidically communicates with wheel drive assembly components to automatically circulate heat transfer fluid between the wheel drive assembly and the reservoir when the operating temperature exceeds a predetermined maximum temperature during aircraft ground travel. The heat dissipating system can be retrofitted in an existing aircraft to improve thermal distribution and prolong wheel drive assembly and drive means operation and useful life.
摘要翻译：提供了一种用于在车内非发动机动力的飞机车轮驱动组件上散热的系统，其具有驱动装置，所述驱动装置为一个或多个飞行器轮提供动力，以在地面上自主地驱动飞行器而不直接使用飞机发动机。散热系统与基本上完全安装在鼻子或主起落架轮内的轮驱动组件是一体的。安装在车轮驱动组件的外侧或内侧的储存器增加了热分配质量并且与车轮驱动组件部件流体连通，以便在飞行器地面行驶期间工作温度超过预定最大温度时，在轮驱动组件和储存器之间自动循环传热流体。散热系统可以在现有的飞机上进行改装，以改善热分配，延长轮驱装配和驱动装置的使用寿命。

3. 发明申请

US20140336847A1 METHOD FOR OPTIMIZING OPERATION OF AIRCRAFT GROUND TRAVEL DRIVE SYSTEM 有权
标题翻译：优化飞机地面行驶驱动系统运行的方法
公开(公告)号：US20140336847A1
公开(公告)日：2014-11-13
申请号：US13591328
申请日：2012-08-22
申请人： Isaiah W. Cox , Jonathan Sidney Edelson , Nechama Cox
发明人： Isaiah W. Cox , Jonathan Sidney Edelson , Nechama Cox
IPC分类号： B64C25/40 , B64C19/00
CPC分类号： B64C25/405 , B64C19/00 , Y02T50/823
摘要： A method is provided for automatically or manually. optimizing independent ground travel operation in an aircraft equipped with one or more self-propelled nose or main wheels powered by a driver means, wherein selected operating parameters indicative of optimized ground travel are monitored by sensors or detectors to provide data and information relating to the selected parameters during operation of the ground travel system. Selected operating parameters can include, for example, speed, direction of travel, torque, component thermal data aircraft location data, and operator inputs, commands, and feedback, as well as other operational data or information. Data is collected, recorded, and analyzed to enable changes to be made to the ground travel system components in real time automatically by intelligent software or manually by a system operator or at a later time to ensure optimum operation of the system.
摘要翻译：提供了一种自动或手动的方法。优化在配备有由驱动装置驱动的一个或多个自走式鼻子或主轮的飞机中的独立地面行驶操作，其中由传感器或检测器监测指示优化地面行驶的选定操作参数，以提供与所选择的相关的数据和信息地面行驶系统运行时的参数。所选择的操作参数可以包括例如速度，行进方向，扭矩，部件热数据飞行器位置数据以及操作员输入，命令和反馈以及其它操作数据或信息。收集，记录和分析数据，以便通过智能软件自动实时地对地面旅行系统组件进行更改，或者由系统操作员手动或随后更改时间来确保系统的最佳操作。

4. 发明授权

US09193449B2 Method for optimizing operation of aircraft ground travel drive system 有权
标题翻译：优化飞机地面行驶驱动系统运行的方法
公开(公告)号：US09193449B2
公开(公告)日：2015-11-24
申请号：US13591328
申请日：2012-08-22
申请人： Isaiah W. Cox , Jonathan Sidney Edelson , Nechama Cox
发明人： Isaiah W. Cox , Jonathan Sidney Edelson , Nechama Cox
IPC分类号： B64C25/40 , B64C19/00
CPC分类号： B64C25/405 , B64C19/00 , Y02T50/823
摘要： A method is provided for automatically or manually optimizing independent ground travel operation in an aircraft equipped with one or more self-propelled nose or main wheels powered by a driver means, wherein selected operating parameters indicative of optimized ground travel are monitored by sensors or detectors to provide data and information relating to the selected parameters during operation of the ground travel system. Selected operating parameters can include, for example, speed, direction of travel, torque, component thermal data, aircraft location data, and operator inputs, commands, and feedback, as well as other operational data or information. Data is collected, recorded, and analyzed to enable changes to be made to the ground travel system components in real time automatically by intelligent software or manually by a system operator or at a later time to ensure optimum operation of the system.
摘要翻译：提供了一种用于在装备有由驱动器装置供电的一个或多个自走式鼻子或主轮的飞行器中自动或手动优化独立地面行驶操作的方法，其中指示优化的地面行驶的选择的操作参数由传感器或检测器监测在地面行驶系统的运行期间提供与所选参数有关的数据和信息。所选择的操作参数可以包括例如速度，行进方向，扭矩，部件热数据，飞行器位置数据和操作员输入，命令和反馈以及其它操作数据或信息。收集，记录和分析数据，以便通过智能软件自动实时地对地面旅行系统组件进行更改，或者由系统操作员手动或随后更改时间来确保系统的最佳操作。

5. 发明授权

US09010959B2 System and method for generating artificial light 有权
标题翻译：用于生成人造光的系统和方法
公开(公告)号：US09010959B2
公开(公告)日：2015-04-21
申请号：US13569314
申请日：2012-08-08
申请人： Jonathan Sidney Edelson , Rodney T. Cox , Isaiah W. Cox
发明人： Jonathan Sidney Edelson , Rodney T. Cox , Isaiah W. Cox
IPC分类号： F21L4/02 , F21L4/00 , F21S9/03 , F21Y101/02
CPC分类号： F21L4/02 , F21L4/00 , F21S9/032 , F21Y2115/10 , Y02B10/10
摘要： A system and method for generating artificial light for interior or exterior illumination are provided to illuminate interior and exterior underground, underwater, ground level, and above ground structures and spaces by employing various combinations of solar photovoltaic-generated power and conventional power to directly power LED or other light sources to provide interior or exterior illumination of a desired optimal intensity. One embodiment of this system provides a virtual skylight that illuminates interior structures and spaces with the benefits of illumination provided by a conventional skylight but without the disadvantages. A direct connection between a solar photovoltaic cell and the LED or other light-producing source eliminates complex and costly circuitry in both interior and exterior applications. The system is configured to provide, alternatively, solar PV power and/or conventional power as required to maintain artificial illumination at a desired optimum threshold intensify.
摘要翻译：提供一种用于产生室内或室外照明的人造光的系统和方法，用于通过采用太阳能光伏发电和常规电力的各种组合来照亮地下，水下，地面以及地上结构和空间的内部和外部，以直接为LED供电或其他光源以提供期望的最佳强度的内部或外部照明。该系统的一个实施例提供了利用由常规天窗提供的照明的好处照亮内部结构和空间的虚拟天窗，但没有缺点。太阳能光伏电池和LED或其他发光源之间的直接连接消除了内部和外部应用中复杂且昂贵的电路。该系统被配置为可替代地提供所需的太阳能PV功率和/或常规功率以将人造照明维持在期望的最佳阈值增强。

6. 发明授权

US09085358B2 Electric motor integrated with a wheel 有权
标题翻译：电动机与车轮集成
公开(公告)号：US09085358B2
公开(公告)日：2015-07-21
申请号：US13050838
申请日：2011-03-17
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 , H02K7/14
CPC分类号： B64C25/405 , H02K7/14 , Y02T50/823
摘要： An integral motor and wheel assembly for aircraft landing gear is provided that includes an electric motor packaged within at least one gear wheel and configured to fit completely within the space provided in an existing aircraft for the landing gear components. The motor is positioned within the wheel to minimize the spin-up weight and to maximize the space within a given volume allocated for the motor. Installation of this motor and gear wheel assembly in an existing aircraft landing gear is designed to permit the continued use of existing landing gear components, including tires, axles, and pistons, so that the assembly can be easily retrofitted into existing aircraft.
摘要翻译：提供一种用于飞机起落架的整体马达和车轮组件，其包括封装在至少一个齿轮内的电动马达，并且构造成完全配合在用于起落架部件的现有飞机内提供的空间内。电动机位于车轮内，以最小化起重量并最大化给定电动机给定体积的空间。将该电动机和齿轮组件安装在现有的飞机起落架中被设计成允许继续使用现有的起落架部件，包括轮胎，轴和活塞，使得组件可以容易地改装成现有的飞行器。

7. 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。

8. 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。

9. 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。

10. 发明申请

US20120001018A1 Electric Motor Integrated with a Wheel 有权
标题翻译：电动机与车轮集成
公开(公告)号：US20120001018A1
公开(公告)日：2012-01-05
申请号：US13050838
申请日：2011-03-17
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 , H02K7/14 , Y02T50/823
摘要： An integral motor and wheel assembly for aircraft landing gear is provided that includes an electric motor packaged within at least one gear wheel and configured to fit completely within the space provided in an existing aircraft for the landing gear components. The motor is positioned within the wheel to minimize the spin-up weight and to maximize the space within a given volume allocated for the motor. Installation of this motor and gear wheel assembly in an existing aircraft landing gear is designed to permit the continued use of existing landing gear components, including tires, axles, and pistons, so that the assembly can be easily retrofitted into existing aircraft.
摘要翻译：提供一种用于飞机起落架的整体马达和车轮组件，其包括封装在至少一个齿轮内的电动马达，并且构造成完全配合在用于起落架部件的现有飞机内提供的空间内。电动机位于车轮内，以最小化起重量并最大化给定电动机给定体积的空间。将该电动机和齿轮组件安装在现有的飞机起落架中被设计成允许继续使用现有的起落架部件，包括轮胎，轴和活塞，使得组件可以容易地改装成现有的飞行器。

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