公开(公告)号：US20140336847A1

公开(公告)日：2014-11-13

申请号：US13591328

申请日：2012-08-22

Applicant: Isaiah W. Cox ,  Jonathan Sidney Edelson ,  Nechama Cox

Inventor： Isaiah W. Cox ,  Jonathan Sidney Edelson ,  Nechama Cox

IPC: B64C25/40 ,  B64C19/00

CPC classification number: B64C25/405 ,  B64C19/00 ,  Y02T50/823

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US08299673B2

公开(公告)日：2012-10-30

申请号：US12008227

申请日：2008-01-09

Applicant: Jonathan Sidney Edelson

Inventor： Jonathan Sidney Edelson

IPC: H02K17/00

CPC classification number: H02K3/28 ,  H02K17/12

Abstract: A high phase order induction machine wound and permitted by coil symmetry to operate at fewer than the magnetically optimal number of poles is constrained by symmetry to be a two pole machine and be capable of operating on odd harmonics only, but with back-iron, end rings, and rotor core optimized for 10 pole operation, might be used normally in ‘5th harmonic’ mode, with ‘7th harmonic’ utilized to engage the ‘mesh effect’. Such a machine thus appears to be operating in the ‘1.4 harmonic’. A high phase order induction machine driven by a second harmonic drive, in which a symmetry imposed by full span windings is broken. This may be most simply accomplished through the use of short pitch windings. Other possible approaches include using non-wound slot drive, and using toroidal windings which localize coils to individual slots.

Abstract translation: 缠绕并允许线圈对称以低于最优磁极数量运行的高相位感应电机受到对称性约束为双极机器，并且能够仅在奇数谐波上运行，但是使用后铁端 环和转子芯优化10极操作，可以在5次谐波模式下正常使用，7次谐波用于啮合网格效应。 因此，这样的机器似乎在1.4谐波中操作。 由二次谐波驱动驱动的高相位感应电机，其中由全跨度绕组施加的对称被破坏。 这可以通过使用短节距绕组最简单地实现。 其他可能的方法包括使用非卷绕槽驱动，并且使用将线圈定位到各个槽的环形绕组。

公开(公告)号：US20120001018A1

公开(公告)日：2012-01-05

申请号：US13050838

申请日：2011-03-17

Applicant: Neal Gilleran ,  Robert M. Sweet ,  Jonathan Sidney Edelson ,  Rodney T. Cox ,  Isaiah Watas Cox

Inventor： Neal Gilleran ,  Robert M. Sweet ,  Jonathan Sidney Edelson ,  Rodney T. Cox ,  Isaiah Watas Cox

IPC: B64C25/50

CPC classification number: B64C25/405 ,  H02K7/14 ,  Y02T50/823

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20110297786A1

公开(公告)日：2011-12-08

申请号：US13082932

申请日：2011-04-08

Applicant: Robert M. Sweet ,  Neal Gilleran ,  Jonathan Sidney Edelson ,  Isaiah Watas Cox ,  Rodney T. Cox

Inventor： Robert M. Sweet ,  Neal Gilleran ,  Jonathan Sidney Edelson ,  Isaiah Watas Cox ,  Rodney T. Cox

IPC: B64C25/34

CPC classification number: B64C25/405 ,  Y02T50/823

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20090302787A1

公开(公告)日：2009-12-10

申请号：US11918914

申请日：2006-04-05

Applicant: Jonathan Sidney Edelson

Inventor： Jonathan Sidney Edelson

IPC: H02P25/08

CPC classification number: H02P25/08 ,  H02K17/12 ,  H02K19/103 ,  H02K19/14 ,  H02K37/04 ,  H02K99/20 ,  H02K2213/03 ,  H02K2213/09 ,  H02P23/08

Abstract: This application describes a motor designed to operate as a reluctance machine at low speeds and as an induction machine at high speeds. The drive waveform is composed of one or more harmonics to be used to match the reluctance pattern of the stator-rotor, causing the rotor to rotate due to the reluctance effect, and one or more other harmonics to induce current in the rotor, causing the rotor to rotate due to the induction effect and the subsequent interaction of the stator and rotor magnetic fields. The two effects are generally not applied simultaneously.

Abstract translation: 该应用描述了一种设计用作低速磁阻电机和高速感应电机的电动机。 驱动波形由用于匹配定子 - 转子的磁阻图案的一个或多个谐波组成，使得转子由于磁阻效应而旋转，以及一个或多个其它谐波以在转子中感应电流，导致 转子由于感应效应和随后的定子和转子磁场的相互作用而旋转。 这两种效果通常不会同时应用。

公开(公告)号：US07469858B2

公开(公告)日：2008-12-30

申请号：US10574761

申请日：2004-10-06

Applicant: Jonathan Sidney Edelson

Inventor： Jonathan Sidney Edelson

IPC: B64C25/40 ,  F16H48/06

CPC classification number: F16H3/56 ,  B64C25/405 ,  Y02T50/823

Abstract: The present invention is a compound planetary gear system which has a moveable sun gear and a lockable sun gear to change the gear ratio between a high gear ratio and a pseudo 1:1 slipping ratio. The system makes use of a ratchet and pawl mechanism to provide a safety backup for when the lockable sun gear is locked. The invention may be used to move the aircraft from a stationary position, for taxiing, and for pre-rotating the wheels prior to landing.

Abstract translation: 本发明是一种复合行星齿轮系统，其具有可移动的太阳齿轮和可锁定的太阳齿轮，以改变高齿轮比和假1：1滑移比之间的齿轮比。 该系统利用棘轮和棘爪机构来为可锁定的太阳齿轮锁定时提供安全备用。 本发明可以用于将飞机从静止位置移动，用于滑行，并且用于在着陆之前预先旋转车轮。

公开(公告)号：US07464549B1

公开(公告)日：2008-12-16

申请号：US11326162

申请日：2006-01-04

Applicant: Jonathan Sidney Edelson ,  Wayne Boyer Collier

Inventor： Jonathan Sidney Edelson ,  Wayne Boyer Collier

IPC: F15B7/02

CPC classification number: F15B7/02 ,  F15B7/008 ,  F16H39/16 ,  F16H39/18

Abstract: The present invention comprises an input drive system, which provides a plurality of phases of oscillating fluid flow, and an output drive system connected directly to the input drive system that is powered by the plurality of phases of oscillating fluid flow. The input drive system comprises a plurality of pistons that are caused to move in a reciprocating fashion by a power source. The power source may be a rotating power source, such as that provided by an electric motor, a diesel or petrol engine, or a turbine system. The input drive system comprises a cam ring attached to a rotating power source; a plurality of cam rollers in contact with the cam ring; and a plurality of pistons attached to the cam rings. The output drive system comprises one or more pistons that are caused to move in a reciprocating fashion by the oscillating fluid flow provided by the input drive system. The output drive system comprises a cam ring attached to a load; a plurality of cam rollers in contact with the cam ring; and a plurality of pistons attached to the cam rings.

Abstract translation: 本发明包括提供多个相位的振荡流体流的输入驱动系统，以及直接连接到由振荡流体流的多个相供电的输入驱动系统的输出驱动系统。 输入驱动系统包括多个活塞，其通过电源以往复方式移动。 电源可以是旋转电源，例如由电动机，柴油或汽油发动机或涡轮机系统提供的电源。 输入驱动系统包括附接到旋转电源的凸轮环; 与凸轮环接触的多个凸轮滚子; 以及附接到所述凸轮环的多个活塞。 输出驱动系统包括通过由输入驱动系统提供的振荡流体流以往复方式移动的一个或多个活塞。 输出驱动系统包括连接到负载的凸轮环; 与凸轮环接触的多个凸轮滚子; 以及附接到所述凸轮环的多个活塞。

公开(公告)号：US07375483B2

公开(公告)日：2008-05-20

申请号：US11585647

申请日：2006-10-23

Applicant: Jonathan Sidney Edelson

Inventor： Jonathan Sidney Edelson

IPC: H02P3/22

CPC classification number: H02P3/14 ,  H02K3/28 ,  H02K17/12 ,  H02P3/22 ,  H02P27/00

Abstract: In the present invention, several polyphase devices are connected together: an inverter, and electrical rotating machine, and a resistive load or braking resistor. The purpose of the resistive load is to dissipate excess electrical power which may be produced when the inverter acts to slow down the rotating machine, causing the rotating machine to act as a generator. In common art, this resistive load is a single DC resistor coupled to the DC link of the inverter via a separate resistor control transistor. In the present invention, the resistive load is a mesh connected array of resistors, and is electrically connected to the same inverter output terminals that the rotating machine is connected to. When it is desired that the resistors absorb energy, for example from a braking operation, then the harmonic content of the inverter output is adjusted, thus placing voltage differences across the resistor array and causing current to flow in the resistors.

Abstract translation: 在本发明中，若干多相装置连接在一起：逆变器和旋转电机以及电阻负载或制动电阻。 电阻负载的目的是消散当变频器作用于减速旋转机器时可能产生的过量电力，导致旋转机器充当发电机。 在常见技术中，该电阻性负载是通过单独的电阻器控制晶体管耦合到逆变器的DC链路的单个DC电阻器。 在本发明中，电阻负载是电阻器的网状连接阵列，并且电连接到与旋转机器连接的相同的逆变器输出端子。 当希望电阻器例如从制动操作中吸收能量时，调整逆变器输出的谐波含量，从而在电阻器阵列上施加电压差并且使电流在电阻器中流动。

公开(公告)号：US07327105B2

公开(公告)日：2008-02-05

申请号：US11525639

申请日：2006-09-21

Applicant: Jonathan Sidney Edelson

Inventor： Jonathan Sidney Edelson

IPC: H02P1/18

CPC classification number: H02K17/12 ,  H02K3/28 ,  H02K5/225 ,  H02K11/33 ,  H02P25/18 ,  H02P25/22 ,  H02P27/00 ,  H02P29/50

Abstract: An electrical rotating apparatus is provided that has variable impedance. This is achieved by connecting one of the polyphase components of the apparatus in a mesh connection. The spanning value, L, of such a mesh connection may be varied by changing the harmonic content supplied by an inverter component. Also provided is a method for connecting an inverter to a motor, wherein a switching arrangement permits the simple alteration between various mesh connections of different span value, changing thereby the Volts/Hertz ratio of the motor.

Abstract translation: 提供具有可变阻抗的电动旋转装置。 这通过将网格连接中的设备的多相分量连接起来实现。 可以通过改变由逆变器部件提供的谐波含量来改变这种网状连接的跨越值L。 还提供了一种用于将逆变器连接到电动机的方法，其中开关装置允许在不同跨度值的各种网格连接之间的简单改变，从而改变电动机的电压/赫兹比。

公开(公告)号：US07166786B2

公开(公告)日：2007-01-23

申请号：US10760697

申请日：2004-01-19

Applicant: Avto Tavkhelidze ,  Jonathan Sidney Edelson ,  Isaiah Wates Cox ,  Stuart Harbron

Inventor： Avto Tavkhelidze ,  Jonathan Sidney Edelson ,  Isaiah Wates Cox ,  Stuart Harbron

IPC: C03C25/68

CPC classification number: B82Y10/00 ,  B82Y30/00 ,  B82Y40/00 ,  G03F7/0002 ,  H01J1/30 ,  H01L21/4867 ,  H01L29/127 ,  H01L31/0352 ,  Y10S977/755 ,  Y10S977/781 ,  Y10S977/782 ,  Y10S977/81

Abstract: A method is disclosed for the induction of a suitable band gap and electron emissive properties into a substance, in which the substrate is provided with a surface structure corresponding to the interference of electron waves. Lithographic or similar techniques are used, either directly onto a metal mounted on the substrate, or onto a mold which then is used to impress the metal. In a preferred embodiment, a trench or series of nano-sized trenches are formed in the metal.

Abstract translation: 公开了一种用于将合适的带隙和电子发射性质诱导到物质中的方法，其中衬底具有对应于电子波干涉的表面结构。 使用平版印刷或类似技术，直接用于安装在基板上的金属上，或者用于模具，然后用于印刷金属。 在优选实施例中，在金属中形成沟槽或一系列纳米尺寸的沟槽。