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    Integrated Electric Motor and Gear in an Aircraft Wheel
    31.
    发明申请
    Integrated Electric Motor and Gear in an Aircraft Wheel 失效
    集成电动机和齿轮在飞轮上

    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。

    Turnaround methods
    32.
    发明申请
    Turnaround methods 有权
    周转方法

    公开(公告)号：US20080059053A1

    公开(公告)日：2008-03-06

    申请号：US11897845

    申请日：2007-08-29

    Applicant: Isaiah Watas Cox ,  Joseph Jeremiah Cox ,  Todd Tripp

    Inventor： Isaiah Watas Cox ,  Joseph Jeremiah Cox ,  Todd Tripp

    IPC: G05D13/02 ,  B64C25/34

    CPC classification number: B64C25/405 ,  B64C25/50 ,  Y02T50/823

    Abstract: A method for reducing the turnaround time of an aircraft having at least one self-propelled undercarriage wheel comprising the step of: moving the aircraft to a required location using at least one self-propelled undercarriage wheel; wherein thrust equipment, (e.g. turbines) are turned on only when needed for takeoff or prior to landing, and are turned off until takeoff or after landing; whereby departing equipment, arriving equipment, and turnaround equipment are not at risk from operating thrust equipment, (e.g. turbines). An apparatus for reducing the turnaround time of an aircraft is disclosed comprising a control unit for facilitating voice communication between a pilot and ground staff. Said control unit may further comprise a control arm for inputting the required direction of movement of said nosewheel; means for transmitting direction information to said self-propelled nosewheel; means for receiving direction information at said self-propelled nosewheel; and means for controlling the direction of said nosewheel. The control unit may also comprise means for turning on and off an APU, parking brakes, and other aircraft features.

    Abstract translation: 一种用于减少具有至少一个自行式起落架车轮的飞行器的周转时间的方法，包括以下步骤：使用至少一个自行式起落架车轮将飞机移动到所需位置; 其中推力设备（例如涡轮机）仅在需要起飞或着陆时被打开，并且在起飞或着陆之后被关闭; 因此离开设备，到达设备和周转设备不会受到推力设备（例如涡轮机）的操作的风险。 公开了一种用于减少飞行器周转时间的装置，包括用于促进飞行员和地勤人员之间的语音通信的控制单元。 所述控制单元还可以包括用于输入所述nosewheel的所需运动方向的控制臂; 用于将方向信息传送到所述自推进轮胎的装置; 用于在所述自推进轮胎上接收方向信息的装置; 以及用于控制所述nosewheel的方向的装置。 控制单元还可以包括用于打开和关闭APU，驻车制动器和其它飞机特征的装置。

    Method for making a low work function electrode
    35.
    发明授权
    Method for making a low work function electrode 失效
    低功函电极制作方法

    公开(公告)号：US6103298A

    公开(公告)日：2000-08-15

    申请号：US955097

    申请日：1997-10-22

    Applicant: Jonathan Sidney Edelson ,  Isaiah Watas Cox

    Inventor： Jonathan Sidney Edelson ,  Isaiah Watas Cox

    IPC: C23C14/12 ,  F25B21/00 ,  H01J1/02 ,  H01J1/13 ,  H01J1/14 ,  H01J1/30 ,  H01J21/04 ,  H01J21/10 ,  H01J45/00 ,  C25B11/04

    CPC classification number: F25B21/00 ,  C23C14/12 ,  H01J1/02 ,  H01J1/13 ,  H01J1/14 ,  H01J1/30 ,  H01J21/04 ,  H01J21/105 ,  H01J45/00 ,  F25B2321/003 ,  F25B2400/15 ,  H01J2201/30426 ,  Y02B30/66

    Abstract: Methods for making low work function electrodes either made from or coated with an electride material in which the electride material has lattice defect sites are described. Lattice defect sites are regions of the crystal structure where irregularities and deformations occur. Also provided are methods for making electrodes which consist of a substrate coated with a layer of a compound comprised of a cation complexed by an electride former, in which said complex has lattice defect sites. In addition, methods for making electrodes which consist of a bulk metal coated with a layer of an electride former having lattice defect sites are described. The electride former stabilizes the loss of electrons by surface sites on the metal, lowering the work-function of the coated surface.

    Abstract translation: 描述了由电镀材料具有晶格缺陷部位的电极材料制成或涂覆低功函电极的方法。 晶格缺陷位点是发生不规则和变形的晶体结构区域。 还提供了制造电极的方法，其由涂覆有由电化学成形剂络合的阳离子组成的化合物层的基底组成，其中所述络合物具有晶格缺陷位点。 此外，描述了制造电极的方法，其由涂覆有具有晶格缺陷位点的电化学成形剂层的体金属组成。 电子前体通过金属上的表面位点稳定电子的损失，降低涂覆表面的功能。

    Electric motor integrated with a wheel
    36.
    发明授权
    Electric motor integrated with a wheel 有权
    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

    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: B64C25/40 ,  H02K7/14

    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。

    Aircraft drive
    37.
    发明授权
    Aircraft drive 有权
    飞机驱动

    公开(公告)号：US08712603B2

    公开(公告)日：2014-04-29

    申请号：US11660569

    申请日：2005-08-02

    Applicant: Isaiah Watas Cox ,  Robert Lincoln Carman, Jr.

    Inventor： Isaiah Watas Cox ,  Robert Lincoln Carman, Jr.

    IPC: G01C23/00 ,  G05D1/00 ,  G06F7/00

    CPC classification number: B64C25/40

    Abstract: The present invention describes a drive system for an aircraft involving one or more nose wheel motors. Data regarding the nose wheel rotation is used to control the ground travel of the aircraft, to predict potential problems, to provide more precise control over the aircraft, and to improve aircraft safety.

    Abstract translation: 本发明描述了一种涉及一个或多个前轮马达的飞机的驱动系统。 关于前轮旋转的数据用于控制飞机的地面行驶，以预测潜在问题，为飞机提供更精确的控制，并提高飞机的安全性。

    Motor for driving aircraft, located adjacent to undercarriage wheel
    38.
    发明授权
    Motor for driving aircraft, located adjacent to undercarriage wheel 有权
    用于驾驶飞机的电机，位于底盘轮附近

    公开(公告)号：US08220740B2

    公开(公告)日：2012-07-17

    申请号：US12291257

    申请日：2008-11-06

    Applicant: Isaiah Watas Cox ,  Hans Juergen Walitzki ,  Jonathan Sidney Edelson

    Inventor： Isaiah Watas Cox ,  Hans Juergen Walitzki ,  Jonathan Sidney Edelson

    IPC: B64C25/50

    CPC classification number: B64C25/001 ,  B64C25/40 ,  B64C25/405 ,  Y02T50/823

    Abstract: The invention disclosed is a self-propelled aircraft undercarriage for driving an aircraft on the ground, comprising: an axle; a strut supporting said axle; at least one wheel rotatably mounted on said axle; and drive means for driving said at least one wheel; characterized in that said drive means is disk shaped and is external to said wheel. In one embodiment of the invention, said drive means is mounted on said axle between said strut and said wheel. In a second embodiment, said drive means is mounted on said axle, on the side of said wheel furthest from said strut.

    Abstract translation: 所公开的发明是用于驾驶飞机在地面上的自行式飞机起落架，包括：一个轴; 支撑所述轴的支柱; 至少一个可旋转地安装在所述轴上的轮; 以及用于驱动所述至少一个车轮的驱动装置; 其特征在于，所述驱动装置是盘形的并且在所述轮的外部。 在本发明的一个实施例中，所述驱动装置安装在所述支柱和所述轮之间的所述轴上。 在第二实施例中，所述驱动装置安装在所述轴上，在所述轮的离所述支柱最远的一侧。

    Self-propelled undercarriage wheel having a low profile tire
    39.
    发明授权
    Self-propelled undercarriage wheel having a low profile tire 有权
    具有低轮胎轮胎的自行式底盘轮

    公开(公告)号：US08109463B2

    公开(公告)日：2012-02-07

    申请号：US12310609

    申请日：2007-08-29

    Applicant: Isaiah Watas Cox ,  Rodney Thomas Cox ,  Joseph Jeremiah Cox

    Inventor： Isaiah Watas Cox ,  Rodney Thomas Cox ,  Joseph Jeremiah Cox

    IPC: B64C25/02

    CPC classification number: B64C25/405 ,  Y02T50/823 ,  Y10T29/4973

    Abstract: An undercarriage wheel is disclosed comprising an axle member that supports a drive member, for example but not limited to a compact high torque electric motor, a wheel member driven by said drive member, and a tire attached to the wheel member, wherein the tire bulges in the width dimension of the wheel, wherein the drive member protrudes from the wheel member and thus occupies at least some of the additional width made available by the bulge of the tire. A further aspect of the invention is an undercarriage wheel that comprises an axle member that supports a drive member, for example but not limited to a compact high torque electric motor, a wheel member driven by said drive member, and a low-profile tire attached to the wheel member. Since the profile of the tire is low, additional space is available inside the wheel for the drive member. Preferably, the drive member occupies at least some of this additional space, and has sufficient power to be able to propel an aircraft to which the undercarriage assembly is attached, either alone or in combination with other self-propelled undercarriage assemblies attached to the aircraft.

    Abstract translation: 公开了一种底架轮，其包括轴构件，其支撑驱动构件，例如但不限于紧凑型高扭矩电动机，由所述驱动构件驱动的车轮构件和附接到车轮构件的轮胎，其中轮胎凸起 在轮的宽度尺寸上，其中驱动构件从轮构件突出，并且因此占据由轮胎的凸起可用的至少一些附加宽度。 本发明的另一方面是一种底架轮，其包括轴构件，其支撑驱动构件，例如但不限于紧凑型高扭矩电动机，由所述驱动构件驱动的车轮构件和附接的低轮胎轮胎 到车轮构件。 由于轮胎的轮廓较低，所以用于驱动构件的车轮内部还有可用的空间。 优选地，驱动构件占据该附加空间中的至少一些，并且具有足够的能力来单独地或与附接到飞行器的其他自行式起落架组件组合地推动起落架组件所附接的飞行器。

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