公开(公告)号：US08541678B2

公开(公告)日：2013-09-24

申请号：US11992995

申请日：2006-10-04

Applicant: Hans Juergen Walitzki ,  Isaiah Watas Cox

Inventor： Hans Juergen Walitzki ,  Isaiah Watas Cox

IPC: H01L37/00 ,  H01L35/30 ,  H01L21/00

CPC classification number: H01L23/34 ,  H01J45/00 ,  H01L35/32 ,  H01L2924/0002 ,  H01L2924/00

Abstract: A thermionic or thermotunneling converter consisting of two electrodes maintained at a desired distance from one another by means of spacers in which the electrodes comprise silicon coated with a hard material, or comprise a ceramic or other refractory material. The spacers are formed by oxidizing one electrode, protecting certain oxidized areas and removing the remainder of the oxidized layer. The protected oxidized areas remain as spacers. These spacers have the effect of maintaining the electrodes at a desired distance without the need for active elements, thus greatly reducing costs.

Abstract translation: 一种由两个电极组成的热电偶或热电子转换器，其中电极通过间隔物彼此保持在所需的距离，其中电极包括涂覆有硬质材料的硅，或者包括陶瓷或其它耐火材料。 间隔物通过氧化一个电极，保护某些氧化区域并去除氧化层的其余部分而形成。 受保护的氧化区域保留为间隔物。 这些间隔物具有将电极保持在期望距离而不需要有源元件的效果，因此大大降低了成本。

公开(公告)号：US20090114765A1

公开(公告)日：2009-05-07

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。

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。

公开(公告)号：US07983804B2

公开(公告)日：2011-07-19

申请号：US11899001

申请日：2007-08-29

Applicant: Isaiah Watas Cox ,  Joseph Jeremiah Cox ,  Jonathan Sidney Edelson

Inventor： Isaiah Watas Cox ,  Joseph Jeremiah Cox ,  Jonathan Sidney Edelson

IPC: G01C23/00

CPC classification number: G08G5/065

Abstract: A system for minimizing damage on collision to a vehicle having at least one self-propelled wheel is disclosed. The system comprises a motor in a wheel of said vehicle which drives the vehicle, means for measuring the speed of said wheel, means for measuring the torque of said motor, means for monitoring the ratio of the torque of the motor to the speed of the wheel, and means for stopping said motor when torque:speed ratio exceeds an acceptable value.

Abstract translation: 公开了一种用于使具有至少一个自推进轮的车辆的碰撞损伤最小化的系统。 该系统包括驱动车辆的所述车辆的车轮中的电动机，用于测量所述车轮的速度的装置，用于测量所述电动机的转矩的装置，用于监测电动机的转矩与所述电动机的转速的比率的装置 车轮以及当转矩比超过可接受值时停止所述电动机的装置。

公开(公告)号：US20090014261A1

公开(公告)日：2009-01-15

申请号：US12217358

申请日：2008-07-03

Applicant: Jonathan Sidney Edelson ,  Isaiah Watas Cox ,  Todd Tripp

Inventor： Jonathan Sidney Edelson ,  Isaiah Watas Cox ,  Todd Tripp

IPC: F16D65/36

CPC classification number: B64C25/405 ,  B64F1/002 ,  Y02T50/823

Abstract: An apparatus for remotely controlling an aircraft having a self-propelled nosewheel, on the ground, comprises parking brakes; an APU on said aircraft; control means for applying and releasing said parking brakes; control means for turning on and off said APU; transmitting means for transmitting information to said parking brakes and said APU; receiving means for receiving information at said parking brakes; and receiving means for receiving information at said APU.

Abstract translation: 一种用于远程控制在地面上具有自推进式nosewheel的飞行器的装置包括驻车制动器; 飞机上的APU; 用于施加和释放所述驻车制动器的控制装置; 用于打开和关闭所述APU的控制装置; 用于向所述停车制动器和所述APU发送信息的发送装置; 用于在所述驻车制动器处接收信息的接收装置; 以及用于在所述APU处接收信息的接收装置。

公开(公告)号：US20080312870A1

公开(公告)日：2008-12-18

申请号：US12069614

申请日：2008-02-11

Applicant: Isaiah Watas Cox ,  Jonathan Sidney Edelson

Inventor： Isaiah Watas Cox ,  Jonathan Sidney Edelson

IPC: G01G19/07 ,  G01G23/36 ,  B64D47/00

CPC classification number: B64C25/405 ,  Y02T50/823

Abstract: A method of measuring the weight of an aircraft is disclosed. The method comprises, in a self-propelled aircraft undercarriage having a electrical rotating machine, the steps of: measuring the current and voltage going into the rotating machine using current and voltage measuring means, calculating the power into the rotating machine, measuring the speed (or torque or acceleration) of said machine using speed sensing means, and comparing the power and speed (or torque or acceleration) results with a database of power and speed relationships of comparable aircraft of varying weights.

Abstract translation: 公开了一种测量飞机重量的方法。 该方法包括在具有旋转电机的自走式飞机起落架中，采用电流和电压测量装置测量进入旋转机器的电流和电压，计算旋转机器的功率，测量速度（ 或扭矩或加速度），并且将功率和速度（或扭矩或加速度）结果与不同重量的可比飞机的功率和速度关系的数据库进行比较。

公开(公告)号：US20080296429A1

公开(公告)日：2008-12-04

申请号：US12217635

申请日：2008-07-07

Applicant: Jonathan Sidney Edelson ,  Isaiah Watas Cox ,  Daniel Liviu Barbalata

Inventor： Jonathan Sidney Edelson ,  Isaiah Watas Cox ,  Daniel Liviu Barbalata

IPC: B64C25/50

CPC classification number: B64F1/22 ,  B64C25/405 ,  Y02T50/823 ,  Y10S180/904

Abstract: An apparatus for controlling the movement of an aircraft having a self-propelled nosewheel, on the ground, is disclosed. The apparatus comprises a control arm; a control unit; means for transmitting information to said self-propelled nosewheel; means for receiving information at said self-propelled nosewheel; and means for controlling at least one of the speed and direction of said nosewheel; whereby airport ground staff can intuitively control the movements of said aircraft by holding said arm and moving it in the direction of required movement of said aircraft.

Abstract translation: 公开了一种用于控制在地面上具有自推进式nosewheel的飞行器的运动的装置。 该装置包括控制臂; 一个控制单元; 将信息传送到所述自推进式报刊的手段; 用于在所述自推进轮胎上接收信息的装置; 以及用于控制所述nosewheel的速度和方向中的至少一个的装置; 由此机场地勤人员可以通过握住所述臂并沿着所述飞行器的所需运动的方向移动它来直观地控制所述飞行器的运动。

公开(公告)号：US6117344A

公开(公告)日：2000-09-12

申请号：US45299

申请日：1998-03-20

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

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

IPC: G03F7/00 ,  G03F7/20 ,  H01J1/30 ,  H01J9/02 ,  H01J45/00 ,  G25F3/02

CPC classification number: B82Y10/00 ,  B82Y40/00 ,  G03F7/0002 ,  H01J1/30 ,  H01J45/00 ,  H01J9/022 ,  G03F7/2059 ,  G03F7/2065

Abstract: Methods for fabricating nano-structured surfaces having geometries in which the passage of elementary particles through a potential barrier is enhanced are described. The methods use combinations of electron beam lithography, lift-off, and rolling, imprinting or stamping processes.

Abstract translation: 描述了具有几何形状的纳米结构表面的方法，其中基本粒子通过势垒的通过被增强。 该方法使用电子束光刻，剥离和滚压，压印或冲压工艺的组合。

公开(公告)号：US5699668A

公开(公告)日：1997-12-23

申请号：US422076

申请日：1995-03-30

Applicant: Isaiah Watas Cox

Inventor： Isaiah Watas Cox

IPC: F25B21/00 ,  F25B30/00 ,  F28D15/00 ,  F28F13/16 ,  H01J1/05 ,  H01L23/427

CPC classification number: H01L23/427 ,  F25B21/00 ,  F28F13/16 ,  F25B2321/003 ,  F25B30/00 ,  H01L2924/0002 ,  Y02B30/66

Abstract: In the method of the present invention, electrostatic fields are used to induce heat pumping action of a working fluid. A plurality of heat pumps with no moving parts are used. The operation of the one pump enhances the operation of the next. The method of the present invention is conducive to devices of a wide range of scales. Furthermore, operation at partial power levels is practicable, and precise control of temperature possible. Control is further enhanced by the addition or removal of further units to the system. Reliability should be enhanced, and peak power demands reduced. Wide selection of possible working fluids allows for the elimination of environmentally harmful halocarbons. In one embodiment of the present invention, chemical working fluids are eliminated entirely. In another embodiment, supercooled fluids such as liquid helium may be used while eliminating the wastage commonly encountered using such fluids.

Abstract translation: 在本发明的方法中，使用静电场来引起工作流体的热泵送作用。 使用多个没有移动部件的热泵。 一个泵的操作增强了下一个的运行。 本发明的方法有利于广泛尺度的装置。 此外，在部分功率水平的操作是可行的，并且可以精确地控制温度。 通过向系统添加或移除其他单元来进一步增强控制。 应提高可靠性，降低峰值功率需求。 广泛选择可能的工作流体允许消除对环境有害的卤代烃。 在本发明的一个实施例中，完全消除了化学工作流体。 在另一个实施例中，可以使用过冷流体如液氦，同时消除使用这种流体常见的浪费。

公开(公告)号：US09216819B2

公开(公告)日：2015-12-22

申请号：US13074801

申请日：2011-03-29

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

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 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.

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。