公开(公告)号：US20110284685A1

公开(公告)日：2011-11-24

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: B64C25/50

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。

公开(公告)号：US20100217456A1

公开(公告)日：2010-08-26

申请号：US12310610

申请日：2007-08-29

Applicant: Jonathan Sidney Edelson ,  Isaiah Watas Cox

Inventor： Jonathan Sidney Edelson ,  Isaiah Watas Cox

IPC: G06F19/00

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

Abstract: A method and apparatus is disclosed for reversing an aircraft on the ground comprising driving the aircraft using at least one self-propelled undercarriage wheel. An apparatus for controlling at least one of speed and at least one direction 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: 公开了一种用于使地面上的飞机反转的方法和装置，包括使用至少一个自走式起落架轮驱动飞行器。 公开了一种用于在地面上控制具有自推进的nosewheel的飞行器的速度和至少一个方向中的至少一个的装置。 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：US20080061401A1

公开(公告)日：2008-03-13

申请号：US11900790

申请日：2007-09-12

Applicant: Isaiah Watas Cox

Inventor： Isaiah Watas Cox

IPC: H01L29/735

CPC classification number: H01L29/732 ,  H01L29/0688

Abstract: A bipolar-junction transistor is disclosed comprising a first layer, a second layer, and a third layer, the surfaces of the layers modified for more precise control of electron function. The surfaces are modified to have a periodically repeating structure of indents where the indentations are of dimensions so as to create de Broglie wave interference, leading to a change in electron work function.

Abstract translation: 公开了一种双极结型晶体管，其包括第一层，第二层和第三层，这些层的表面被修改以更精确地控制电子功能。 这些表面被修改为具有周期性重复的凹槽结构，其中凹口具有尺寸，以便产生德布罗意波干涉，导致电子功函数的变化。

公开(公告)号：US06214651B1

公开(公告)日：2001-04-10

申请号：US09436913

申请日：1999-11-09

Applicant: Isaiah Watas Cox

Inventor： Isaiah Watas Cox

IPC: B05D512

CPC classification number: C23C16/27 ,  C23C16/278 ,  H01J19/24 ,  H01J21/04

Abstract: A novel use of doped carbonaceous material is disclosed, integral to the operation of Vacuum Diode Heat Pumps and Vacuum Diode Thermionic Generators. In the preferred embodiment, the use of nitrogen-doped diamond enhances the operation of Vacuum Diode Heat Pumps and Vacuum Diode Thermionic Generators.

Abstract translation: 公开了掺杂碳质材料的新用途，与真空二极管热泵和真空二极管热电偶发生器的操作是一体的。 在优选实施例中，使用掺杂氮的金刚石增强了真空二极管热泵和真空二极管热电发生器的操作。

公开(公告)号：US09914530B2

公开(公告)日：2018-03-13

申请号：US13416614

申请日：2012-03-09

Applicant: Isaiah Watas Cox ,  Rodney T. Cox ,  Aaron Z. Sichel

Inventor： Isaiah Watas Cox ,  Rodney T. Cox ,  Aaron Z. Sichel

IPC: B64C25/40 ,  B64F1/00 ,  B64F1/305

CPC classification number: B64C25/405 ,  B64F1/00 ,  B64F1/3055 ,  Y02T50/823

Abstract: A method for reducing aircraft turnaround time by improving airport ramp safety is provided. The method minimizes the time interval between an aircraft's landing and takeoff by independently moving the aircraft on the ground without the aircraft's engines by eliminating hazards from jet blast, the possibility of engine ingestion, and the time previously required to wait in the gate area upon arrival or at departure until jet blast or engine ingestion did not pose a danger. Turnaround time is further reduced by providing an onboard driver controllable to drive at least one of the aircraft's wheels between landing and takeoff, thereby eliminating the need for a tow vehicle and the time required to move the aircraft with a tow vehicle.

公开(公告)号：US08924040B2

公开(公告)日：2014-12-30

申请号：US12310610

申请日：2007-08-29

Applicant: Jonathan Sidney Edelson ,  Isaiah Watas Cox

Inventor： Jonathan Sidney Edelson ,  Isaiah Watas Cox

IPC: B64C25/00 ,  B64C25/50 ,  B64F1/22 ,  B64C25/40

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

Abstract: A method and apparatus is disclosed for reversing an aircraft on the ground comprising driving the aircraft using at least one self-propelled undercarriage wheel. An apparatus for controlling at least one of speed and at least one direction 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: 公开了一种用于使地面上的飞机反转的方法和装置，包括使用至少一个自走式起落架轮驱动飞行器。 公开了一种用于在地面上控制具有自推进的nosewheel的飞行器的速度和至少一个方向中的至少一个的装置。 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：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：US08532957B2

公开(公告)日：2013-09-10

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: G01G19/00

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：US07975960B2

公开(公告)日：2011-07-12

申请号：US11991344

申请日：2006-08-29

Applicant: Isaiah Watas Cox ,  Joseph Jeremiah Cox

Inventor： Isaiah Watas Cox ,  Joseph Jeremiah Cox

IPC: B64C25/50

CPC classification number: B64C25/40 ,  B64C25/36 ,  B64C25/405 ,  B64C25/50 ,  Y02T50/823

Abstract: An apparatus for driving a taxiing aircraft is disclosed, comprising, in an aircraft, two self-propelled nosewheels, each having an electric motor; equipment for flight; dual-function controlling means for controlling said equipment for flight and said nosewheels, said dual-function controlling means being disposed in the cockpit of said aircraft; sensing means; and switching means, —wherein said switching means are operable to switch the function of said dual-function controlling means between controlling said equipment for flight and controlling said nosewheels. Said dual function controlling means may control speed and/or steering of the aircraft. Second controlling means may be provided, and may be disposed externally to the aircraft.

Abstract translation: 公开了一种用于驾驶滑行飞机的装置，在飞行器中包括两个具有电动马达的自推进式导轨; 飞机设备 双功能控制装置，用于控制所述飞行设备和所述飞轮，所述双功能控制装置设置在所述飞机的驾驶舱内; 传感装置; 以及开关装置，其中所述开关装置可操作以在所述用于飞行的所述设备和控制所述滑轮之间切换所述双功能控制装置的功能。 所述双功能控制装置可以控制飞机的速度和/或转向。 可以设置第二控制装置，并且可以设置在飞机的外部。

公开(公告)号：US20090152055A1

公开(公告)日：2009-06-18

申请号：US12316957

申请日：2008-12-17

Applicant: Isaiah Watas Cox

Inventor： Isaiah Watas Cox

IPC: F16D55/02

CPC classification number: F16D65/847 ,  F16D65/827

Abstract: The present invention provides a means for cooling the brakes of under-carriage wheels by disengaging and spinning the motor used to provide traction on landing, thereby providing fan cooling of the brakes.

Abstract translation: 本发明提供了一种用于通过分离和旋转用于在着陆上提供牵引力的电动机来冷却载具下车轮的制动器的装置，从而提供制动器的风扇冷却。