Turnaround methods
    41.
    发明授权
    Turnaround methods 有权
    周转方法

    公开(公告)号:US07891609B2

    公开(公告)日:2011-02-22

    申请号:US11897845

    申请日:2007-08-29

    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。

    SELF-PROPELLED UNDERCARRIAGE WHEEL HAVING A LOW PROFILE TIRE
    42.
    发明申请
    SELF-PROPELLED UNDERCARRIAGE WHEEL HAVING A LOW PROFILE TIRE 有权
    具有低轮廓轮胎的自行车底盘

    公开(公告)号:US20100288873A1

    公开(公告)日:2010-11-18

    申请号:US12310609

    申请日:2007-08-29

    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以单独地或与其附接到飞行器的其他自行式起落架组件相结合地推动起落架组件所附接的飞行器。

    Nosewheel control apparatus
    43.
    发明申请
    Nosewheel control apparatus 有权
    编号控制装置

    公开(公告)号:US20090261197A1

    公开(公告)日:2009-10-22

    申请号:US11991344

    申请日:2006-08-29

    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。

    Apparatus for voice communication between persons inside and persons outside an aircraft
    44.
    发明申请
    Apparatus for voice communication between persons inside and persons outside an aircraft 审中-公开
    用于内部人员和飞机外部人员之间的语音通信的装置

    公开(公告)号:US20090065638A1

    公开(公告)日:2009-03-12

    申请号:US12220597

    申请日:2008-07-24

    CPC classification number: B64C25/405 B64F1/22 Y02T50/823

    Abstract: An apparatus for facilitating voice communication between persons outside an aircraft and persons inside an aircraft, is disclosed, comprising: an external control unit comprising: voice sensing means; transmitting means for transmitting voice information to persons in said aircraft; receiving means for receiving voice information from persons in said aircraft; and amplifying means for enabling said voice information to be heard; and an in-aircraft control unit comprising: voice sensing means; transmitting means for transmitting voice information to persons external to said aircraft; receiving means for receiving voice information from persons external to said aircraft; and amplifying means for enabling said voice information to be heard.

    Abstract translation: 公开了一种用于促进飞机外部人员和飞机内人员之间的语音通信的装置,包括:外部控制单元,包括:语音感测装置; 用于将语音信息发送到所述飞行器中的人的发送装置; 用于从所述飞行器中的人接收语音信息的接收装置; 以及用于使所述语音信息能够被听到的放大装置; 以及飞机内控制单元,包括:语音检测装置; 发送装置,用于向所述飞机外部的人传送语音信息; 用于从所述飞机外部的人接收语音信息的接收装置; 以及用于使得能够听到所述语音信息的放大装置。

    Thermionic power unit
    45.
    发明授权
    Thermionic power unit 有权
    热电单元

    公开(公告)号:US07419022B2

    公开(公告)日:2008-09-02

    申请号:US10719446

    申请日:2003-11-21

    Inventor: Isaiah Watas Cox

    Abstract: It is the principal object of the invention to provide a new and improved electrical power unit for use in automobiles, on aircraft, or for local generation of electrical power. In one embodiment of the present invention, an electrical power unit comprises: a combustion chamber that burns fuel to produce heat energy; and a thermionic device that converts the heat energy into electrical energy. In another embodiment of the present invention, the electrical power unit additionally comprises an electric motor. In a further embodiment, the electrical power unit additionally comprises an electrically power air compressor, an electrically power hydraulic compressor, and an electrical power conditioning unit.

    Abstract translation: 本发明的主要目的是提供一种用于汽车,飞机上或用于本地产生电力的新的和改进的电力单元。 在本发明的一个实施例中,电力单元包括:燃烧燃料以产生热能的燃烧室; 以及将热能转换成电能的热离子装置。 在本发明的另一实施例中,电力单元另外包括电动机。 在另一实施例中,电力单元另外包括电力空气压缩机,电动液压压缩机和电力调节单元。

    Method for flat electrodes
    46.
    发明授权
    Method for flat electrodes 失效
    扁平电极的方法

    公开(公告)号:US07005381B1

    公开(公告)日:2006-02-28

    申请号:US10639055

    申请日:2003-08-11

    Inventor: Isaiah Watas Cox

    CPC classification number: H01J9/02 H01J21/04 H01L37/00

    Abstract: The present invention is a method for reducing nanoscale surface roughness. The method involves exposing the surface to an environment that preferentially promotes evaporation of material from the region of nanoscale roughness. The methods involve either heating the surface, or flushing an inert gas across the surface, or a combination of both.

    Abstract translation: 本发明是减少纳米级表面粗糙度的方法。 该方法包括将表面暴露于优先促进材料从纳米级粗糙度区域蒸发的环境中。 这些方法包括加热表面,或者通过表面冲洗惰性气体,或两者的组合。

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