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    • 1. 发明授权
    • Liquid metal contact as possible element for thermotunneling
    • 液态金属接触作为热电偶的可能元件
    • US08575597B2
    • 2013-11-05
    • US11982286
    • 2007-10-31
    • Avto TavkhelidzeLeri TsakadzeZaza TaliashviliLarissa JangidzeRodney Thomas Cox
    • Avto TavkhelidzeLeri TsakadzeZaza TaliashviliLarissa JangidzeRodney Thomas Cox
    • H01L29/08H01L29/00
    • H01L29/456H01L29/43
    • The use of liquid metal contacts for devices based on thermotunneling has been investigated. Electric and thermal characteristics of low wetting contact Hg/Si, and high wetting contacts Hg/Cu were determined and compared. Tunneling I-V characteristics for Hg/Si were obtained, while for Hg/Cu, I-V characteristics were ohmic. The tunneling I-V characteristic is explained by the presence of a nanogap between the contact materials. Heat conductance of high wetting and low wetting contacts were compared, using calorimeter measurements. Heat conductance of high wetting contact was 3-4 times more than of low wetting contact. Both electric and thermal characteristics of liquid metal contact indicated that it could be used for thermotunneling devices. To reduce the work function and make liquid metal more suitable for room temperature cooling, Cs was dissolved in liquid Hg. Work function as low as 2.6 eV was obtained.
    • 已经研究了使用液态金属触点作为基于热电穿孔的装置。 确定并比较了低湿接触Hg / Si和高湿接触Hg / Cu的电热特性。 获得Hg / Si隧道I-V特性,而对于Hg / Cu,I-V特性为欧姆。 隧道I-V特性由接触材料之间的纳米隙的存在来解释。 使用量热仪测量比较了高润湿和低湿接触的导热性。 高润湿接触的热传导是低湿接触的3-4倍。 液态金属触点的电气和热特性均表明它可用于热电偶穿孔装置。 为了降低功能,使液态金属更适合于室温冷却,Cs溶解在液态Hg中。 工作功能低至2.6 eV。
    • 3. 发明授权
    • Integrated direct drive starter/generator for turbines
    • 用于涡轮机的集成式直接驱动启动器/发电机
    • US08146369B2
    • 2012-04-03
    • US12291258
    • 2008-11-06
    • Hans Juergen WalitzkiJonathan Sidney EdelsonRodney Thomas Cox
    • Hans Juergen WalitzkiJonathan Sidney EdelsonRodney Thomas Cox
    • F02C7/26
    • F04D27/004F02C7/268H02K15/02Y10T29/49009
    • A starter/generator machine for a turbine with a turbine enclosure, an air duct, and a plurality of fan blades is provided. The starter/generator machine includes a plurality of stator elements spaced at intervals in a ring shape adjacent to the air duct and a plurality of rotor elements mounted on the fan blades. The stator elements and the rotor elements are mounted to interact magnetically to exert a force sufficient to move the rotor elements. The stator elements are shaped to minimize air flow interference and are formed with a core, at least one pole, and multiple windings. The spacing between the stator elements and the rotor elements forms an air gap on the order of 5-10 mm, and the number of stator elements is different from the number of rotor elements.
    • 提供了一种用于具有涡轮机壳体,空气管道和多个风扇叶片的涡轮机的起动/发电机。 起动机/发电机包括多个定子元件,它们以与空气管道相邻的环形间隔开,并且多个转子元件安装在风扇叶片上。 定子元件和转子元件被安装成磁力相互作用以施加足以移动转子元件的力。 定子元件成形为使空气流动干扰最小化并且形成有芯,至少一个极和多个绕组。 定子元件和转子元件之间的间隔形成大约5-10mm的气隙,并且定子元件的数量与转子元件的数量不同。
    • 4. 发明授权
    • Self-propelled undercarriage wheel having a low profile tire
    • 具有低轮胎轮胎的自行式底盘轮
    • US08109463B2
    • 2012-02-07
    • US12310609
    • 2007-08-29
    • Isaiah Watas CoxRodney Thomas CoxJoseph Jeremiah Cox
    • Isaiah Watas CoxRodney Thomas CoxJoseph Jeremiah Cox
    • B64C25/02
    • B64C25/405Y02T50/823Y10T29/4973
    • 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.
    • 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。
    • 5. 发明申请
    • SELF-PROPELLED UNDERCARRIAGE WHEEL HAVING A LOW PROFILE TIRE
    • 具有低轮廓轮胎的自行车底盘
    • US20100288873A1
    • 2010-11-18
    • US12310609
    • 2007-08-29
    • Isaiah Watas CoxRodney Thomas CoxJoseph Jeremiah Cox
    • Isaiah Watas CoxRodney Thomas CoxJoseph Jeremiah Cox
    • B64C25/50B23P11/00
    • B64C25/405Y02T50/823Y10T29/4973
    • 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.
    • 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。