AIRCRAFT PROPELLER BALANCING SYSTEM
    1.
    发明申请
    AIRCRAFT PROPELLER BALANCING SYSTEM 审中-公开
    飞机螺旋桨平衡系统

    公开(公告)号:WO2011046620A2

    公开(公告)日:2011-04-21

    申请号:PCT/US2010/002764

    申请日:2010-10-14

    Abstract: An aircraft system and method with a first counterweight rotating balancing rotor including holding stepping inboard magnets and outboard mass concentration, and a second counterweight rotating balancing rotor including holding stepping inboard magnets and outboard mass concentration. The system includes an.inboard electromagnetic coil driver with a first inboard electromagnetic coil, and a second inboard electromagnetic coil, the inboard electromagnetic coil driver and the first counterweight balancing rotor and the second counterweight balancing rotor centered around the aircraft propeller shaft rotating machine member with the first inboard electromagnetic coil proximate the first inboard magnets of the first counterweight balancing rotor, with the inboard electromagnetic coil driver proximate the rotation axis of the aircraft propeller shaft rotating machine member and the first counterweight balancing rotor outboard of the inboard electromagnetic coil driver with the first inboard electromagnetic coil generating a electromagnetic field to electromagnetically step the first inboard magnets of the at least first counterweight balancing rotor to electromagnetically actuate rotational movement of the first counterweight balancing rotor around the rotating machine member and relative to the inboard electromagnetic coil driver to a first rotor held balancing position. The second inboard electromagnetic coil is proximate the second counterweight balancing rotor, with the second inboard electromagnetic coil proximate the second inboard magnets of the second counterweight balancing rotor, wherein the second inboard electromagnetic coil generates an electromagnetic field to electromagnetically step the second inboard magnets of the second counterweight balancing rotor to electromagnetically actuate rotational movement of the second counterweight balancing rotor around the rotation axis and relative to the inboard electromagnetic coil driver and to a second rotor held position.

    Abstract translation: 具有第一配重旋转平衡转子的航空器系统和方法,第一平衡转子包括保持步进内侧磁体和外侧质量集中,以及第二平衡重旋转平衡转子包括保持步进内侧磁体和外侧质量集中。 该系统包括具有第一内侧电磁线圈和第二内侧电磁线圈的内侧电磁线圈驱动器,内侧电磁线圈驱动器和第一平衡重转子以及第二平衡重转子,所述第二平衡重平衡转子以飞行器螺旋桨轴旋转机器构件为中心, 所述第一内侧电磁线圈靠近所述第一配重平衡转子的所述第一内侧磁体,其中所述内侧电磁线圈驱动器靠近所述飞机螺旋桨轴旋转机器构件的所述旋转轴线,并且所述第一配重平衡转子与所述内侧电磁线圈驱动器的外侧 第一内侧电磁线圈产生电磁场以电磁地步进至少第一配重平衡转子的第一内侧磁体,以电磁地致动第一平衡重平衡转子围绕旋转机器m的旋转运动 余料并且相对于内侧电磁线圈驱动器转动到第一转子保持平衡位置。 第二内侧电磁线圈靠近第二平衡重平衡转子,第二内侧电磁线圈靠近第二平衡重转子的第二内侧磁体,其中第二内侧电磁线圈产生电磁场以电磁地步进第二平衡重平衡转子的第二内侧磁体 第二配重平衡转子,以电磁地致动第二配重平衡转子围绕旋转轴线且相对于内侧电磁线圈驱动器和第二转子保持位置的旋转运动。

    METHOD FOR BUILDING A MOTOR
    2.
    发明申请
    METHOD FOR BUILDING A MOTOR 审中-公开
    建立电机的方法

    公开(公告)号:WO2007030572A2

    公开(公告)日:2007-03-15

    申请号:PCT/US2006/034778

    申请日:2006-09-06

    Abstract: The present invention provides a method for building a component for an electrical rotating machine and comprises: providing powdered magnetic material; providing electrically conductive material; positioning the powdered magnetic material and the electrically conductive material within a mold functional to provide the materials with the required dimensions after application of a hot isostatic pressing (HIP) procedure; and applying at least one HIP procedure to the materials in the mold. Temperatures and pressures of the process are chosen to ensure that the electrically conducting and magnetic portions of the component are bonded without the materials seeping into each other. In one aspect the present invention thus provides a method for building small compact motor systems using motor components formed from pressed powder. A technical advantage of this approach is that the component has uniform grain structure and thus consistent magnetic and structural properties. The motor may be located inside a vehicle drive wheel, as it is equipped to be a drive motor providing the necessary torque with reasonable system mass. The motor systems of the invention may utilize polyphase electric motors, and are preferably connected to appropriate drive systems via mesh connections, to provide variable V/Hz ratios.

    Abstract translation: 本发明提供了一种用于构建用于旋转电机的部件的方法,并且包括:提供粉末状磁性材料; 提供导电材料; 将粉末状磁性材料和导电材料定位在模具内,以在施加热等静压(HIP)过程之后提供具有所需尺寸的材料; 并对模具中的材料应用至少一个HIP程序。 选择过程的温度和压力以确保部件的导电部分和磁性部分结合,而材料彼此不渗入。 在一方面,本发明因此提供了一种使用由压制粉末形成的电动机部件来构建小型紧凑型电动机系统的方法。 这种方法的技术优势在于该部件具有均匀的晶粒结构并且因此具有一致的磁性和结构性质。 电动机可以位于车辆驱动轮内,因为它装备成驱动电动机,以合理的系统质量提供必要的扭矩。 本发明的电动机系统可以使用多相电动机,并且优选地通过网状连接连接到适当的驱动系统,以提供可变的V / Hz比。

    SUN VISOR FOR MOTOR VEHICLE
    3.
    发明申请
    SUN VISOR FOR MOTOR VEHICLE 审中-公开
    SUV VISOR FOR MOTOR VEHICLE

    公开(公告)号:WO2005021304A1

    公开(公告)日:2005-03-10

    申请号:PCT/IB2004/002707

    申请日:2004-08-20

    CPC classification number: B60J3/0208

    Abstract: The invention relates to an accessory (10) for a motor vehicle visor (30) which includes a tinted, transparent sheet (12) element and mounting means whereby it can be mounted on a vehicle visor. In its mounted configuration on a vehicle visor it is displaceable between a first position, in which it is located within the perimeter of the visor, and a second position, in which it extends from the edge of the visor remote from the edge about which the visor is pivotally displaceable. With the visor in its operative configuration and the sheet element in its second position, the sheet element can serve to shield a vehicle driver's eyes against the rays of a low setting sun, a rising sun and oncoming vehicle headlights, while visibility through and around the sheet element still permits clear road visibility for driving purposes.

    Abstract translation: 本发明涉及一种用于机动车辆遮阳板(30)的附件(10),其包括有色透明片(12)元件和安装装置,由此可将其安装在车辆遮阳板上。 在其安装在车辆遮阳板上的构造中,其可位于其位于遮阳板周边内的第一位置和第二位置之间,第二位置从遮板的边缘远离边缘延伸, 遮阳板可枢转地移动。 当遮阳板处于其操作配置并且片材元件处于其第二位置时,片材元件可用于屏蔽车辆驾驶员的眼睛抵抗低太阳,冉冉升起的太阳和迎面而来的车辆前灯的光线,同时通过和围绕 板材仍然允许驾驶目的的清晰的道路可见性。

    AIRCRAFT PROPELLER BALANCING SYSTEM
    5.
    发明申请
    AIRCRAFT PROPELLER BALANCING SYSTEM 审中-公开
    飞机螺旋桨平衡系统

    公开(公告)号:WO2011046620A3

    公开(公告)日:2011-11-24

    申请号:PCT/US2010002764

    申请日:2010-10-14

    Abstract: An aircraft system and method with a first counterweight rotating balancing rotor including holding stepping inboard magnets and outboard mass concentration, and a second counterweight rotating balancing rotor including holding stepping inboard magnets and outboard mass concentration. The system includes an.inboard electromagnetic coil driver with a first inboard electromagnetic coil, and a second inboard electromagnetic coil, the inboard electromagnetic coil driver and the first counterweight balancing rotor and the second counterweight balancing rotor centered around the aircraft propeller shaft rotating machine member with the first inboard electromagnetic coil proximate the first inboard magnets of the first counterweight balancing rotor, with the inboard electromagnetic coil driver proximate the rotation axis of the aircraft propeller shaft rotating machine member and the first counterweight balancing rotor outboard of the inboard electromagnetic coil driver with the first inboard electromagnetic coil generating a electromagnetic field to electromagnetically step the first inboard magnets of the at least first counterweight balancing rotor to electromagnetically actuate rotational movement of the first counterweight balancing rotor around the rotating machine member and relative to the inboard electromagnetic coil driver to a first rotor held balancing position. The second inboard electromagnetic coil is proximate the second counterweight balancing rotor, with the second inboard electromagnetic coil proximate the second inboard magnets of the second counterweight balancing rotor, wherein the second inboard electromagnetic coil generates an electromagnetic field to electromagnetically step the second inboard magnets of the second counterweight balancing rotor to electromagnetically actuate rotational movement of the second counterweight balancing rotor around the rotation axis and relative to the inboard electromagnetic coil driver and to a second rotor held position.

    Abstract translation: 一种具有第一配重旋转平衡转子的飞行器系统和方法,包括保持踏板内侧磁体和外侧质量集中,以及包括保持踏板内侧磁体和外侧质量集中的第二配重旋转平衡转子。 该系统包括具有第一内侧电磁线圈的电子线圈驱动器和第二内置电磁线圈,内侧电磁线圈驱动器和第一配重平衡转子和第二配重平衡转子以飞机螺旋桨轴旋转机器构件为中心, 靠近第一配重平衡转子的第一内侧磁体的第一内侧电磁线圈,内侧电磁线圈驱动器靠近飞机驱动轴转动机构的旋转轴线,并且内侧电磁线圈驱动器的第一配重平衡转子外侧与 第一内侧电磁线圈产生电磁场以电磁步进所述至少第一配重平衡转子的第一内侧磁体,以电磁致动第一配重平衡转子围绕旋转机器m的旋转运动 并且相对于内侧电磁线圈驱动器到第一转子保持平衡位置。 第二内侧电磁线圈靠近第二配重平衡转子,其中第二内侧电磁线圈靠近第二对重平衡转子的第二内侧磁体,其中第二内侧电磁线圈产生电磁场以电磁地步进第二内侧磁体 第二配重平衡转子,用于电磁地驱动第二配重平衡转子围绕旋转轴线和相对于内侧电磁线圈驱动器和第二转子保持位置的旋转运动。

    AIRFOIL ASSEMBLY AND METHOD
    8.
    发明申请
    AIRFOIL ASSEMBLY AND METHOD 审中-公开
    航空组件和方法

    公开(公告)号:WO2015127300A1

    公开(公告)日:2015-08-27

    申请号:PCT/US2015/016948

    申请日:2015-02-20

    CPC classification number: B64C21/00 B64C23/005 Y02T50/166

    Abstract: Airfoil assemblies and methods of using them are provided to accelerate air flow relative to the airfoil assemblies and to improve laminar air flow over airfoils. The airfoil may include a cathode disposed near a leading portion of the airfoil to ionize on rushing air and for initiating an electric field. An anode disposed near an opposite portion of the airfoil completes the electric field to accelerate ionized air flowing relative to the airfoil, whereby ionized positively charged air particles tend to separate and accelerate continuously toward the anode in a substantially smooth laminar path of travel uninterruptedly. An air ionizing antenna may be employed for radiating an electromagnetic field transversely to the electric field to cause the electromagnetic field to ionize additional air flowing relative to the airfoil.

    Abstract translation: 提供翼型组件和使用它们的方法以加速相对于翼型组件的空气流动并且改善翼型件上的层流空气流动。 翼型件可以包括设置在翼型件的引导部分附近的阴极,以在冲刷空气中电离并用于启动电场。 设置在翼型件的相对部分附近的阳极完成电场以加速相对于翼型流动的电离空气,由此电离的带正电的空气颗粒倾向于在不间断的基本平滑的层流路径中朝向阳极分离和加速。 可以使用空气电离天线来辐射横向于电场的电磁场,以使电磁场离开相对于翼型流动的附加空气。

    ENDOTRACHEAL TUBE STABILIZER APPARATUS AND METHOD
    9.
    发明申请
    ENDOTRACHEAL TUBE STABILIZER APPARATUS AND METHOD 审中-公开
    内管式稳定器装置和方法

    公开(公告)号:WO2013040230A1

    公开(公告)日:2013-03-21

    申请号:PCT/US2012/055189

    申请日:2012-09-13

    CPC classification number: A61M16/0497

    Abstract: A neonatal endotracheal tube stabilizer has a tube cradle, a tube fixation element attached to said tube cradle and a stabilization bar having a plurality of engagement elements. The stabilization bar extends on either side of the tube cradle to engage two cheek pads. The cheek pads each have a releasable engagement interface dimensioned to engage the engagement elements of the stabilization rod in at least one engaged position. When so engaged, the cradle firmly holds the endotracheal tube in a position selected by a health care provider.

    Abstract translation: 新生儿气管插管稳定器具有管支架,连接到所述管支架的管固定元件和具有多个接合元件的稳定杆。 稳定杆在管支架的任一侧延伸,以接合两个脸颊垫。 面颊垫各自具有可释放的接合界面,其尺寸适于在至少一个接合位置中接合稳定杆的接合元件。 当这样接合时,摇篮将气管插管牢固地保持在由医疗保健提供者选择的位置。

    METHOD FOR BUILDING A MOTOR
    10.
    发明申请
    METHOD FOR BUILDING A MOTOR 审中-公开
    建立电机的方法

    公开(公告)号:WO2007030572A3

    公开(公告)日:2007-05-10

    申请号:PCT/US2006034778

    申请日:2006-09-06

    Abstract: The present invention provides a method for building a component for an electrical rotating machine and comprises: providing powdered magnetic material; providing electrically conductive material; positioning the powdered magnetic material and the electrically conductive material within a mold functional to provide the materials with the required dimensions after application of a hot isostatic pressing (HIP) procedure; and applying at least one HIP procedure to the materials in the mold. Temperatures and pressures of the process are chosen to ensure that the electrically conducting and magnetic portions of the component are bonded without the materials seeping into each other. In one aspect the present invention thus provides a method for building small compact motor systems using motor components formed from pressed powder. A technical advantage of this approach is that the component has uniform grain structure and thus consistent magnetic and structural properties. The motor may be located inside a vehicle drive wheel, as it is equipped to be a drive motor providing the necessary torque with reasonable system mass. The motor systems of the invention may utilize polyphase electric motors, and are preferably connected to appropriate drive systems via mesh connections, to provide variable V/Hz ratios.

    Abstract translation: 本发明提供了一种用于构建电动旋转机器的部件的方法,包括:提供粉末状磁性材料; 提供导电材料; 将粉末状磁性材料和导电材料定位在模具内,以在施加热等静压(HIP)程序之后提供具有所需尺寸的材料; 以及对模具中的材料施加至少一个HIP程序。 选择该过程的温度和压力以确保部件的导电和磁性部分粘合,而不会使材料彼此渗透。 在一个方面,本发明因此提供了一种使用由压粉形成的马达部件来构建小型紧凑型马达系统的方法。 该方法的技术优点是该组分具有均匀的晶粒结构,因此具有一致的磁性和结构性能。 马达可以位于车辆驱动轮内,因为其被配备为具有合理系统质量的必要扭矩的驱动马达。 本发明的电机系统可以使用多相电动机,并且优选地通过网状连接连接到适当的驱动系统,以提供可变的V / Hz比。

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