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    Flying device and a wing construction for the same
    55.
    发明授权
    Flying device and a wing construction for the same 有权
    飞行装置和翼结构相同

    公开(公告)号：US09308984B2

    公开(公告)日：2016-04-12

    申请号：US14006754

    申请日：2012-03-19

    申请人： Aki Suokas

    发明人： Aki Suokas

    IPC分类号： B64C1/26 ,  B64C3/56 ,  B64C31/028 ,  B64C39/06

    CPC分类号： B64C1/26 ,  B64C3/56 ,  B64C31/028 ,  B64C39/068

    摘要： Flying device, in which there is a fuselage (2, 2′), wings (8, 9), which are connected to each other to form an essentially looped structure, elements (4, 5) for creating a flying force, and the desired elements (e.g., 7, 7′) for controlling the flying device (1). The wings (8, 9) of the flying device (1) form a unified totality detachable from the fuselage (2, 2′). A wing construction is also included.

    摘要翻译： 具有彼此连接以形成基本环形结构的机身（2,2'），机翼（8,9）的飞行装置，用于产生飞行力的元件（4,5），以及 用于控制飞行装置（1）的所需元件（例如，7,7'）。 飞行装置（1）的翼（8,9）形成从机身（2,2'）可拆卸的统一的总体。 还包括机翼结构。

    MINIMIZING DRAG-INDUCED FORCES on a WHEELED VEHICLE
    56.
    发明申请
    MINIMIZING DRAG-INDUCED FORCES on a WHEELED VEHICLE 审中-公开
    在轮式车辆上最小化拖车诱发力

    公开(公告)号：US20160068015A1

    公开(公告)日：2016-03-10

    申请号：US14479699

    申请日：2014-09-08

    申请人： Garth L. MAGEE

    发明人： Garth L. MAGEE

    IPC分类号： B60B1/02 ,  B60C11/03 ,  B62D25/18 ,  B60B7/00 ,  B60B1/00 ,  B62D35/00

    CPC分类号： B62D35/00 ,  B60B1/00 ,  B60B1/003 ,  B60B1/02 ,  B60B1/0246 ,  B60B1/0261 ,  B60B1/041 ,  B60B1/06 ,  B60B3/00 ,  B60B3/007 ,  B60B3/02 ,  B60B3/08 ,  B60B3/10 ,  B60B7/00 ,  B60B7/0006 ,  B60B7/0066 ,  B60B2900/1216 ,  B60C11/03 ,  B60C11/0302 ,  B60C11/0306 ,  B60C11/0327 ,  B60C11/11 ,  B60C19/00 ,  B60C2011/0337 ,  B60C2200/10 ,  B60C2200/14 ,  B60Y2200/13 ,  B62D25/18 ,  B62D35/005 ,  B63B1/322 ,  B64C1/0009 ,  B64C31/028 ,  Y02T10/88 ,  Y10T29/49492

    摘要： An aerodynamically optimized drag-reduction apparatus for optimally reducing the drag-induced resistive forces upon a terrestrial vehicle, where the drag-induced resistive moments on wheel surfaces pivoting about the stationary point of ground contact are reduced, and the vehicle propulsive forces needed to countervail the resistive forces on the wheel are reduced. The drag reduction apparatus includes: a streamlined fairing positioned on a vehicle to shield the faster moving upper wheel surfaces from headwinds; an engine exhaust pipe disposed on a vehicle whereby exhaust gases deflect headwinds to shield the faster moving upper wheel surfaces of an automotive wheel; an automotive spoked wheel having streamlined oval-shaped wheel spokes; a streamlined spoke tailfin rotatably attached to a wheel spoke; a cycle wheel with a tapered spoke having a thin aerodynamic profile near the rim and tapering to a round profile towards the central hub; and a tire having streamlined tread blocks arranged in an aerodynamic pattern.

    摘要翻译： 一种空气动力优化的减阻装置，用于最佳地减小地面车辆上的阻力感应阻力，其中围绕地面接触点的静止点枢转的车轮表面上的阻力引起的阻力矩减小，并且需要抵抗车辆的推进力 车轮上的阻力减小。 减阻装置包括：位于车辆上的流线型整流罩，用于屏蔽快速移动的上轮表面与逆风; 设置在车辆上的发动机排气管，由此排气偏转逆风以屏蔽汽车轮的更快移动的上轮表面; 汽车喇叭轮具有流线型的椭圆形轮辐; 一个可旋转地连接到轮辐的流线型辐条尾巴; 具有锥形轮辐的循环轮在轮缘附近具有薄的空气动力学轮廓并且朝着中心轮毂逐渐变细到圆形轮廓; 以及具有以空气动力学模式布置的流线型胎面花纹块的轮胎。

    System for Airboarding Behind an Aircraft
    57.
    发明申请
    System for Airboarding Behind an Aircraft 审中-公开
    飞机背后的飞机系统

    公开(公告)号：US20150266573A1

    公开(公告)日：2015-09-24

    申请号：US14656648

    申请日：2015-03-12

    申请人： Aaron Wypyszynski

    发明人： Aaron Wypyszynski

    IPC分类号： B64C31/02 ,  B64C13/04 ,  B64C25/06 ,  B64C25/34 ,  B64D3/00 ,  B64D17/80

    CPC分类号： B64D17/80 ,  B64C31/028 ,  B64C39/026 ,  B64D3/00

    摘要： A system for airboarding and performing stunts behind an aircraft includes a lifting board, a handle, and a tow rope connected to the board and handle. The lifting board may include landing gear, a binding for securing an operator to the board, tail sections for stabilizing the board during flight, and ailerons for facilitating turns and rolls. The system may include a control system integrated into the handle and board that improves the operator's ability to control the board.

    摘要翻译： 飞机背后的飞行和执行特技的系统包括提升板，手柄和连接到板和手柄的拖绳。 提升板可以包括起落架，用于将操作者固定到板的装订，用于在飞行期间稳定板的尾部部分和用于便于转动和滚动的副翼。 该系统可以包括集成到手柄和板中的控制系统，其提高操作者控制电路板的能力。

    METHOD and APPARATUS for MINIMIZING DRAG-INDUCED FORCES on a WHEELED VEHICLE
    59.
    发明申请
    METHOD and APPARATUS for MINIMIZING DRAG-INDUCED FORCES on a WHEELED VEHICLE 审中-公开
    用于在车轮上最小化DRAG诱发力的方法和装置

    公开(公告)号：US20140265431A1

    公开(公告)日：2014-09-18

    申请号：US13799005

    申请日：2013-03-13

    申请人： Garth L. Magee

    发明人： Garth L. Magee

    IPC分类号： B62D35/00 ,  B60B7/00 ,  B60C11/03 ,  B60B1/00

    CPC分类号： B62D35/00 ,  B60B1/00 ,  B60B1/003 ,  B60B1/02 ,  B60B1/0246 ,  B60B1/0261 ,  B60B1/041 ,  B60B1/06 ,  B60B3/00 ,  B60B3/007 ,  B60B3/02 ,  B60B3/08 ,  B60B3/10 ,  B60B7/00 ,  B60B7/0006 ,  B60B7/0066 ,  B60B2900/1216 ,  B60C11/03 ,  B60C11/0302 ,  B60C11/0306 ,  B60C11/0327 ,  B60C11/11 ,  B60C19/00 ,  B60C2011/0337 ,  B60C2200/10 ,  B60C2200/14 ,  B60Y2200/13 ,  B62D25/18 ,  B62D35/005 ,  B63B1/322 ,  B64C1/0009 ,  B64C31/028 ,  Y02T10/88 ,  Y10T29/49492

    摘要： An aerodynamically optimized drag-reduction means and method for optimal minimization of the drag-induced resistive forces upon a terrestrial vehicle wheel, where the drag-induced resistive moments on wheel surfaces pivoting about the point of ground contact are reduced, and the vehicle propulsive forces needed to countervail the resistive forces on the wheel are reduced. The drag reduction means includes: a streamlined wheel cover positioned on a vehicle to shield the faster moving upper wheel surfaces from headwinds; a streamlined wind-deflecting fairing positioned on a vehicle to shield the faster moving upper wheel surfaces from headwinds; an engine exhaust pipe diposed on a vehicle whereby exhaust gases deflect headwinds to shield the faster moving upper wheel surfaces of an automotive wheel; an automotive spoked wheel having streamlined oval-shaped wheel spokes arranged in one or more rows for greater axial strength; a streamlined tailfin rotatably attached to a wheel spoke, which thereby may pivot about the spoke in response to varying crosswinds; and a tire having streamlined tread blocks arranged in an aerodynamic pattern.

    摘要翻译： 一种空气动力学优化的减阻装置和方法，用于最佳地最小化地面车轮上的阻力感应阻力，其中围绕地面接触点枢转的车轮表面上的阻力引起的阻力矩减小，并且车辆推进力 需要抵抗车轮上的阻力减小。 减阻装置包括：定位在车辆上的流线型车轮罩，以防止更快的移动的上轮表面与逆风; 一种位于车辆上的流线型的风向整流罩，用于屏蔽更快的移动的上轮表面与逆风; 发动机排气管沾在车辆上，由此废气偏转逆风以屏蔽汽车轮的更快移动的上轮面; 具有流线型椭圆形轮辐的汽车发条轮，其布置成一行或多行以获得更大的轴向强度; 可旋转地附接到轮辐的流线型尾翼，其可响应于不同的侧风而围绕辐条枢转; 以及具有以空气动力学模式布置的流线型胎面花纹块的轮胎。

    Light plane in the ultralight category and sport plane category
    60.
    发明授权
    Light plane in the ultralight category and sport plane category 有权
    轻型飞机在超轻型类和运动型飞机类

    公开(公告)号：US08210466B2

    公开(公告)日：2012-07-03

    申请号：US10554309

    申请日：2004-04-13

    申请人： Hans Gygax

    发明人： Hans Gygax

    IPC分类号： B64C1/00

    CPC分类号： B64C31/028

    摘要： This light aeroplane at the same time fulfilled the weight limits for the European ultra light class or acolyte class as do at the same time for the US-American sport plan Category. It comprises an engine arranged at the nose and is provided with tractor airscrew and the cabin cell that is arranged behind the engine and is wide enough for two adjacent passenger seats. A central tube (1) with a 200 mm diameter extends forwards towards the engine and to the rear at least behind the front edge of the lateral rudder and elevator control. Everything else is constructed around said tube. A square profiled element (12) is transversally guided edgeways beneath the central tube (1) and is rigidly connected to the same in a positively engaged manner. An upwardly projecting tube bend (11), which arches over the length of the square profiled element is fixed to the rear side of the square profiled element (12) with the ends thereof. The level of a virtual plane cabin floor is defined above the square profile (12). The free space above said floor is orthorhombic: at least 190 cm long, at least 45 cm wide and at least 40 cm high.

    摘要翻译： 同时，这架轻型飞机也同时满足了欧美超轻型飞机等级的要求，同时也适用于美国的美式运动计划类别。 它包括布置在鼻子处的发动机，并且设置有拖拉机螺旋桨和布置在发动机后面并且对于两个相邻乘客座椅足够宽的舱室单元。 具有200mm直径的中心管（1）至少在侧向舵和电梯控制的前边缘之后朝向发动机向后延伸。 其他一切都是围绕所述的管子构成的。 方形异形元件（12）在中心管（1）下方横向引导，并以正向接合的方式与其刚性连接。 在方形异形元件的长度上拱起的向上突出的管弯头（11）的端部固定到方形异形元件（12）的后侧。 虚拟飞机舱底板的水平面定义在方形轮廓（12）的上方。 地板上方的自由空间是斜方晶的：至少190厘米长，至少45厘米宽和至少40厘米高。