利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

106 条记录 (耗时 0.013 秒)

    DRAGONFLY UNMANNED AERIAL VEHICLE
    22.
    发明申请
    DRAGONFLY UNMANNED AERIAL VEHICLE 审中-公开
    无人驾驶的远程车辆

    公开(公告)号：US20110278391A1

    公开(公告)日：2011-11-17

    申请号：US12781039

    申请日：2010-05-17

    申请人： Andrey KOTLER

    发明人： Andrey KOTLER

    IPC分类号： B64C33/00

    CPC分类号： B64C39/028 ,  B64C33/02 ,  B64C2201/025 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/127

    摘要： A micro aerial vehicle apparatus capable of flying in different flight modes is disclosed. The apparatus includes a fuselage; at least one pair of blade-wings; and an actuator for actuating the blade-wings by flapping the blade-wings in dissonance or resonance frequencies.

    摘要翻译： 公开了能够以不同飞行模式飞行的微型飞行器具。 该装置包括机身; 至少一对叶片翼; 以及致动器，用于通过以不相干或共振频率拍打叶片翼来致动叶片翼。

    Man-powered ornithopter-sailplane
    23.
    发明授权
    Man-powered ornithopter-sailplane 失效
    人造鸟类飞机

    公开(公告)号：US07410121B2

    公开(公告)日：2008-08-12

    申请号：US10571399

    申请日：2004-05-31

    申请人： Remigijus Dainys

    发明人： Remigijus Dainys

    IPC分类号： B64C33/00

    CPC分类号： B64C33/025 ,  B64C33/00

    摘要： A man-powered ornithopter-sailplane, which has one or two pair of flapping wings and a hang-glider wing wherein substantially novel femoral and humeral muscular propulsion engines with the aid of which the body members connected thereto form integrated moving-flying and controlling-guiding mechanisms. Femoral arms are fixed to the torso base from which the movements for the wings flapping with respect to axles inclined to a horizontal direction are transmitted through the intermediate links of a kinematic chain. The wings comprise a row of rotational rods arranged therein and provided with elastic feather-like panels which produced during flapping, in a closed or turned position thereof, aerodynamic profiles and corresponding lifting and propulsion aerodynamic forces. The controlling-guiding movements are transmitted from the humeral arms to the flapping wings using movable ball joints. The diversity of movements of the femoral arms, humeral arms, hang-glider wing make it possible to control the flight.

    摘要翻译： 具有一对或两对拍动翼和悬挂式滑翔机翼的人造鸟类飞机，其中基本上是新颖的股骨和肱骨肌肉推进发动机，借助于此与其连接的身体构件形成集成的移动飞行和控制 - 指导机制。 股骨臂固定在躯体基座上，相对于倾斜于水平方向的轴的翼的运动从该躯体基座传播通过运动链的中间环节。 翼片包括一排设置在其中的旋转杆，并且设置有弹性羽毛状面板，其在关闭或转动位置中在拍打期间产生空气动力学特性和相应的提升和推进空气动力。 控制引导运动使用可移动的球窝接头从肱骨臂传递到扑翼。 股骨臂，肱骨臂，悬挂滑翔机翼的运动多样化，可以控制飞行。

    Rotating wing apparatus
    24.
    发明申请
    Rotating wing apparatus 审中-公开
    旋翼机

    公开(公告)号：US20080078860A1

    公开(公告)日：2008-04-03

    申请号：US11518966

    申请日：2006-09-11

    申请人： Phillip Createman

    发明人： Phillip Createman

    IPC分类号： B64C33/00

    CPC分类号： B64C11/00 ,  B63H1/04

    摘要： A rotating wing apparatus comprises two identical rectangular flat panels, each panel having planar surfaces, and each panel having an axis of rotation that passes lengthwise through the middle of the panel such that the axis is parallel to and equidistant from the longer edges of the panel. The operation of the apparatus begins with the panels lying flat side-by-side, with a longer edge of each panel abutted against a longer edge of the other panel. The panels then “fold downwards” with respect to each other, hinging at the abutted longer edges, such that each panel rotates about its axis at the same rate as the other panel but in a direction opposite that of the other panel, and such that the axes move towards each other, until a surface of each panel comes flat against a surface of the other panel. From this point the abutted longer edges of the panels now separate from each other, and the other longer edges of the panels then abut and hinge upon each other, such that the axes now move away from each other, until the panels again lie flat side by side, at which point the apparatus would again look like it did at the beginning of the operation except with the positions of the edges and surfaces of each panel reversed, and the panels continuing to hinge at the longer edges. The panels continue to rotate in this manner.

    摘要翻译： 旋转翼装置包括两个相同的矩形平板，每个面板具有平面表面，并且每个面板具有沿纵向方向穿过面板的中间的旋转轴线，使得该轴线平行于面板的较长边缘并且等距离 。 设备的操作开始于平面并排放置的面板，每个面板的较长边缘抵靠另一个面板的较长边缘。 然后，面板相对于彼此“折叠”，在邻接的较长边缘处铰接，使得每个面板以与另一个面板相同的速度绕其轴线旋转，但是在与另一个面板相反的方向上旋转，并且使得 轴彼此相对移动，直到每个面板的表面平坦地抵靠另一个面板的表面。 从这一点上，面板的相邻的较长边缘现在彼此分离，并且面板的另一个较长边缘随后彼此邻接并铰接，使得轴线现在彼此远离，直到面板再次平放 在这一点上，设备将再次看起来像在操作开始时所做的，除了每个面板的边缘和表面的位置反转，并且面板在更长的边缘上继续铰链。 面板继续以这种方式旋转。

    Human powered hang glider
    25.
    发明授权
    Human powered hang glider 失效
    人力悬挂滑翔机

    公开(公告)号：US4417707A

    公开(公告)日：1983-11-29

    申请号：US342833

    申请日：1982-01-26

    申请人： Ken Leong

    发明人： Ken Leong

    IPC分类号： B64C31/028 ,  B64C33/00 ,  B64C31/02

    CPC分类号： B64C33/00 ,  B64C31/028 ,  Y10S244/90

    摘要： A human powered hang glider (10) has a fixed wing portion (12) and a pair of movable wing portions (14, 16). Flexible sheet material (26, 28) is connected to trailing edges (30, 32) of the movable wing portions (14, 16). A support structure (34, 36) for the flexible sheet material (26, 28) overlies each flexible sheet material (26, 28). Elastic bands (52) and wires (74, 76) are connected in opposing relationship to the movable wing portions (14, 16) to allow reciprocation of the movable wing portions (14, 16). When the flexible bands (52) cause upward movement of the movable wing portions (14, 16) the flexible sheet members (26, 28) move away from their associated support structures (34, 36), allowing air to pass through the support structures (34, 36). When pilot (70 pulls on wires (74, 76) to move the movable wing portions (14, 16) downward, the flexible sheet portions (26, 28) move against their associated support structures (34, 36) to provide increased lift from the movable wing portions (14, 16). In a typical flight, these movements are performed occasionally, and the hang glider is otherwise launched, flown and landed in a conventional manner.

    摘要翻译： 人力悬挂滑翔机（10）具有固定翼部（12）和一对可动翼部（14,16）。 柔性片材（26,28）连接到可动翼部分（14,16）的后缘（30,32）。 用于柔性片材（26,28）的支撑结构（34,36）覆盖每个柔性片材（26,28）。 弹性带（52）和电线（74,76）以可动翼部（14,16）相对的关系连接，以允许可动翼部（14,16）的往复运动。 当柔性带（52）引起可动翼部分（14,16）的向上移动时，柔性片件（26,28）远离其相关联的支撑结构（34,36）移动，允许空气通过支撑结构 （34,36）。 当飞行员（70）拉动导线（74,76）以向下移动可动翼部分（14,16）时，柔性片部分（26,28）抵靠其相关联的支撑结构（34,36）移动，以提供从 可移动翼部（14,16），在典型的飞行中，这些运动偶尔进行，悬挂滑翔机以其它方式发射，以常规的方式飞行着陆。