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    ORNITHOPTER
    33.
    发明申请
    ORNITHOPTER 有权

    公开(公告)号：US20160009389A1

    公开(公告)日：2016-01-14

    申请号：US14759321

    申请日：2014-02-19

    Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.

    Inventor： Satoshi KURODA ,  Tomoyuki MORI ,  Kazuya HATTORI ,  Masato TAHARA ,  Oki TAKAYAMA

    IPC: B64C33/02

    CPC classification number: B64C33/02 ,  A63H27/008 ,  B64C2201/025

    Abstract: An ornithopter includes a main wing mounted on a fuselage, and a control system configured to control a flapping motion of the main wing. The main wing includes an inner spar, an outer spar, and a wrist portion disposed between the inner spar and the outer spar and which varies a bending angle, which is a relative angle between the inner spar and the outer spar, within a predetermined angle range. The control system includes an actuator which performs a raising motion and a lowering motion of the inner spar by moving the inner spar in an upward direction and in a downward direction, an angle sensor which measures the bending angle, and a control unit which controls the actuator to move the inner spar in response to the measured bending angle.

    Abstract translation: 一种鸟巢器包括安装在机身上的主翼，以及配置成控制主翼的扑动运动的控制系统。 主翼包括内翼梁，外翼梁和设置在内翼梁和外翼梁之间的腕部，并且在预定角度内改变作为内翼梁和外翼梁之间的相对角度的弯曲角度 范围。 该控制系统包括：致动器，其通过沿向上方向和向下方向移动内部翼梁来执行内部翼梁的升高运动和下降运动;角度传感器，其测量弯曲角度;以及控制单元， 致动器以响应于测量的弯曲角度来移动内部翼梁。

    Ornithopter
    35.
    发明申请
    Ornithopter 审中-公开

    公开(公告)号：US20110079677A1

    公开(公告)日：2011-04-07

    申请号：US12924592

    申请日：2010-09-30

    Applicant: Nathan J. Chronister

    Inventor： Nathan J. Chronister

    IPC: B64C33/00

    CPC classification number: B64C39/028 ,  A63H27/008 ,  B64C2201/025

    Abstract: The claimed invention is an ornithopter with three improvements over previous designs. First, it has a more efficient wing. Instead of using a heavy bracing rod to regulate the flexibility of the wing, it uses a lightweight cable tension system. Second, it has a steering mechanism that separates the servos from the tail itself, reducing the likelihood of damage in the event of a crash. Third, the ornithopter has a modular design, which allows more control over the external appearance of the model. Various bodies can be used with the same drive mechanism, and it permits the individual hobbyist or the kit manufacturer to produce additional body designs without having to take on the complex task of designing a new flapping mechanism.

    Abstract translation: 所要求保护的发明是具有对先前设计的三个改进的鸟巢车。 首先，它有一个更有效的翼。 它不是使用重型支撑杆来调节机翼的灵活性，而是使用轻型电缆张力系统。 第二，它具有将舵机与尾部本身分离的转向机构，从而减少在发生坠机事故时损坏的可能性。 第三，鸟巢车具有模块化设计，可以更好地控制车型的外观。 可以使用具有相同驱动机构的各种身体，并且允许个体爱好者或套件制造商生产额外的身体设计，而不必承担设计新的扑动机构的复杂任务。

    FLYING WING ROTATION MECHANISM OF MICRO AIR VEHICLE
    36.
    发明申请
    FLYING WING ROTATION MECHANISM OF MICRO AIR VEHICLE 审中-公开
    微型空中飞行器的飞行旋转机构

    公开(公告)号：US20070210207A1

    公开(公告)日：2007-09-13

    申请号：US11748635

    申请日：2007-05-15

    Applicant: Wei-Hsiang LIAO

    Inventor： Wei-Hsiang LIAO

    IPC: B64C33/00

    CPC classification number: B64C33/02 ,  B64C39/028 ,  B64C2201/025 ,  B64C2201/042

    Abstract: A flying wing rotation mechanism of a micro air vehicle is driven under a control of a power module and a detent member. The flying wing rotation mechanism of a micro air vehicle includes a flapping arm and a flying wing. The flapping arm is connected to the detent member, and swings as the power module drives the detent member. An end of the flying wing is pivoted to the flapping arm. When the flapping arm swings, the flying wing swings with the flapping arm in sync. When swing direction of the flapping arm changes, the flying wing rotates relative to an axial direction of the flapping arm.

    Abstract translation: 微型飞行器的飞翼旋转机构在功率模块和制动构件的控制下被驱动。 微型飞行器的飞翼旋转机构包括拍动臂和飞翼。 拍动臂连接到止动构件，并且当电源模块驱动制动构件时摆动。 飞翼的末端枢转到拍动臂。 当摇摆臂摆动时，飞翼与颤动臂同步摆动。 当摆动臂的摆动方向改变时，飞翼相对于拍动臂的轴向旋转。

    Ornithopter with independently controlled wings
    37.
    发明申请
    Ornithopter with independently controlled wings 审中-公开
    具有独立控制翅膀的Ornithopter

    公开(公告)号：US20050269447A1

    公开(公告)日：2005-12-08

    申请号：US11147044

    申请日：2005-06-07

    Applicant: Nathan Chronister

    Inventor： Nathan Chronister

    IPC: B64C33/00 ,  B64C33/02 ,  B64C39/02

    CPC classification number: B64C39/028 ,  B64C33/02 ,  B64C2201/025 ,  B64C2201/042 ,  B64C2201/141 ,  B64C2201/146

    Abstract: The invention described here offers a more effective method of ornithopter flight control. To accomplish this, the ornithopter has dual microprocessor-controlled drive systems for flapping the wings independently of each other. Various wing movements can cause the ornithopter to turn, roll, or pitch up or down. Weight and complexity are reduced by eliminating the need for servo-controlled tail surfaces.

    Abstract translation: 这里描述的发明提供了一种更有效的鸟虱飞行控制方法。 为了实现这一点，鸟巢车具有双微处理器控制的驱动系统，用于彼此独立地扑翼。 各种机翼动作可能会导致鸟类玩家向上或向下转动，滚动或俯仰。 通过不需要伺服控制的尾部表面来减轻重量和复杂性。

    Moving apparatus
    38.
    发明申请
    Moving apparatus 审中-公开
    移动装置

    公开(公告)号：US20050151010A1

    公开(公告)日：2005-07-14

    申请号：US10769304

    申请日：2004-01-30

    Applicant: Masaki Hamamoto ,  Yoshiji Ohta ,  Keita Hara

    Inventor： Masaki Hamamoto ,  Yoshiji Ohta ,  Keita Hara

    IPC: B25J5/00 ,  B64C33/02 ,  B64C39/02 ,  H02N2/00

    CPC classification number: B64C33/02 ,  B64C39/028 ,  B64C2201/025 ,  B64C2201/044 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146

    Abstract: On a main body portion of a fluttering apparatus, a wing (left wing) is formed which has a front wing shaft, a rear wing shaft and a wing film provided spreading over the front and rear wing shafts. Further, on the main body portion, a rotary actuator for driving the front wing shaft and a rotary actuator for: driving the rear wing shaft are mounted. The front (rear) wing shafts reciprocate in a plane orthogonally crossing an axis of rotation with the actuator serving as the fulcrum. Thus, a moving apparatus is obtained which has superior maneuverability and can move not hindered by any obstacle or geometry both indoors and outdoors.

    Abstract translation: 在飘动装置的主体部分上，形成有一个翼翼（左翼），其具有前翼轴，后翼轴和设置在前翼和后翼轴上的翼片。 此外，在主体部分上安装有用于驱动前翼轴的旋转致动器和用于驱动后翼轴的旋转致动器。 前（后）翼轴在与作为支点的致动器正交的旋转轴线的平面中往复运动。 因此，获得具有优异的机动性并且可以在室内和室外不受任何障碍物或几何形状阻碍的移动装置。

    Compressed air engine and flying object equipped therewith
    39.
    发明授权
    Compressed air engine and flying object equipped therewith 失效
    压缩空气发动机和配备的飞行物体

    公开(公告)号：US06530541B1

    公开(公告)日：2003-03-11

    申请号：US10167728

    申请日：2002-06-11

    Applicant: Jong Bok Woo ,  Ja Kook Koo ,  Kwang Joon Yoon ,  Yun Je Kim

    Inventor： Jong Bok Woo ,  Ja Kook Koo ,  Kwang Joon Yoon ,  Yun Je Kim

    IPC: B64C3300

    CPC classification number: F01B17/02 ,  A63H27/008 ,  A63H29/16 ,  B64C33/025 ,  B64C39/028 ,  B64C2201/025 ,  B64D27/02

    Abstract: A compressed air engine and a flying object using the engine are disclosed. The flying object includes the following elements. That is, the compressed air engine includes: a top member 11 provided with an air inlet 16; an upper cylinder 12; a lower cylinder 13; a bottom member 14; an air pipe, for passing of a compressed air; a shuttle 20 for performing up/down movements within a cylinder formed by the upper and lower cylinders; and a pair of pistons 21a and 21b over and under the shuttle respectively. The pair of the wings are symmetrically and pivotally assembled to the shuttle and the lower cylinder through securing shafts so as to perform up/down movements in accordance with the up/down movements of the shuttle. A compressed air container 2 is assembled to the bottom of the bottom member, for storing the compressed air.

    Abstract translation: 公开了使用该发动机的压缩空气发动机和飞行物体。 飞行物体包括以下元件。 也就是说，压缩空气发动机包括：设置有进气口16的顶部构件11; 上筒12; 下筒13; 底部构件14; 用于通过压缩空气的空气管; 用于在由上下缸形成的缸内进行升/降运动的梭20; 以及分别在梭子上方和下方的一对活塞21a和21b。 一对翼通过固定轴对称地和枢转地组装到梭子和下部圆筒上，以便根据梭子的上下运动来进行上/下移动。 压缩空气容器2组装到底部件的底部，用于储存压缩空气。

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