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    PASSIVE TORQUE BALANCING IN A HIGH-FREQUENCY OSCILLATING SYSTEM
    151.
    发明申请
    PASSIVE TORQUE BALANCING IN A HIGH-FREQUENCY OSCILLATING SYSTEM 审中-公开
    在高频振荡系统中的被动扭矩平衡

    公开(公告)号：WO2011142864A2

    公开(公告)日：2011-11-17

    申请号：PCT/US2011/024479

    申请日：2011-02-11

    Applicant: PRESIDENT AND FELLOWS OF HARVARD COLLEGE ,  SREETHARAN, Pratheev ,  WOOD, Robert

    Inventor： SREETHARAN, Pratheev ,  WOOD, Robert

    IPC: B64C33/02

    CPC classification number: B64C33/02 ,  B64C33/00 ,  B64C39/028 ,  B64C2201/025 ,  Y10T74/18928 ,  Y10T74/18968

    Abstract: A passively torque-balanced device includes (a) a frame; (b) a drivetrain including a drive actuator mounted to the frame and configured for reciprocating displacement, an input platform configured for displacement by the drive actuator, a plurality of rigid links, including a proximate link and remote links, wherein the rigid links are collectively mounted to the frame, and a plurality of joints joining the rigid links and providing a plurality of non-fully actuated degrees of freedom for displacement of the rigid links, the plurality of joints including a fulcrum joint that is joined both to the input platform and to the proximate rigid link; and (c) at least two end effectors respectively coupled with the remote links and configured for displacement without full actuation.

    Abstract translation: 无源扭矩平衡装置包括（a）框架; （b）动力传动系，其包括安装到所述框架并被构造成用于往复运动的驱动致动器，构造成用于由所述驱动致动器移位的输入平台，包括邻近链节和远程链节的多个刚性连杆，其中所述刚性连杆集体 安装到框架上的多个接头以及连接刚性连杆并提供多个非完全致动的刚性连杆自由度的多个接头，所述多个接头包括支撑接头，该支点接合到输入平台和 到邻近的刚性连接; 和（c）至少两个末端执行器，其分别与远程链接联接并被配置为在没有完全致动的情况下进行位移。

    RESONANCE ENGINE
    152.
    发明申请
    RESONANCE ENGINE 审中-公开
    谐振发动机

    公开(公告)号：WO2011073659A1

    公开(公告)日：2011-06-23

    申请号：PCT/GB2010/052100

    申请日：2010-12-15

    Applicant: GREENYER, Guy, Thomas

    Inventor： GREENYER, Guy, Thomas

    IPC: B64C33/02 ,  B64C39/02

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

    Abstract: A resonance engine is disclosed comprising: a driver plate (12), to which is coupled at least one oscillatory transducer (14); a drive signal generator connected to the oscillatory transducer for excitation thereof; a first spring-mass resonator, having a first natural resonant frequency, with a proximal end attached to the driver plate (12) and a free distal end; and a reaction means attached to the driver plate substantially opposite to the first spring-mass resonator. When the oscillatory transducer (14) is excited by a drive signal from the generator having a component at or close to said natural resonant frequency, the first spring-mass resonator oscillates at resonance, substantially in anti -phase to the driver plate (12). Small vibrational strains in the oscillatory transducer (14) are converted to large strains of controllable kinematic movements.

    Abstract translation: 公开了一种共振发动机，包括：驱动器板（12），其耦合到至少一个振荡换能器（14）; 驱动信号发生器连接到振荡换能器以用于激励; 第一弹簧质量谐振器，具有第一自然谐振频率，其近端附接到驱动器板（12）和自由远端; 以及附接到驱动器板的基本上与第一弹簧质量谐振器相对的反作用装置。 当振荡换能器（14）被来自具有等于或接近于所述固有谐振频率的分量的发生器的驱动信号激发时，第一弹簧 - 质量谐振器基本上以相位振荡器振荡，基本上与驱动器板（12）反相， 。 振荡换能器（14）中的小振动应变被转换为大的可控运动运动。

    RESONANCE DRIVE FOR A WINGBEAT ARRANGEMENT
    153.
    发明申请
    RESONANCE DRIVE FOR A WINGBEAT ARRANGEMENT 审中-公开
    共振驱动器SHOCK WING安排

    公开(公告)号：WO2009024115A3

    公开(公告)日：2009-06-25

    申请号：PCT/DE2008001247

    申请日：2008-07-27

    Applicant: GONZALEZ DE MENDOZA Y KAEDING ADRIAN CARLOS

    Inventor： GONZALEZ DE MENDOZA Y KAEDING ADRIAN CARLOS

    IPC: B64C33/02

    CPC classification number: B64C39/024 ,  B63H3/002 ,  B64C33/02 ,  B64C2201/025 ,  B64C2201/042

    Abstract: A wingbeat arrangement, particularly for use with a flying device, with one or more wings beating back and forth and with a restoring force device, which is coupled thereto and is configured to counter a deflection of the beating wings from at least one assigned starting position with a restoring force, characterized in that this back and forth movement is initiated, maintained or retarded by a controllable driving mechanism and, after or during the initiation of driving energy, over at least one sensory device, a conclusion is reached concerning the resulting amplitude, the instantaneous position or the frequency of the beating wings and the information, supplied by this sensory device, is used to influence the energy content, the direction of action or the development of this or a subsequent impulse as a function of time by means of a control system in such a manner, that the resulting amplitude or frequency of the wings oscillations approaches a value specified by the control system.

    Abstract translation: 设置冲击叶片组件，特别是用于在飞行器中，具有一个或多个往复扑翼和一个与其耦合的恢复力装置，其被配置成在至少一个相应的分配的起始位置，相对的恢复力的扑翼的偏转，其特征在于它 是往复通过可控驱动激发运动，在过渡保持或减速，并且之后或通过至少一个感觉装置引入驱动能量对所得到的振幅时，当前位置或所述叶片振动的频率被关闭并且这个感官 提供的信息服务装置来影响能量含量，有效的方向或这个或的后续冲击力随时间的变化由控制器的装置，使得所得的振幅或频率F1的 gelschwingung一个由所述控制值的方法预先确定。

    MECHANISM FOR BIAXIAL ROTATION OF A WING AND VEHICLE CONTAINING SUCH MECHANISM
    154.
    发明申请
    MECHANISM FOR BIAXIAL ROTATION OF A WING AND VEHICLE CONTAINING SUCH MECHANISM 审中-公开
    包含这种机构的翼和车的双轴旋转机构

    公开(公告)号：WO2008010830A9

    公开(公告)日：2008-07-17

    申请号：PCT/US2006043294

    申请日：2006-11-08

    Applicant: UNIV DELAWARE TECHNOLOGY CORP ,  AGRAWAL SUNIL K ,  MCINTOSH SEAN ,  KHAN ZAEEM

    Inventor： AGRAWAL SUNIL K ,  MCINTOSH SEAN ,  KHAN ZAEEM

    IPC: B64C33/00 ,  B64C33/02

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

    Abstract: A vehicle with wings and a mechanism for causing a flapping motion in wings. Each wing structure comprises a wing and a wing spar coupled to a follower via a resilient member. Each wing carrier is pivotally connected to the body and is configured to restrain lateral movement and permit rotation of the wing spar about a feathering axis. A biasing member provides torsional bias to each wing spar. A linkage, driven by an actuator, transmits cyclic motion that rotates the wing carrier about a flapping axis, which moves the follower along a follower path. A guide attached to the vehicle body lies in the path of each follower, and the follower and guide are shaped such that each wing spar has a first rotational position about its axis along a first portion of the follower path and a second rotational position along a second portion of the follower path.

    Abstract translation: 一种带有机翼和机翼的机翼，用于在机翼中产生拍打动作。 每个机翼结构包括机翼和通过弹性构件连接到随动机的翼梁。 每个翼载体可枢转地连接到主体，并且构造成限制横向运动并且允许翼梁围绕羽化轴旋转。 偏置构件为每个翼梁提供扭转偏置。 由致动器驱动的联动装置传递使翼载体绕扑动轴线旋转的循环运动，其使得从动件沿着从动路径移动。 附接到车身的导向器位于每个从动件的路径中，并且从动件和导向件被成形为使得每个翼梁具有围绕其轴线沿着从动路径的第一部分的第一旋转位置和沿着从动件路径的第一部分的第二旋转位置 从动路径的第二部分。

    MICROSTRUCTURES USING CARBON FIBER COMPOSITE HONEYCOMB BEAMS
    155.
    发明申请
    MICROSTRUCTURES USING CARBON FIBER COMPOSITE HONEYCOMB BEAMS 审中-公开
    使用碳纤维复合蜂窝骨架的微结构

    公开(公告)号：WO2004103889A3

    公开(公告)日：2005-05-26

    申请号：PCT/US2004012538

    申请日：2004-04-23

    Applicant: UNIV CALIFORNIA ,  WOOD ROBERT

    Inventor： WOOD ROBERT

    IPC: B64C33/00 ,  B64C33/02 ,  B64C39/02 ,  B81B20060101

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

    Abstract: A drive assembly for a wing of a micromechanical flying insect. The drive assembly comprises a honey comb structure. A method for flying a micromechanical flying insect comprising moving a wing with a drive assembly having a stiffness to weight ratio greater than about 16 x 10 N/mKg.

    Abstract translation: 用于微机械飞行昆虫机翼的驱动组件。 驱动组件包括蜂巢结构。 一种用于飞行微机械飞行昆虫的方法，包括使具有大于约16×10 10 N / mKg的刚度重量比的驱动组件移动机翼。

    MOTION ASSISTING APPARATUS
    157.
    发明申请
    MOTION ASSISTING APPARATUS 审中-公开
    运动辅助装置

    公开(公告)号：WO2003004122A1

    公开(公告)日：2003-01-16

    申请号：PCT/GB2002/002976

    申请日：2002-06-28

    Applicant: SINCLAIR, Peter

    IPC: A63H31/08

    CPC classification number: A63H31/08 ,  A63H27/008 ,  B64C33/02 ,  B64C39/028 ,  B64C2201/025 ,  B64C2201/042 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/148 ,  B64C2201/203

    Abstract: A drive assembly for use with a mechanical flying or walking device comprises an articulated member (7) having first and second portions (7a, 7b) arranged such that the portions move relative to each other, and a drive mechanism (9) for imparting motion to the articulated member. The drive mechanism (9) comprises: a drive member for imparting a cyclic motion on the articulated member; and a control member for controlling, in a predetermined manner, the relative position of the first and second portions during each cycle of the cyclic motion of the articulated member. In the case of a mechanical flying device, two such drive assemblies may be provided, the articulated member of each assembly forming a wing.

    Abstract translation: 一种与机械飞行或行走装置一起使用的驱动组件包括具有第一和第二部分（7a，7b）的铰接构件（7），所述第一和第二部分（7a，7b）布置成使得所述部分相对于彼此移动;以及驱动机构（9） 到铰接构件。 驱动机构（9）包括：用于在铰接构件上施加循环运动的驱动构件; 以及控制构件，用于以预定的方式控制在铰接构件的循环运动的每个循环期间第一和第二部分的相对位置。 在机械飞行装置的情况下，可以设置两个这样的驱动组件，每个组件的铰接构件形成翼。

    Ornithopter
    160.
    发明专利
    Ornithopter 有权
    扑翼机

    公开(公告)号：JP2014162264A

    公开(公告)日：2014-09-08

    申请号：JP2013032544

    申请日：2013-02-21

    Applicant: Mitsubishi Heavy Ind Ltd ,  三菱重工業株式会社

    Inventor： KURODA TOMOHITO ,  MORI TOMOYUKI ,  HATTORI KAZUNARI ,  TAHARA MASATO ,  TAKAYAMA OKI

    IPC: B64C33/02 ,  A63H27/18 ,  A63H27/28

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

    Abstract: PROBLEM TO BE SOLVED: To provide an ornithopter having excellent mimesis performance and capable of suppressing thrust loss and resistance increase.SOLUTION: The ornithopter comprises: a main wing attached to a shell 2; and a control system for controlling flap operation of the main wing. The main wing has an inner girder 21, an outer girder 22, and a wrist 30 interposed between the inner and outer girders and configured so that a folding angle which is a relative angle between the inner and outer girders can be varied within a predetermined variation range. The control system has an actuator 120 for performing launch operation and low hit operation of the inner girder by making the inner girder move in a vertical direction, an angle sensor 140 for measuring the folding angle, and a control device 110 for operating the inner girder by controlling the actuator according to the folding angle.

    Abstract translation: 要解决的问题：提供具有优异的缪斯性能并且能够抑制推力损失和阻力增加的鸟巢车。解决方案：炊具包括：附接到壳体2的主翼; 以及用于控制主翼的皮瓣操作的控制系统。 主翼具有内梁21，外梁22和插入在内梁和外梁之间的手腕30，并且构造成使得内外梁之间的相对角度的折角可以在预定变化范围内变化 范围。 控制系统具有致动器120，用于通过使内梁沿垂直方向移动来执行内梁的发射操作和低命中操作，用于测量折叠角度的角度传感器140以及用于操作内梁的控制装置110 通过根据折叠角度控制致动器。

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