公开(公告)号：US07963478B2

公开(公告)日：2011-06-21

申请号：US11997029

申请日：2006-02-08

申请人： Kwang Ho Kim ,  Jae Hak Jeon ,  Yoon Joo Kim

发明人： Kwang Ho Kim ,  Jae Hak Jeon ,  Yoon Joo Kim

IPC分类号： B64C33/00

CPC分类号： B64C33/02

摘要： The present invention provides a wing-flapping flying apparatus, which can fly by moving its wings similar to a bird hovering or flying in the air by flapping its wings. The wing-flapping flying apparatus comprises: a body; a rotating shaft rotatably joined to the body; driving means for rotating the rotating shaft; and wings reciprocated between two points and connected to the rotating shaft so as to be rotated together with the rotating shaft and to be relatively torsionally rotated with respect to the rotating shaft. The wing-flapping flying apparatus generates lift throughout an entire wing-flapping movement without generating lift only throughout the half of a wing-flapping movement or offsetting the generated lift by the other half of the wing-flapping movement. Therefore, the wing-flapping flying apparatus can provide not only a stable flight but also a softly hovering or ascending and descending flight.

摘要翻译： 本发明提供了一种飞翼飞行装置，其可以通过使翅膀类似于通过扑翼而悬挂在空中的鸟类飞行。 飞翼飞行装置包括：主体; 可旋转地连接到主体的旋转轴; 用于旋转所述旋转轴的驱动装置; 并且翼在两点之间往复运动并连接到旋转轴，以便与旋转轴一起旋转并且相对于旋转轴相对地扭转。 飞翼飞行装置在整个飞翼拍动运动中产生升力，而不会在飞翼运动的整个半部中产生升力，或者将所产生的升力抵消翼翼运动的另一半。 因此，飞翼飞行装置不仅可以提供稳定的飞行，还可以提供轻柔的悬停或上升和下降的飞行。

公开(公告)号：US20110079677A1

公开(公告)日：2011-04-07

申请号：US12924592

申请日：2010-09-30

申请人： Nathan J. Chronister

发明人： Nathan J. Chronister

IPC分类号： B64C33/00

CPC分类号： B64C39/028 ,  A63H27/008 ,  B64C2201/025

摘要： 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.

摘要翻译： 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。

公开(公告)号：US20100288871A1

公开(公告)日：2010-11-18

申请号：US12812456

申请日：2008-01-11

申请人： Hee Chul Hwang ,  II Hyun Paik ,  Jae Yeon Kim

发明人： Hee Chul Hwang ,  II Hyun Paik ,  Jae Yeon Kim

IPC分类号： B64C33/00

CPC分类号： A63H27/008 ,  A63H30/04

摘要： The present invention provides a remote-controlled ornithopter capable of flying forward in the upright position, which includes X-shaped main wings? having opposite phases to offset moments applied to a fuselage of the ornithopter. The ornithopter includes the fuselage (100), the X-shaped main wings (200), which are provided on the front end of the fuselage, tail wings (300), which are provided on the medial portion or the rear end of the fuselage, and a tail rotor (400), which controls a direction in which the fuselage flies. The ornithopter further includes a drive unit (500), which operates the main wings, and a flight control unit (600), which has a receiver to receive a signal for controlling the drive unit and the tail rotor. The ornithopter further includes a remote controller (700), which transmits the signal for controlling the drive unit and the tail rotor to the receiver.

摘要翻译： 本发明提供一种能够在直立位置向前飞行的远程控制的鸟巢器，其包括X形主翼？ 具有相反的相位，以抵消施加到鸟笼的机身的时刻。 机动车包括机身（100），设置在机身前端的X形主翼（200），尾翼（300），其设置在机身的内侧部分或后端 以及控制机身飞行方向的尾部转子（400）。 鸟巢器还包括操作主翼的驱动单元（500）和飞行控制单元（600），其具有用于接收用于控制驱动单元和尾部转子的信号的接收器。 鸟巢器还包括遥控器（700），其将用于控制驱动单元和尾部转子的信号发送到接收器。

公开(公告)号：US20070295858A1

公开(公告)日：2007-12-27

申请号：US11474886

申请日：2006-06-26

申请人： Thomas B. Higham

发明人： Thomas B. Higham

IPC分类号： B64C33/00

CPC分类号： A63H27/008

摘要： An new ornithopter is provided with an elongated body, wings extending laterally from the forward end of the elongated body, and a tail extending laterally from the rear end of the elongated body. In one embodiment, an elongated rotatable member is rotatably coupled at one end to the forward end of the body, and a mass is connected to the other end of the elongated rotatable member. The elongated rotatable member and the mass are rotated to drive the ornithopter. In another embodiment, a mass is coupled to the forward end of the elongated body, and the mass is moved laterally from one side of the elongated body to the other side of the elongated body to drive the ornithopter. The mass may be imparted with rotational and/or translational movement.

摘要翻译： 新的鸟巢器具有细长的主体，从细长主体的前端横向延伸的翼和从细长体的后端横向延伸的尾部。 在一个实施例中，细长的可旋转构件在一端可旋转地联接到主体的前端，并且质量体连接到细长的可旋转构件的另一端。 细长的可旋转构件和质量块被旋转以驱动鸟巢车。 在另一个实施例中，质量块联接到细长体的前端，并且质量体从细长体的一侧横向移动到细长体的另一侧以驱动鸟巢式搅拌器。 质量可以被赋予旋转和/或平移运动。

公开(公告)号：US20070210207A1

公开(公告)日：2007-09-13

申请号：US11748635

申请日：2007-05-15

申请人： Wei-Hsiang LIAO

发明人： Wei-Hsiang LIAO

IPC分类号： B64C33/00

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

摘要： 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.

摘要翻译： 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。

公开(公告)号：US07255305B2

公开(公告)日：2007-08-14

申请号：US10979046

申请日：2004-11-02

申请人： Milan Dennis Earl ,  Rebecca A. Earl

发明人： Milan Dennis Earl ,  Rebecca A. Earl

IPC分类号： B64C33/00

CPC分类号： B64C33/02

摘要： An efficient flying device having flapping wings, an ornithopter, which uses many of the principles seen in bird flight, is presented herein. The wings are highly flexible, translationally stable and oscillate as a natural pendulum. Described as a springboard, the wings have a singular natural frequency, and a pumping means drives the wings at that frequency. Feedback means are described by which to accomplish this, whereby deflection of the wing affects an escapement mechanism which controls the timing and direction of the pumping means. Wing design is described whereby camber, flexure, torsion and directionality of wing components affect efficient propulsion, lift and differential reactivity with air during downstrokes and upstrokes. A crook element in the wing spar at a location proximal to the body of the device redirects vertical oscillation to horizontal. Other features are addressed, such as rearward vortex production and reaction, a double aerofoil wing construction, lateral and vertical wing curvature, rearward wing and featherlike element flexure to produce thrust, and connection of separate elastic elements to reduce power requirements.

摘要翻译： 本文介绍了一种具有扑翼的高效飞行装置，其使用鸟类飞行中观察到的许多原理的鸟巢飞机。 翅膀是高度灵活的，平移稳定的，并作为自然摆动摆动。 被描述为跳板，机翼具有奇异的固有频率，并且泵送装置以该频率驱动机翼。 描述了用于实现这一点的反馈装置，由此机翼的偏转影响控制泵送装置的定时和方向的擒纵机构。 描述了机翼设计，因此翼部件的弯度，弯曲，扭转和方向性在下冲和上冲时影响有效的推进，升力和与空气的反应性。 在靠近设备主体的位置的翼梁中的弯曲元件将垂直振荡重定向到水平。 其他特征被解决，例如向后涡流产生和反应，双机翼结构，侧向和垂直翼部曲率，后翼和羽状元件弯曲以产生推力，以及连接单独的弹性元件以减少功率要求。

公开(公告)号：US20050269447A1

公开(公告)日：2005-12-08

申请号：US11147044

申请日：2005-06-07

申请人： Nathan Chronister

发明人： Nathan Chronister

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

CPC分类号： B64C39/028 ,  B64C33/02 ,  B64C2201/025 ,  B64C2201/042 ,  B64C2201/141 ,  B64C2201/146

摘要： 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.

摘要翻译： 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。

公开(公告)号：US5163861A

公开(公告)日：1992-11-17

申请号：US688533

申请日：1991-06-12

申请人： Gerard Van Ruymbeke

发明人： Gerard Van Ruymbeke

IPC分类号： A63H27/28 ,  A63H13/02 ,  A63H27/00 ,  A63H29/18 ,  A63H29/24 ,  A63H31/00 ,  A63H31/08 ,  B64C33/00 ,  F16H35/00

CPC分类号： A63H27/008

摘要： Process and apparatus providing the automatic locking of the wings of a wing-operated flying toy, wherein a locking device associated with the operating mechanism is applied, under the effect of elastic pressure, against a notch or slot of the circular disk of the draw crank of the operating mechanism, so that when an elastic band attains its normal power under the effect of torsional moment, the locking device is unable to engage or hold its position in the notch or slot; whereas when the power has almost attained its lowest value at the moment when the elastic band is almost completely untwisted, the locking device is able to engage and maintain itself in the slit causing the wing operating mechanism to lock and prevent movement of the wings.

摘要翻译： PCT No.PCT / FR89 / 00663 Sec。 371日期1991年6月12日 102（e）1991年6月12日PCT 1989年12月19日PCT PCT。 出版物WO90 / 06794 日期：1990年6月28日。提供机翼操作的飞行玩具的机翼的自动锁定的过程和装置，其中与弹性压力相关联的锁定装置在弹性压力的作用下施加于 操作机构的牵引曲柄的圆盘，使得当弹性带在扭转力矩的作用下达到其正常功率时，锁定装置不能接合或保持其在凹口或槽中的位置; 而当弹性带几乎完全解开时，功率几乎达到最低值时，锁定装置能够使其自身接合并保持在狭缝中，从而使机翼操作机构锁定并防止机翼的移动。

公开(公告)号：US3508840A

公开(公告)日：1970-04-28

申请号：US3508840D

申请日：1968-04-09

申请人： GUY LEDERLIN

发明人： LEDERLIN GUY

IPC分类号： B63H1/36 ,  B64C33/00 ,  F03D5/00 ,  F04D33/00 ,  B64C33/02

CPC分类号： B63H1/36 ,  B64C33/00 ,  F03D5/005 ,  F04D33/00 ,  Y02E10/70

公开(公告)号：US3161376A

公开(公告)日：1964-12-15

申请号：US25278063

申请日：1963-01-21

申请人： LYLE HAROLD M

发明人： LYLE HAROLD M

IPC分类号： B64C33/00

CPC分类号： B64C33/00