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131. 发明公开

EP2285460A4 DIRECTIONALLY CONTROLLABLE FLYING VEHICLE AND A PROPELLER MECHANISM FOR ACCOMPLISHING THE SAME 有权
标题翻译：方向控制平面和螺旋桨结构的驱动器
公开(公告)号：EP2285460A4
公开(公告)日：2012-06-06
申请号：EP09730710
申请日：2009-03-30
申请人： DAVIS STEVEN
发明人： DAVIS STEVEN
IPC分类号： A63H27/127 , A63H30/04 , A63H33/18 , B64C11/00 , B64C27/20 , B64C27/32 , B64C27/57 , B64C27/72 , B64C29/00 , B64C39/02 , B64C39/06
CPC分类号： B64C27/20 , A63H27/12 , A63H30/04 , A63H33/18 , B64C27/32 , B64C27/57 , B64C27/72 , B64C39/024 , B64C2201/027 , B64C2201/108 , Y02T50/34

132. 发明授权

EP2210653B1 SINGLE ROTOR MODEL HELICOPTER WITH IMPROVED STABILITY BEHAVIOR 有权
标题翻译：与转子和改进稳定性能模型直升机
公开(公告)号：EP2210653B1
公开(公告)日：2012-04-18
申请号：EP08757540.3
申请日：2008-05-29
申请人： Shanghai Nine Eagles Electronic Technology Co., Ltd
发明人： HUANG, Guochuan , WU, Yuchen , YU, Yizhen , DING, Huanzhong
IPC分类号： A63H27/133 , B64C27/625
CPC分类号： A63H27/12 , B64C27/43 , B64C27/625
摘要： A single rotor model helicopter is provided, comprising a spindle, a rotor head provided on the spindle, a pair of rotor blades mounting on the rotor head and a pair of hybrid control rocker arms. Said helicopter further includes an operating system and a stabilizing system. The pair of hybrid control rocker arms are set on the both sides of the rotor head respectively and rotatably connected with the pitch control rocker arm through the hole located on the center of the hybrid control rocker arm in order to control the attack angles of the rotor blades, wherein the pitch control rocker arms are also provided on the both sides of the rotor head. Each hybrid control rocker arm has two control points. The first pair of control points diagonally opposite provided on the pair of hybrid control rocker arms are controlled by the cyclic torque transmitted from the operating system, and the second pair of control points diagonally opposite provided are controlled by the stabilizing system. Furthermore, the second control points controlled by the stabilizing system and the first control points controlled by the swash plate can move about a fulcrum. Present invention can separately adjust the operating sensitivity and stability, thereby find the optimum combination of dynamic stability and maneuverability of the model helicopter.

133. 发明公开

EP2340880A1 Dual-rotor model helicopter control system 有权
标题翻译： Doppelrotor-Hubschraubersteuerungssystem
公开(公告)号：EP2340880A1
公开(公告)日：2011-07-06
申请号：EP10190960.4
申请日：2010-11-12
申请人： Luo, Zhihong
发明人： Luo, Zhihong
IPC分类号： A63H27/133
CPC分类号： A63H27/12
摘要： A coaxial dual-rotor model helicopter system includes a power control mechanism, a transmission mechanism, a control mechanism and a rotor mechanism. The rotor mechanism includes an upper rotor (12) and a lower rotor (22) coaxially installed on an upper side and a lower side of a main shaft (8) and controlled by an inner shaft (81) and an outer shaft (82) for rotating. The control mechanism includes a Bell self-balance mechanism (11) to control the upper rotor (12) and a Bell-Hiller control structure (21) to control the lower rotor (22) . The power control mechanism (3) controls the rotor mechanism through the transmission mechanism and the control mechanism. Thepresent invention achieves balance effect through the upper rotor (12) by employing the Bell self-balance mechanism (11) that has a great stability to provide automatic control. The lower rotor (22) aims to control direction and employs the Bell-Hiller control structure (21) that has a high maneuverability to perform active control.
摘要翻译：同轴双转子模型直升机系统包括功率控制机构，传动机构，控制机构和转子机构。转子机构包括同轴安装在主轴（8）的上侧和下侧并由内轴（81）和外轴（82）控制的上转子（12）和下转子（22）用于旋转。控制机构包括用于控制上转子（12）的贝尔自平衡机构（11）和用于控制下转子（22）的贝尔 - 希勒控制结构（21）。动力控制机构（3）通过传动机构和控制机构控制转子机构。本发明通过采用具有很大稳定性以提供自动控制的贝尔自平衡机构（11），通过上转子（12）实现平衡效果。下转子（22）旨在控制方向，并采用具有高机动性的贝尔 - 希勒控制结构（21）来执行主动控制。

134. 发明公开

EP2172396A4 ROTOR HEAD OF REMOTELY-CONTROLLED HELICOPTER, AND REMOTELY-CONTROLLED HELICOPTER 审中-公开
标题翻译：旋翼遥控直升机及直升机遥控器
公开(公告)号：EP2172396A4
公开(公告)日：2011-06-08
申请号：EP07768007
申请日：2007-07-02
申请人： HIROBO CO LTD
发明人： UEBORI TAKAKAZU , NAKAMURA KIMIO
IPC分类号： B64C27/605 , A63H27/133
CPC分类号： A63H27/12

135. 发明公开

EP2327462A1 Ferngesteuertes Spielzeug 审中-公开
公开(公告)号：EP2327462A1
公开(公告)日：2011-06-01
申请号：EP09177228.5
申请日：2009-11-26
申请人： Nikko Entertainment B.V.
发明人： Bakker, Jeroen
IPC分类号： A63H17/26 , A63H27/133 , B60F5/02 , B62D57/04
CPC分类号： A63H27/12 , A63H17/262
摘要： Es ist ein ferngesteuertes Spielzeug mit einem Fahrzeuggehäuse, mindestens einer Fortbewegungsvorrichtung und einer Fernsteuervorrichtung vorgesehen, wobei das Fahrzeuggehäuse eine Empfängereinheit zum Empfangen von durch die Fernsteuereinheit gesendeten Steuersignale aufweist, dadurch gekennzeichnet, dass das Spielzeug sowohl auf einer Ebene als auch in der Luft fortbewegbar ist, wobei es wenigstens einen Antriebsmotor zum Antreiben der mindestens eine Fortbewegungsvorrichtung 20; 22, 22' aufweist.
摘要翻译：该玩具具有车辆外壳（10），其包括用于接收由遥控单元发送的控制信号的接收器单元。玩具在平面和空中移动，驱动电机驱动移动装置（20）。运动装置包括三个滚轮（24）和/或滚轮和推进器（22,22'）。车轮和/或跑步者与车辆壳体连接，使得在螺旋桨的致动期间壳体从表面抬起，其中表面被提供用于运动。螺旋桨附接到旋转轴（28）。

136. 发明授权

EP1893314B8 HELICOPTER 有权
标题翻译：直升机
公开(公告)号：EP1893314B8
公开(公告)日：2009-12-30
申请号：EP06850428.1
申请日：2006-12-15
申请人： Silverlit Toys Manufactory Ltd
发明人： VON DE ROSTYNE, Alexander, Jozef Magdalena
IPC分类号： A63H27/133 , B64C27/43 , B64C27/82 , B64C27/625
CPC分类号： A63H27/12

137. 发明公开

EP2043914A1 CONTROL SYSTEM FOR A FLYING VEHICLE 有权转让
标题翻译：飞行器控制系统
公开(公告)号：EP2043914A1
公开(公告)日：2009-04-08
申请号：EP06719556.0
申请日：2006-01-12
申请人： Zaptoys International Ltd.
发明人： REHKEMPER, Jeffrey , GRISOLIA, Nicholas , GREENLEY, Peter , GOULD, Bret
IPC分类号： B64C27/00
CPC分类号： A63H30/00 , A63H27/12
摘要： In one embodiment of the present invention there is described a vehicle having a propeller mechanism for propelling the vehicle in a horizontal direction. The vehicle includes a transmitter positioned on the bottom of the vehicle for transmitting a signal from the vehicle downwardly away from the vehicle. A receiver is positioned on the bottom of the vehicle for receiving the signal as it is bounced off of a surface, defined as a bounced signal. A control system is also provided that automatically sets a speed of the propeller mechanism in response to the receiver. The control system sets the speed of the propeller mechanism to a first speed when the receiver receives the bounced signal and the control system sets the speed of the propeller mechanism to a second speed when the receiver does not receive the bounced signal. The first speed is predefined as a speed that causes the vehicle to gain altitude, while the second speed is predefined as a speed that causes the vehicle to lose altitude. When the vehicle reaches a predetermined distance away from the surface of the object, the vehicle will hover at the predetermined distance as the control system toggles between the first and second speeds.
摘要翻译：在本发明的一个实施例中，描述了一种具有用于沿水平方向推动车辆的螺旋桨机构的车辆。车辆包括位于车辆底部的发射器，用于从车辆向下发射信号以远离车辆。接收器位于车辆的底部，用于在信号从表面反弹离开表面时接收信号，该表面被定义为反弹信号。还提供了一种控制系统，其根据接收器自动设定螺旋桨机构的速度。当接收器接收到反弹信号时，控制系统将螺旋桨机构的速度设置为第一速度，并且当接收器没有接收到反弹信号时，控制系统将螺旋桨机构的速度设置为第二速度。第一速度被预定义为使车辆获得高度的速度，而第二速度被预定义为导致车辆失去高度的速度。当车辆到达距物体表面预定距离时，随着控制系统在第一和第二速度之间切换，车辆将悬停在预定距离处。

138. 发明公开

EP2032225A1 A FLYING TOY SUPPORTED BY A BIROTOR WHOSE BLADES ARE PARTIALLY FLEXIBLE 审中-公开
标题翻译：飞行玩具与部分柔性翼的双转子
公开(公告)号：EP2032225A1
公开(公告)日：2009-03-11
申请号：EP07764834.3
申请日：2007-06-20
申请人： ALESSANDRO QUERCETTI & C. Fabbrica Giocattoli Formativi - S.p.A.
发明人： QUECETTI, Alessandro
IPC分类号： A63H27/04
CPC分类号： A63H27/04 , A63H27/082 , A63H27/12
摘要： A flying toy suitable for being raised and then maintained in flight by the wind action, and controlled and maneuvered by means of an anchorage cable in a manner similar to that of a kite, that is provided with a birotor (1-6), and wherein the blades (1-4) of each rotor are partially flexible. The birotor is composed of two superimposed and coaxial rotors (1-6) and a synchronization mechanism (13) which obliges said rotors to effect symmetrical counter-rotations. Each blade (1-4) of each rotor comprises a substantially rigid proximal portion (1 ) whose cross section has the shape and the inclination incidence suggested by the laws of the aerodynamic, and comprises a distal portion (3) having a noticeable capability of undergoing flexional deformations. The flexible distal portion (3) may have a cross section identical or similar to the cross section of the rigid proximal portion (1 ), or a cross section simplified with respect to the rigid proximal portion (1). The flexible distal portion (3) may form an extension of the rigid proximal portion (1 ) or be pivoted to the rigid proximal portion (1 ) around an axis (4) at least approximately parallel to the rotor axis, whereby the distal portion (3) of the blade can orientate itself with respect to the proximal portion (1 ).

139. 发明授权

EP1888404B1 LANDING GEAR FOR A MICRO AIR VEHICLE 失效
标题翻译：用于微型空气动力车的起落架
公开(公告)号：EP1888404B1
公开(公告)日：2008-10-29
申请号：EP06784598.2
申请日：2006-06-06
申请人： Honeywell International Inc.
发明人： MANTYCH, Glen, A. , GOOSSEN, Emray, R.
IPC分类号： B64C39/00 , A63H27/133
CPC分类号： A63H27/02 , A63H27/12 , A63H27/14 , B64C39/028 , B64C2201/027 , B64C2201/108
摘要： Self-leveling legs (30, 32) are used to accommodate landing a ducted fan hovercraft (20) on a sloped surface (52) such as a roof-top. These legs (30, 32) move to accommodate a variation of slope within their range of motion irrespective to the azimuth of the vehicle body (38). The configuration and operation of the landing legs (30, 32) allow the hovercraft (20) to land in a stable fashion with the hovercraft (20) vehicle body (38) maintained in a vertical orientation. The basic kinematics of the present invention is the displacement of one landing leg (30) upwards is connected by a horizontal member (46) to the opposite leg and displaces it downwards (32), and visa-versa. Planar surface contact is accomplished by the unique curvature of the legs (30, 32) and the splay of the legs from the vehicle body (38).
摘要翻译：自流平支腿（30,32）用于容纳在涵盖诸如屋顶的倾斜表面（52）上的涵道风扇气垫船（20）。这些腿（30,32）移动以适应其运动范围内的斜率变化，而与车体（38）的方位无关。登陆腿（30,32）的配置和操作允许气垫船（20）以气垫船（20）车身（38）保持垂直定向的稳定方式着陆。本发明的基本运动学特征是一个着陆腿（30）向上的位移通过水平构件（46）连接到相对的腿并将其向下移动（32），反之亦然。平面表面接触通过腿部（30,32）的独特弯曲以及腿部从车身（38）的张开来实现。

140. 发明公开

EP1943001A1 ROTARY-WING VEHICLE SYSTEM 有权
标题翻译： SWING车辆系统
公开(公告)号：EP1943001A1
公开(公告)日：2008-07-16
申请号：EP06745084.1
申请日：2006-04-30
申请人： Zimet, Nachman , Divon, Avner
发明人： Zimet, Nachman , Divon, Avner
IPC分类号： A63H27/133 , B64C27/10
CPC分类号： B64C27/10 , A63H27/12
摘要： There is provided a rotary-wing apparatus that is aeronautically stable, easy to fly with a multidimensional control, small size, and safe to fly and low cost to produce. The rotary-wing apparatus includes a coaxial, counter rotating rotor drive providing lifting power with an inherent aeronautical stability; auxiliary propellers that face the direction of flight and are located on opposite sides of the coaxial rotary-wing apparatus and enable flying forwards, backwards and perform yawing. The rotary-wing coaxial helicopter toy is remotely controlled and safe to fly indoors and outdoors, while performing exciting maneuvers even by untrained kids .

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