公开(公告)号：US09150069B2

公开(公告)日：2015-10-06

申请号：US14454973

申请日：2014-08-08

申请人： Arash Kalantari ,  Matthew Spenko

发明人： Arash Kalantari ,  Matthew Spenko

IPC分类号： B60F5/02 ,  B64C25/36 ,  A63H27/133 ,  B64C37/00 ,  B64C39/02 ,  A63H27/00 ,  A63H33/00

CPC分类号： B60F5/02 ,  A63H27/12 ,  A63H33/005 ,  B64C25/36 ,  B64C37/00 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/127

摘要： A vehicle capable of both aerial and terrestrial locomotion. The terrestrial and aerial vehicle includes a flying device and a rolling cage connected to the flying device by at least one revolute joint. The rolling cage at least partially surrounds the flying device and is free-rolling and not separately powered.

摘要翻译： 一种能够进行空中和陆地运动的车辆。 陆地和空中飞行器包括通过至少一个旋转接头连接到飞行装置的飞行装置和滚动笼。 滚动笼至少部分地围绕飞行装置，并且是自由滚动的，而不是分开供电。

公开(公告)号：US20120122367A1

公开(公告)日：2012-05-17

申请号：US12947815

申请日：2010-11-16

申请人： Michael Sivan

发明人： Michael Sivan

IPC分类号： A63H27/133 ,  A63H30/04

CPC分类号： A63H27/12 ,  A63H30/04 ,  G05D1/0016 ,  G05D1/0033

摘要： Remote control of a toy helicopter by projecting a modulated Infra-Red light spot on a wall. The spot is beamed from a hand-held remote control unit and aimed by the user in different directions. The helicopter follows that spot by a controlled ascend or descend if the light spot is above or below the helicopter respectively, as well as turns right or left in the direction of the light spot.

摘要翻译： 通过将调制的红外光点投射在墙上来遥控玩具直升机。 该点由手持式遥控器发射，用户在不同方向上瞄准。 如果光点分别在直升机上方或下方，直升机也可以通过控制的上升或下降跟随该点，以及沿着光点的方向向右或向左转。

公开(公告)号：US20110159776A1

公开(公告)日：2011-06-30

申请号：US12944122

申请日：2010-11-11

申请人： Paul Mak

发明人： Paul Mak

IPC分类号： A63H27/133

CPC分类号： G05D1/0858

摘要： There is provided a method and apparatus for controlling a toy helicopter in flight. The toy helicopter is powered by a first rotor and a second rotor. A target speed ratio is determined for the speed of the first rotor and the speed of the second rotor. The speed of the rotors is adjusted incrementally until the target ratio is achieved

公开(公告)号：US07946526B2

公开(公告)日：2011-05-24

申请号：US11263903

申请日：2005-11-02

申请人： Nachman Zimet

发明人： Nachman Zimet

IPC分类号： B64C27/82 ,  B64C27/10 ,  A63H27/133

CPC分类号： B64C27/10 ,  A63H27/12

摘要： 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 said 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 in doors and out doors, while performing exciting maneuvers even by untrained kids.

摘要翻译： 一种航空稳定的旋翼式装置，易于飞行，具有多维度，小尺寸，飞行安全，生产成本低。 旋转翼装置包括具有固有的航空稳定性的提升力的同轴的反转转子驱动器; 辅助螺旋桨，其面向飞行方向并且位于所述同轴旋转翼装置的相对侧，并且能够向前，向后飞行并执行偏航。 旋转翼同轴直升机玩具远程控制和安全地飞行在门和门外，同时执行令人兴奋的动作，甚至未经训练的孩子。

公开(公告)号：US20100130093A1

公开(公告)日：2010-05-27

申请号：US12323209

申请日：2008-11-25

申请人： Alexander Jozef Magdalena Van de Rostyne ,  Chi Pok Billy WAI

发明人： Alexander Jozef Magdalena Van de Rostyne ,  Chi Pok Billy WAI

IPC分类号： A63H27/133

CPC分类号： A63H27/12 ,  B64C27/605 ,  B64C27/625

摘要： A remote control toy helicopter has a main rotor and an auxiliary rotor both driven by a rotor shaft. The auxiliary rotor has elongated elements at an acute angle relative to blades of the main rotor. A control system is provided that includes an actuator for engaging with a control assembly depending from the auxiliary rotor. The inter-engagement of the actuator and the control assembly effects change in the angle of incidence of the elongated elements of the auxiliary rotor. The interaction occurs when the assembly engages with the actuator by a depending arm associated with the assembly.

摘要翻译： 遥控玩具直升机具有由转子轴驱动的主转子和辅助转子。 辅助转子相对于主转子的叶片具有锐角的细长元件。 提供了一种控制系统，其包括用于与从辅助转子悬挂的控制组件接合的致动器。 致动器和控制组件的相互接合效应改变了辅助转子的细长元件的入射角。 当组件通过与组件相关联的悬垂臂与致动器接合时，发生相互作用。

公开(公告)号：US20100025525A1

公开(公告)日：2010-02-04

申请号：US12185277

申请日：2008-08-04

申请人： Alexander Jozef Magdalena Van de Rostyne ,  Kwok Leung Wong

发明人： Alexander Jozef Magdalena Van de Rostyne ,  Kwok Leung Wong

IPC分类号： A63H27/133

CPC分类号： A63H27/12

摘要： A toy helicopter, in accordance with the present disclosure, includes a body having a longitudinal length and a main rotor. There is an element movable along the longitudinal length. The element allows a user to selectively adjust the location of the center of gravity of a toy helicopter by moving the element along the longitudinal length, thereby changing the velocity of the helicopter.

摘要翻译： 根据本公开的玩具直升机包括具有纵向长度的主体和主转子。 有一个沿纵向长度移动的元件。 该元件允许用户通过沿着纵向长度移动元件来选择性地调整玩具直升机的重心位置，从而改变直升机的速度。

公开(公告)号：US07416466B2

公开(公告)日：2008-08-26

申请号：US11222352

申请日：2005-09-07

申请人： Kunikazu Isawa

发明人： Kunikazu Isawa

IPC分类号： A63H27/133

CPC分类号： A63H27/12

摘要： A flying toy is provided in which a flying object on a model having an optional character can be caused to freely ascend/descend or hover by remote control. The flying toy comprises: a flying object which replicates a model having a character; an upper rotor and a lower rotor which are provided on the top of the flying object and which concentrically rotate in directions opposite from each other; a stabilizer which rotates in conjunction with at least one of the rotors and which stabilizes a posture; a driver which is provided inside the flying object and which rotates the upper rotor, the lower rotor and the stabilizer; a control circuit for remote control to control an operation of the driver and a battery to serve as a power source which are provided inside the flying object.

摘要翻译： 提供了一种飞行玩具，其中具有可选字符的模型上的飞行物体可以通过遥控器自由地上升/下降或悬停。 飞行玩具包括：复制具有角色的模型的飞行对象; 上转子和下转子，其设置在飞行物体的顶部并且彼此相反的方向同心旋转; 稳定器，其与至少一个转子一起旋转并稳定姿势; 驱动器，其设置在飞行物体的内部并使上部转子，下部转子和稳定器旋转; 用于控制驾驶员的操作的遥控器的控制电路和设置在飞行物体内部的用作电源的电池。

公开(公告)号：US20080076320A1

公开(公告)日：2008-03-27

申请号：US11953826

申请日：2007-12-10

申请人： Alexander Jozef Van De Rostyne

发明人： Alexander Jozef Van De Rostyne

IPC分类号： A63H27/133

CPC分类号： A63H27/12

摘要： A helicopter has a main rotor with propeller blades which is driven by a rotor shaft and which is hinge-mounted to this rotor shaft. The angle between the surface of rotation of the main rotor and the rotor shaft may vary. A swinging manner on an oscillatory shaft is essentially transverse to the rotor shaft of the main rotor and is directed transversally to the longitudinal axis of the vanes. The main rotor and the auxiliary rotor are connected to each other by a mechanical link. The swinging motions of the auxiliary rotor controls the angle of incidence (A) of at least one of the propeller blades of the main rotor. There are wings from the body and a stabilizer at the tail.

摘要翻译： 直升机具有主转子，其具有由转子轴驱动的螺旋桨叶片，并且铰链安装在该转子轴上。 主转子和转子轴的旋转表面之间的角度可以变化。 振荡轴上的摆动方式基本上横向于主转子的转子轴，横向于叶片的纵向轴线。 主转子和辅助转子通过机械连接相互连接。 辅助转子的摆动运动控制主转子至少一个螺旋桨叶片的入射角（A）。 身上有翅膀和尾巴的稳定器。

公开(公告)号：US06960112B2

公开(公告)日：2005-11-01

申请号：US10778369

申请日：2004-02-13

申请人： David Vincent Helmlinger ,  Gregory Gilbert Garneau ,  Lee Chun Wah ,  Chung Zhi Jie

发明人： David Vincent Helmlinger ,  Gregory Gilbert Garneau ,  Lee Chun Wah ,  Chung Zhi Jie

IPC分类号： A63H20060101 ,  A63H27/00 ,  A63H27/127 ,  A63H27/133

CPC分类号： A63H27/12

摘要： An airfoil blade in a powered toy aircraft has a body with a cushioned edge. The body has a first end adjoining a hub, a second opposing end, a forward edge, and an opposing trailing edge. The cushioned leading edge is attached mechanically to the body and extends along the forward edge so as to form a cushioned leading edge of the blade or along the second end to form a cushioned blade tip or both. The body is formed from a first resiliently flexible polymer plastic material. The cushioned edge is formed from a second noticeably softer material such as an elastomer.

公开(公告)号：US5836545A

公开(公告)日：1998-11-17

申请号：US728929

申请日：1996-10-11

申请人： Paul E. Arlton ,  David J. Arlton ,  Paul Klusman

发明人： Paul E. Arlton ,  David J. Arlton ,  Paul Klusman

IPC分类号： A63H27/133 ,  B64C1/00 ,  B64C1/08 ,  B64C25/00 ,  B64C25/52 ,  B64C27/00 ,  B64C27/04 ,  B64C27/06 ,  B64C27/10 ,  B64C27/32 ,  B64C27/39 ,  B64C27/467 ,  B64C27/605 ,  B64C27/625 ,  B64C27/82 ,  B64D35/02

CPC分类号： A63H27/12

摘要： A model rotary wing aircraft is provided that includes a fuselage, a power plant, a main rotor, a tail rotor, and a drive apparatus. The power plant includes a passive cooling system to transfer heat produced by the power plant to the atmosphere. The passive cooling system consumes less than about five percent of the power produced by the power plant. The main rotor is driven by the power plant at a main rotor speed of rotation and the tail rotor is driven by the power plant at a tail rotor speed of rotation. The drive apparatus transfers power from the power plant to the main rotor and tail rotor to rotate the tail rotor at a tail rotor speed of rotation that is about three times greater than the main rotor speed of rotation to minimize the amount of power used by the tail rotor.

摘要翻译： 提供了一种型号旋翼飞机，其包括机身，发电厂，主转子，尾转子和驱动装置。 发电厂包括一个被动冷却系统，用于将发电厂产生的热量转移到大气中。 被动冷却系统消耗的电力不到发电厂产生的功率的5％左右。 主转子由发电厂以主转子旋转速度驱动，尾转子由发电厂以转子转子旋转速度驱动。 驱动装置将电力从发电厂传递到主转子和尾部转子，以使转子的转子旋转速度大于主转子旋转速度的三分之一，从而将尾部转子的转速最小化， 尾转子。