专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

81. 发明公开

EP2351607A2 Flying toy 有权
标题翻译： Fliegendes Spielzeug
公开(公告)号：EP2351607A2
公开(公告)日：2011-08-03
申请号：EP10193761.3
申请日：2010-12-06
申请人： Silverlit Limited
发明人： Van de Rostyne, Alexander , Wong, Kwok
IPC分类号： A63H27/133 , A63H27/26 , A63H30/04
CPC分类号： B64C27/43 , A63H27/06 , A63H27/12 , A63H30/04 , B64C27/82
摘要： A flying toy comprises a first wing and a second wing attached to and extending from opposite sides of a fuselage. There is a first propulsion unit, having a first motor and a first propeller system rotated by the first motor, mounted with the first wing; and a second propulsion unit, having a second motor and a second propeller system rotated by the second motor, mounted with the second wing. Each propulsion system has main blades and auxiliary blades which interact with each other. Each of two wings can be angled relative to horizontal independently. The toy can operate as a plane or helicopter.
摘要翻译：飞行玩具包括附接到机身的相对侧并从机身的相对侧延伸的第一翼和第二翼。第一推进单元具有安装有第一翼的第一马达和由第一马达旋转的第一螺旋桨系统; 以及第二推进单元，其具有安装有第二翼的由第二马达旋转的第二马达和第二螺旋桨系统。每个推进系统具有彼此相互作用的主叶片和辅助叶片。两个翼中的每一个可以相对于水平独立地成角度。玩具可以作为飞机或直升机操作。

82. 发明公开

EP2298644A1 Helicopter 有权
标题翻译：直升机
公开(公告)号：EP2298644A1
公开(公告)日：2011-03-23
申请号：EP09170725.7
申请日：2009-09-18
申请人： Silverlit Toys Manufactory Ltd.
发明人： van de Rostyne, Alexander Jozef Magdalena , Wai, Chi Pok Billy
IPC分类号： B64C27/605 , A63H27/133
CPC分类号： A63H27/12 , B64C27/605
摘要： A helicopter (1) includes a system to effect motion in a horizontal dimension thereby to direct the desired direction. The rotor blades are driven by a rotor shaft (9) and are hinge mounted on this rotor shaft, such that the angle between the plane of rotation of the main rotor and the rotor shaft (9) may vary. A control for moving the angle of incidence of at least one blade of the rotor (5) cyclically along at least part of a 360-degree rotation path around the rotor shaft is provided. This causes a variation in a lift force of the blade along at least part of the rotations path. This causes the body (2) to be urged in a relatively horizontal direction from a relative position of rest. The control includes an actuator for engaging with an assembly depending from the rotor, the inter-engagement of the actuator and assembly effecting a change in the angle of incidence of at least the one blade of the rotor (5). The system includes a rotor, preferably complemented with a stabilizer rotor (6). There is a control ring attached to the main rotor (5), and an actuator device connected with the helicopter body structure (2). The control ring is generally centered around the vertical rotor axis, and moves with the rotor when tilted around the feather axis.
摘要翻译：直升机（1）包括在水平尺寸上进行运动的系统，从而引导所需的方向。转子叶片由转子轴（9）驱动并且铰接安装在该转子轴上，使得主转子和转子轴（9）的旋转平面之间的角度可以变化。提供了一种用于沿转子轴周围的360度旋转路径的至少一部分循环移动转子（5）的至少一个叶片的入射角的控制器。这导致叶片沿着旋转路径的至少一部分的升力的变化。这使得主体（2）从相对于静止位置的相对水平的方向被推动。控制器包括用于与从转子悬垂的组件接合的致动器，致动器和组件的相互接合实现至少转子（5）的一个叶片的入射角的变化。该系统包括优选地与稳定器转子（6）相配合的转子。连接到主转子（5）上的控制环和与直升机主体结构（2）连接的致动器装置。控制环通常围绕垂直转子轴线居中，并且当绕着轴线倾斜时与转子一起移动。

83. 发明公开

EP2285460A1 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：EP2285460A1
公开(公告)日：2011-02-23
申请号：EP09730710.2
申请日：2009-03-30
申请人： Davis, Steven
发明人： Davis, Steven
IPC分类号： A63H27/127 , B64C27/20 , B64C39/06 , B64C29/00 , B64C27/32 , B64C11/00
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
摘要： A flying vehicle in accordance to an embodiment of the present invention includes a propeller control mechanism for flying the vehicle. The propeller control mechanism includes a propeller having a center shaft for connecting to the drive shaft; first and second propeller blades extending from the center shaft; and a control mechanism including a first linkage connecting the center shaft to the first propeller blade and a second linkage connecting the center shaft to a region defined on the propeller, wherein a change in a driving torque of the drive shaft causes the first linkage and the second linkage to change the pitch and height of the propeller blades while substantially unchanging the tip path plane of the propeller blades.

84. 发明公开

EP2254793A2 MODULES AND METHODS FOR BIASING POWER TO A MULTI-ENGINE POWER PLANT SUITABLE FOR ONE ENGINE INOPERATIVE FLIGHT PROCEDURE TRAINING 失效
标题翻译：模块和方法平衡，以多个引擎HAVING热电厂AN OEI程序的培训适合...功率
公开(公告)号：EP2254793A2
公开(公告)日：2010-12-01
申请号：EP08872452.1
申请日：2008-11-23
申请人： Sikorsky Aircraft Corporation
发明人： RUCCI, John , STOBIECKI, Anthony, Z. , DAVIS, Brent , MYERS, Christopher, James
IPC分类号： B64C27/12 , B64D35/08 , B64D43/00 , B64D45/00
CPC分类号： G09B9/46 , A63H27/12 , B62D1/02 , B62D1/22 , B64C27/04 , G09B9/08 , G09B9/16 , G09B9/165 , G09B9/18 , G09B9/203 , G09B9/206 , G09B9/44
摘要： A system and method for conducting flight procedures training in a rotary-wing aircraft with a multi-engine powerplant includes determining a variable bias relative an available power margin to simulate a reduced power available flight condition; and displaying symbology indicative of the simulated reduced power available flight condition.

85. 发明公开

EP2254674A1 ACROBATIC ROTARY-WING TOY HELICOPTER 审中-公开
标题翻译：杂技SWING玩具直升机
公开(公告)号：EP2254674A1
公开(公告)日：2010-12-01
申请号：EP09715688.9
申请日：2009-02-23
申请人： Spin Master Ltd.
发明人： ELSON, James, E. , SINK, Charles
IPC分类号： A63H27/133 , A63H27/24 , B64C27/10 , B64C27/26
CPC分类号： A63H27/12
摘要： There is provided a rotary-wing toy helicopter generally comprising a transverse shaft, a plane body fixedly attached to the transverse shaft and a rotor assembly rotatably attached to the transverse shaft. The rotor assembly generally comprises a primary drive means connected to a drive shaft for driving at least one set of lifting blades and a secondary drive means connected to the transverse shaft for driving rotation of the transverse shaft and the plane body clockwise or counterclockwise around the axis of transverse shaft.

86. 发明公开

EP2242552A2 PROCÉDÉ DE PILOTAGE D'UN DRONE À VOILURE TOURNANTE AVEC STABILISATION AUTOMATIQUE EN VOL STATIONNAIRE 有权
标题翻译：程序，以保持一个摆无人机自动飞行镇定无人过问状态
公开(公告)号：EP2242552A2
公开(公告)日：2010-10-27
申请号：EP09718030.1
申请日：2009-01-21
申请人： Parrot
发明人： SEYDOUX, Henri , LEFEBURE, Martin , CALLOU, François , JONCHERY, Claire , LANFREY, Jean-Baptiste
IPC分类号： A63H27/133 , A63H30/04
CPC分类号： A63H27/12 , A63H30/04 , G05D1/0858
摘要： The method of the invention can particularly be used for piloting radio-controlled toys and comprises the following operations: fitting the drone with a telemeter and a video camera; acquiring the altitude of the drone relative to the ground using the telemeter; acquiring the horizontal speed of the drone; and automatically stabilising the drone in a hovering flight by controlling the vertical thrust force of the drone in order to stabilise the altitude acquired by the telemeter and by controlling the horizontal thrust force of the drone so as to cancel the horizontal speed. The video camera is a front sight camera directed towards the front of the drone, and the horizontal speed of the drone is acquired from a plurality of video images taken by said front sight camera.

87. 发明公开

EP2233393A2 Verriegelungssystem 有权
公开(公告)号：EP2233393A2
公开(公告)日：2010-09-29
申请号：EP10157279.0
申请日：2010-03-23
申请人： Schnoell, Gregor
发明人： Schnoell, Gregor
IPC分类号： B64C1/30 , B64C27/08 , B64C39/02
CPC分类号： B64C1/30 , A63H27/12 , B64C27/08 , B64C39/024 , B64C2201/027 , B64C2201/102 , B64C2201/108
摘要： Die Erfindung betrifft ein Verriegelungssystem, insbesondere für Komponenten eines Hubschraubers, das Folgendes aufweist: ein Zentralteil (10) mit mehreren Anschlagselementen (11); zwei oder mehr Ausleger (20), die an dem Zentralteil angelenkt oder mit diesem lösbar verbunden sind; ein in den Zentralteil zumindest teilweise einführbares und von diesem lösbares Verschlussteil (30), wobei Zentralteil und Verschlussteil derart geformt sind, dass bei einer Dreh- und/oder Verschiebebewegung die beiden Teile und die Ausleger mechanisch derart ineinander greifen, dass der Ausleger zwischen dem Anschlagelement des Zentralteils und dem Verschlussteil arretiert werden kann.
摘要翻译：该系统具有带有一组捕获元件（11）的中心部分（10）和一组与中心部分铰接或可拆卸地连接的托架（20）。封闭部分（30）可部分插入中心部分。中心部分和封闭部分形成为使得中心部分，封闭部分和支架在中心部分和封闭部分的旋转或滑动运动期间彼此机械接合，使得支架锁定在捕获元件和封闭部分。

88. 发明公开

EP2189201A1 Helicopter with main and auxiliary rotors 审中-公开
标题翻译： Helikopter mit Haupt- und Hilfsrotoren
公开(公告)号：EP2189201A1
公开(公告)日：2010-05-26
申请号：EP09176464.7
申请日：2009-11-19
申请人： Silverlit Toys Manufactory Ltd
发明人： Van De Rostyne, Alexander Jozef Magdalena , Wai, Chi Pok Billy
IPC分类号： A63H27/133 , B64C27/605 , B64C27/625
CPC分类号： A63H27/12 , B64C27/605 , B64C27/625
摘要： A remote control toy helicopter (1) has a main rotor (4) and an auxiliary rotor (5) both driven by a rotor shaft. The auxiliary rotor has elongated elements (28) at an acute angle relative to blades (12a,12b) of the main rotor. A control system is provided that includes an actuator for engaging with a control assembly depending from the auxiliary rotor (5). The inter-engagement of the actuator and the control assembly effects change in the angle of incidence of the elongated elements (28) of the auxiliary rotor (5). 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（1）具有由转子轴驱动的主转子（4）和辅助转子（5）。辅助转子具有相对于主转子的叶片（12a，12b）成锐角的细长元件（28）。提供一种控制系统，其包括用于与从辅助转子（5）悬垂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（5）的细长元件（28）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。

89. 发明授权

EP1893314B1 HELICOPTER 有权
公开(公告)号：EP1893314B1
公开(公告)日：2009-11-18
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

90. 发明公开

EP1961472A1 Control apparatus of wireless remote-control model and operating parameter setup system thereof 审中-公开
标题翻译：用于无线电控制模型和系统控制装置来设置操作参数
公开(公告)号：EP1961472A1
公开(公告)日：2008-08-27
申请号：EP08002290.8
申请日：2008-02-07
申请人： Thunder Tiger Corporation
发明人： Shigetada, Taya
IPC分类号： A63H30/04 , A63H27/133
CPC分类号： A63H30/04 , A63H27/12
摘要： A control apparatus for a wireless remote-control model (100) and its operating parameter setup system is set up and changed by a personal computer (200), and various settings of setup information are transmitted to a wireless remote-control helicopter (100) through a communication line (12), and control parameters are stored in a set value storage module (4A) of a memory (4), such that control parameters for the movement characteristics of the wireless remote-control model (100) can be set up or changed easily to reduce the burden on the side of a signal transmitter.
摘要翻译：用于无线远程控制模型（100）和它的操作参数设置系统的控制装置被设置和由个人计算机（200）来改变，以及设置信息的各种设置为反式mitted到无线遥控的直升机（100）通过通信线路（12），以及控制参数被存储的存储器的设置值存储模块（4A）（4）中，检查没有为无线远程控制模型（100）的移动特性的控制参数可被设置向上或容易地改变，以减少对一个信号发射器一侧的负担。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式