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1. 发明授权

US11731060B2 Flying toys 有权
公开(公告)号：US11731060B2
公开(公告)日：2023-08-22
申请号：US17100105
申请日：2020-11-20
申请人： Rehco, LLC
发明人： Jeffrey Rehkemper , Adam Gelder
IPC分类号： A63H29/16 , A63H27/00 , B64D27/08 , B64C11/00 , B64C5/02 , B64C5/06 , B64D37/06 , F15B15/20 , A63H29/24 , B64D37/04 , A63H27/26
CPC分类号： A63H29/16 , A63H27/00 , A63H27/02 , A63H27/06 , A63H29/24 , B64C5/02 , B64C5/06 , B64C11/00 , B64D27/08 , B64D37/04 , B64D37/06 , F15B15/20 , B64C2203/00
摘要： In one embodiment there is provided a flying toy that can be manually pumped with air. The pressurized air is kept in a canister and use to drive a propeller to propeller the toy for flight.

2. 发明申请

US20180128923A1 METHOD FOR REALIZING OR IMPROVING OBSTACLE AVOIDANCE FUNCTIONALITY OF FLYING DEVICE AND FLYING DEVICE USING THE SAME 审中-公开
公开(公告)号：US20180128923A1
公开(公告)日：2018-05-10
申请号：US15681244
申请日：2017-08-18
申请人： HON HAI PRECISION INDUSTRY CO., LTD.
发明人： MAO-KUO HSU
IPC分类号： G01S17/93 , B64C39/02
CPC分类号： G01S17/93 , B64C39/024 , B64C2201/141 , B64C2201/146 , B64C2203/00 , G01S13/9303 , G01S15/93
摘要： This disclosure relates to a method for realizing obstacle avoidance functionality of a flying device. The method includes: providing a flying device without obstacle avoidance functionality, wherein the flying device includes a flying body and a remote controller; the flying body includes a wireless receiving module, a flying controlling module and an actuator; and second, installing a sensor and a micro controlling module; the wireless receiving module only send a first flying order that is from the remote controller, to the micro controlling module; the sensor only send an obstacle information to the micro controlling module; and the micro controlling module calculates the first flying order and the obstacle information to obtain a second flying order, and sends the second flying order to the flying controlling module; and the flying controlling module controls the flying body to fly according to the second flying order.

3. 发明授权

US09529358B2 Remote control system and method and usage related to such a system 有权
标题翻译：遥控系统及与此类系统相关的方法和用法
公开(公告)号：US09529358B2
公开(公告)日：2016-12-27
申请号：US14441016
申请日：2013-11-01
申请人： KVASER AB
发明人： Lars-Berno Fredriksson
IPC分类号： A63H30/04 , H04L12/40 , B64C39/00 , G05D1/00 , B64C39/02
CPC分类号： G05D1/0016 , A63H30/04 , B64C39/024 , B64C2201/146 , B64C2203/00
摘要： The invention relates to a remote control system (195) comprising mobile units (190, 1102, 1105), and a by control means (106, 110) provided controller unit for these. Said units are equipped with a function performing means (161) and transferring means (207, 270) that generates information signals (301) respectively transmits the same. Signal processing means (261, 268) and their exerting function (314) for controlling the functions of the respective mobile unit are placed respectively takes place only in the current mobile device. In accordance with the proposed use in connection with the present invention object, a controller area network type of system is constructed with a distributed and integrated network structure (1751). Only signal processing means (1753) and their function exertion means (1754) for controlling of a mobile unit, which is positioned in the actual unit, is used for its control. According to the method establishes a structure of a controller area network type with modular units (1753′), nodes (1753) and a communication protocol (501) for the node communication. All messages transmitted by the nodes are received by the modular units (1754, 1792). A information comparison (1755, 176) is used to select respective message or part thereof.
摘要翻译：本发明涉及包括移动单元（190,1102,1105）的远程控制系统（195），以及由这些控制装置（106,110）提供的控制单元。所述单元配备有产生信息信号（301）的功能执行装置（161）和传送装置（207,270），分别传送它们。信号处理装置（261,268）及其用于控制各个移动单元的功能的作用功能（314）分别仅在当前的移动装置中进行。根据本发明目的的提出的使用，系统的控制器区域网络类型由分布式和集成的网络结构构成（1751）。仅用于控制位于实际单元中的移动单元的信号处理装置（1753）及其功能消耗装置（1754）用于其控制。根据该方法建立了具有用于节点通信的模块单元（1753'），节点（1753）和通信协议（501）的控制器区域网络类型的结构。由节点发送的所有消息都由模块单元（1754,1792）接收。信息比较（1755,176）用于选择相应的消息或其一部分。

4. 发明申请

US20160228764A9 WIRELESS COMMUNICATION SYSTEM FOR GAME PLAY WITH MULTIPLE REMOTE CONTROL FLYING CRAFT 有权
公开(公告)号：US20160228764A9
公开(公告)日：2016-08-11
申请号：US14691412
申请日：2015-04-20
申请人： QFO Labs, Inc.
发明人： John Paul Condon , James Edward Fairman , Bradley Dean Pedersen
IPC分类号： A63F13/235 , A63F13/837 , A63F13/245
CPC分类号： A63F13/235 , A63F13/00 , A63F13/245 , A63F13/837 , A63H13/00 , A63H17/00 , A63H17/32 , A63H27/00 , A63H27/12 , A63H30/04 , A63H33/26 , A63H2200/00 , B64C2201/027 , B64C2201/042 , B64C2201/146 , B64C2203/00 , F21L4/027 , F21V23/0435 , F41G1/36 , G05D1/0033
摘要： A gaming system for enabling three-dimensional game play of remote-control craft controlled by a controller, each craft including a communication system with both radio frequency (RF) and infrared (IR) capabilities. The system can include a plurality of hovering remote-control flying craft each controlled by a handheld controller, and further may include at least one additional game accessory elements, such as a puck, a ground station or a gun. Each pairing of craft and controllers communicate via an RF protocol that transmits at least control communications between the controller and the craft based on pair identification information in an RF communication protocol. The craft and game-accessory elements also communicate via at least an IR protocol that communicates game-play information. Selectable pairs of craft and controllers may be assigned to different teams for playing multiplayer team games based on team identification information in the RF communication protocol.

5. 发明申请

US20160107751A1 CONTROLLED FLIGHT OF A MULTICOPTER EXPERIENCING A FAILURE AFFECTING AN EFFECTOR 有权
标题翻译：经营影响影响的故障的多功能人员的控制飞行
公开(公告)号：US20160107751A1
公开(公告)日：2016-04-21
申请号：US14893874
申请日：2014-06-05
申请人： ETH ZURICH
发明人： Raffaello D'ANDREA , Sergei LUPASHIN , Mark W. MUELLER , Markus WAIBEL
IPC分类号： B64C39/02 , B64D45/00 , B64C27/08
CPC分类号： B64C13/24 , B64C27/08 , B64C27/20 , B64C27/32 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2203/00 , B64D45/00 , G05D1/0072
摘要： According to a first aspect of the invention, there is provided a method for operating a multicopter experiencing a failure during flight, the multicopter comprising a body, and at least four effectors attached to the body, each operable to produce both a torque and a thrust force which can cause the multicopter to fly when not experiencing said failure. The method may comprise the step of identifying a failure wherein the failure affects the torque and/or thrust force produced by an effector, and in response to identifying a failure carrying out the following steps, (1) computing an estimate of the orientation of a primary axis of said body with respect to a predefined reference frame, wherein said primary axis is an axis about which said multicopter rotates when flying, (2) computing an estimate of the angular velocity of said multicopter, (3) controlling one or more of said at least four effectors based on said estimate of the orientation of the primary axis of said body with respect to said predefined reference frame and said estimate of the angular velocity of the multicopter. The step of controlling one or more of said at least four effectors may be performed such that (a) said one or more effectors collectively produce a torque along said primary axis and a torque perpendicular to said primary axis, wherein (i) the torque along said primary axis causes said multicopter to rotate about said primary axis, and (ii) the torque perpendicular to said primary axis causes said multicopter to move such that the orientation of said primary axis converges to a target orientation with respect to said predefined reference frame, and (b) such that said one or more effectors individually produce a thrust force along said primary axis.
摘要翻译：根据本发明的第一方面，提供了一种用于操作在飞行期间经历故障的多机器的方法，所述多机器包括主体，以及附接到所述主体的至少四个执行器，每个可操作以产生扭矩和推力在不经历所述故障时可能导致多机器飞行的力。该方法可以包括识别故障的步骤，其中故障影响由效应器产生的扭矩和/或推力，并且响应于识别执行以下步骤的故障，（1）计算一个所述主体相对于预定义的参考框架的主轴线，其中所述主轴线是所述多机器在飞行时旋转的轴线，（2）计算所述多机器的角速度的估计，（3）控制一个或多个基于所述身体的主轴的方向相对于所述预定参考框架的所述估计和所述多机器的角速度的估计，至少四个效应器。可以执行控制所述至少四个效应器中的一个或多个的步骤，使得（a）所述一个或多个效应器共同地沿着所述主轴产生扭矩和垂直于所述主轴的扭矩，其中（i）沿着所述主轴使所述多机器人围绕所述主轴线旋转，并且（ii）垂直于所述主轴线的转矩使得所述多机器人移动，使得所述主轴线的方向相对于所述预定参考系收敛到目标方位，和（b）使得所述一个或多个效应器单独地沿着所述主轴产生推力。

6. 发明申请

US20160016652A1 AERIAL VEHICLES AND METHODS OF USE 有权
标题翻译：航空器及其使用方法
公开(公告)号：US20160016652A1
公开(公告)日：2016-01-21
申请号：US14734864
申请日：2015-06-09
申请人： Ronald M. Barrett , Robert B. Honea , Richard B. Bramlette
发明人： Ronald M. Barrett , Robert B. Honea , Richard B. Bramlette
IPC分类号： B64C3/00 , A63H27/00 , B64C15/02 , B64C11/00 , B64C25/06 , B64C9/00
CPC分类号： A63H27/12 , A63H27/02 , A63H33/003 , B64C25/06 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/104 , B64C2201/108 , B64C2201/128 , B64C2203/00 , B64D27/02
摘要： An aerial vehicle capable of convertible flight from hover to linear flight includes a body having a longitudinal body axis, a plurality of forward wings, a plurality of aft wings, at least one motor, and at least three aerodynamic propulsors driven by the at least one motor. Each forward wing extends a forward wing plane. Each aft wing extends from an aft wing plane. The aerodynamic propulsors are mounted longitudinally between the plurality of forward wings and plurality of aft wings.
摘要翻译：能够从悬停到线性飞行的可转换飞行的飞行器包括具有纵向轴线的主体，多个前翼，多个后翼，至少一个马达以及由至少一个驱动的至少三个空气动力推进器发动机。每个前翼延伸一个前翼平面。每个后翼从后翼平面延伸。空气动力学推进器纵向安装在多个前翼和多个后翼之间。

7. 发明申请

US20150273351A1 REMOTE-CONTROL FLYING COPTER 有权
标题翻译：远程控制飞行复制
公开(公告)号：US20150273351A1
公开(公告)日：2015-10-01
申请号：US14686335
申请日：2015-04-14
申请人： QFO Labs, Inc.
发明人： John Paul Condon , James Edward Fairman , Bradley Dean Pedersen , Thomas Edward KraMer , Scott Andrew Melanson
IPC分类号： A63H27/00 , A63H30/04
CPC分类号： A63F13/235 , A63F13/00 , A63F13/245 , A63F13/837 , A63H13/00 , A63H17/00 , A63H17/32 , A63H27/00 , A63H27/12 , A63H30/04 , A63H33/26 , A63H2200/00 , B64C2201/027 , B64C2201/042 , B64C2201/146 , B64C2203/00 , F21L4/027 , F21V23/0435 , F41G1/36 , G05D1/0033
摘要： A hovering remote-control flying craft having a molded frame assembly includes a plurality of arms extending from a center body with an electric motor and corresponding propeller on each arm. In various embodiments, the motor and propeller are mounted downward-facing at a distal portion of each arm with a motor cover over the motor. The center body can be formed of a two-piece molded structure that sandwiches a circuit board to provide structural support for the frame. The circuit board can include a plurality of tabs that facilitate mounting of wire connectors, and can also provide antennas and emitters for both IR and RF communications. In some embodiments, a removable safety ring protects the propellers from lateral contact.
摘要翻译：具有模制框架组件的悬停的遥控飞行器包括从中心体与电动机延伸的多个臂和在每个臂上的对应的螺旋桨。在各种实施例中，马达和螺旋桨在每个臂的远端部分朝下安装，马达盖上电动马达。中心体可以由两片模制的结构形成，其夹持电路板以为框架提供结构支撑。电路板可以包括便于安装导线连接器的多个接头，并且还可以为IR和RF通信提供天线和发射器。在一些实施例中，可移除的安全环保护螺旋桨免受横向接触。

8. 发明授权

US09038938B2 UAV kit 有权
标题翻译：无人机套件
公开(公告)号：US09038938B2
公开(公告)日：2015-05-26
申请号：US14003406
申请日：2012-03-26
申请人： Petter Muren , Trygve Frederik Marton , Geir Morten Mellem , Dag Henning Paulsen
发明人： Petter Muren , Trygve Frederik Marton , Geir Morten Mellem , Dag Henning Paulsen
IPC分类号： B64C39/02 , A63H27/00 , B64D47/08
CPC分类号： B64C39/024 , A63H27/12 , B64C39/028 , B64C2201/024 , B64C2201/127 , B64C2201/201 , B64C2201/203 , B64C2203/00 , B64D47/08
摘要： The embodiments herein disclose a personal UAV kit for storing, preparing and remote control of micro UAVs (40). The UAV kit includes a base unit (10), a control unit (30) and at least one UAV. The UAVs can typically be a winged aircraft with foldable wings or a helicopter with a two-bladed or foldable rotor. The base unit comprises UAV compartments for housing at least one UAV, bay (14) for storing the control unit, batteries and electronic components for charging, communication, control and processing and storing of data. In addition, the system includes an eye near display device for viewing system information and sensor data, typically live video, transmitted from the UAV.
摘要翻译：本文的实施方案公开了用于存储，准备和远程控制微型无人机（40）的个人UAV套件。 UAV套件包括基本单元（10），控制单元（30）和至少一个UAV。无人机通常可以是具有可折叠翼的有翼飞机或具有双叶片或可折叠转子的直升机。基座单元包括用于容纳至少一个UAV的UAV隔间，用于存储控制单元的舱（14），用于对数据进行充电，通信，控制和处理和存储的电池和电子组件。此外，该系统包括用于观看系统信息的眼睛附近，以及从UAV发送的通常是实时视频的传感器数据。

9. 发明授权

US08764506B2 Manually pivoting wings on a toy airplane 失效
标题翻译：在玩具飞机上手动旋转翅膀
公开(公告)号：US08764506B2
公开(公告)日：2014-07-01
申请号：US13283737
申请日：2011-10-28
申请人： Jon Vanderbeek , Ryan Kratz
发明人： Jon Vanderbeek , Ryan Kratz
IPC分类号： A63H27/00
CPC分类号： A63H27/007 , A63H27/14 , B64C2203/00
摘要： An embodiment of the invention includes a flying vehicle having a fuselage, a pair of wings, the ability to manually apply a force against a portion of the wings causing the leading edge of each wing to sweep outwardly, the ability to mechanically holding the wings in a predetermined swept position, and the ability to bias the wings towards an initial inwardly swept position. A launcher rod with a rubber band is used to launch the vehicle.
摘要翻译：本发明的一个实施例包括具有机身，一对机翼的飞行车辆，能够手动地将力抵靠在翼的一部分上，使得每个机翼的前缘向外扫掠，将机翼保持在机械上的能力预定的扫掠位置，以及将翼朝向初始向内扫掠位置偏置的能力。用橡皮筋的发射杆用于发射车辆。

10. 发明公开

US20240361777A1 GYRO UNIT AND STEERING SYSTEM 审中-公开
公开(公告)号：US20240361777A1
公开(公告)日：2024-10-31
申请号：US18643213
申请日：2024-04-23
申请人： Futaba Corporation
发明人： Masahiro TANAKA , Yuhei SUZUKI
IPC分类号： G05D1/245 , B64C19/00 , G05D1/223 , G05D109/22 , G05D111/50
CPC分类号： G05D1/245 , B64C19/00 , G05D1/223 , B64C2203/00 , G05D2109/22 , G05D2111/52
摘要： A gyro unit mounted on a steered object for performing steering based on a steering signal received from the outside comprises a gyro sensor, a calculation portion and a controller. The calculation portion is configured to perform calculations for posture control of the steered object based on the steering signal and a detection signal of the gyro sensor. The controller is configured to perform control such that a control direction of the posture control switches when the steered object moves forward and backward.

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