公开(公告)号：WO2005032681A2

公开(公告)日：2005-04-14

申请号：PCT/US2004/030423

申请日：2004-09-17

Applicant: WUEST, Wilmer, L.

Inventor： WUEST, Wilmer, L.

IPC: A63H1/00

CPC classification number: A63H27/04

Abstract: In one embodiment of the invention, a captive propelled model is provided comprising a balancing member having a pivoting pin disposed between two ends of the balancing member. A figurine having an actuator and at least one actuable member is disposed near one end of the balancing member, and a counterweight is disposed near the opposite end. A platform for the device includes wiring for connecting a power supply to the actuator. In a further embodiment of the invention, a conductive member is disposed so as to receive the pivoting pin and thereby establish an axis of rotation about which the balancing member rotates when propelled by the actuable member. The conductive surface is also in contact with a drag-line or the like that is suspended from the balancing member to establish an electrical ground for the power supply circuit. In a further embodiment of the invention, a captive propelled model further comprises a remote controller, a switch having a receiver to receive a control signal from the remote controller, and associated wiring and connections so that an operator can control the device remotely.

Abstract translation: 在本发明的一个实施例中，提供了一种自持式推进模型，其包括平衡构件，该平衡构件具有布置在平衡构件的两端之间的枢转销。 具有致动器和至少一个可致动构件的小雕像设置在平衡构件的一端附近，并且配重靠近相对端部布置。 该装置的平台包括用于将电源连接到致动器的布线。 在本发明的另一个实施例中，导电构件被设置成接收枢转销并由此建立平衡构件在被可致动构件推动时围绕其旋转的旋转轴线。 导电表面还与从平衡构件悬挂的拖线等接触，以为电源电路建立电接地。 在本发明的另一个实施例中，固定式推进模型进一步包括遥控器，具有接收器以从遥控器接收控制信号的开关，以及相关的布线和连接，使得操作者可以远程控制该设备。 p>

公开(公告)号：WO2004094018A2

公开(公告)日：2004-11-04

申请号：PCT/DE2004/000860

申请日：2004-04-22

Applicant: KRUZEL, Reinhold

Inventor： KRUZEL, Reinhold

IPC: A63H27/00

CPC classification number: A63H27/04

Abstract: Vorrichtung zum Antrieb von Flugzeugmodellen (1), bestehend aus einer ortsfes­ten Halterung (2, 12), einem drehbar an dieser gelagertem Gehäuse (3, 13), sowie einem Arm (4) an dem Gehäuse zur Befestigung eines Flugzeugmodells, wobei das Gehäuse (3, 13) eine Stromversorgung in Form von Batterien (2) oder Akkus sowie eine von dieser versorgte Steuerelektronik enthält, die zur Versorgung we­nigstens eines Elektromotors im Flugzeugmodell (1) dienen, wobei die Kabel zwischen der Steuerelektronik und dem Elektromotor am oder im Arm (4) ange­ordnet sind und der Arm über eine Steckverbindung mit der Steuerelektronik ver­bunden ist und wobei an der Vorrichtung ein Schalter zum Ein- und Ausschalten der Stromversorgung vorhanden ist.

Abstract translation: 用于模型飞机（1）的推进器，由所述壳体上的固定保持器（2，12），一个可旋转地支撑该滑动壳体（3，13）上，和一个臂（4）的用于附着模型飞机，所述壳体（ 3，13）包括的电池（2）或可充电电池和一个通过这些控制电子器件，其用于在模型飞机提供至少一个电动马达提供服务的形式的电源（1），由此，控制电子装置和上或在所述臂的电动机之间的电缆（ 4）被布置，并经由插塞连接到控制电子设备的臂被连接到所述设备，并且其中存在用于接通和关断电源的开关。

公开(公告)号：WO2004080556A2

公开(公告)日：2004-09-23

申请号：PCT/US2004002797

申请日：2004-02-02

Applicant: DAVIS STEVEN

Inventor： DAVIS STEVEN

IPC: A63H1/00 ,  A63H27/04 ,  A63H27/127 ,  A63H30/04 ,  A63H33/18 ,  B64C27/00 ,  A63H

CPC classification number: A63H27/04 ,  A63H27/12 ,  A63H30/04 ,  A63H33/18

Abstract: A rotating toy may then include a hub having a central axis and a lower portion; a plurality of counter rotating blades extending outwardly from the lower portion of the hub, the plurality of counter rotating blades having a tip connected to an outer ring; a single means for rotating the hub and blades sufficiently quickly to generate a major portion of the lift generated by the aircraft through the single rotating means; and the hub having an upper portion above the plurality of counter rotating blades and above the single rotating means such that the aircraft includes a center of gravity above the plurality of counter rotating blades to provide a self-stabilizing rotating toy. In furtherance thereto the single rotating means may be secured on the central axis and positioned below the counter rotating blades.

Abstract translation: 然后，旋转玩具可以包括具有中心轴线和下部分的轮毂; 多个反向旋转叶片，其从所述轮毂的下部向外延伸，所述多个反转叶片具有连接到外圈的尖端; 用于使轮毂和叶片足够快地旋转以产生飞行器通过单个旋转装置产生的升力的主要部分的单个装置; 并且所述轮毂在所述多个反转叶片上方具有上部并且在所述单个旋转装置上方，使得所述飞行器在所述多个反向旋转叶片之上包括重心以提供自稳定旋转玩具。 为了促进这一点，单个旋转装置可以固定在中心轴线上并且位于相对旋转叶片的下方。

公开(公告)号：WO2004041381A3

公开(公告)日：2004-09-16

申请号：PCT/GB0304742

申请日：2003-11-04

Applicant: LEVITATION TECHNOLOGIES LTD ,  JERMYN PHIL

Inventor： JERMYN PHIL

IPC: A63H27/04 ,  B64C13/20 ,  B64C27/00 ,  G01B11/27 ,  G05D1/08 ,  G01D5/34 ,  G02B27/28 ,  G06F3/02

CPC classification number: B64C27/00 ,  A63H27/04 ,  B64C13/20 ,  G01B11/272 ,  G05D1/0808

Abstract: A method and apparatus for controlling a powered craft in flight by an unsupported hand held control element. The position and attitude of the craft are controlled by the position and attitude of the control element. The position and attitude of the craft is determined with respect to a straight line between the controller and the craft, for example a beam of radiation. The controller and the craft are both provided with transducers comprising emitter and/or detector arrays in communication with one another.

Abstract translation: 一种用于通过不支撑的手持式控制元件在飞行中控制动力飞行器的方法和装置。 工艺的位置和姿态由控制元件的位置和姿态控制。 相对于控制器和飞行器之间的直线（例如辐射束）确定飞行器的位置和姿态。 控制器和工艺都配备有包括彼此连通的发射器和/或检测器阵列的换能器。

公开(公告)号：WO9948579A3

公开(公告)日：2000-02-03

申请号：PCT/US9905652

申请日：1999-03-15

Applicant: GRAY MATTER HOLDINGS LLC

Inventor： LE GETTE BRIAN EDWARD ,  MATLIN TAI HOON KIM ,  WARING JAMES ASHLEY

IPC: A63H27/04 ,  A63H27/08

CPC classification number: A63H27/08 ,  A63H27/04

Abstract: A remote controlled aircraft (100) has a center member (112) and a steering assembly. The steering assembly comprises a carriage (120), a remote control motor (121), a center member (112) and a connecting arm. The carriage (120) pivotably is attached to the center member (112). The remote control motor has a control arm (122) and is disposed within the carriage (120). The center member arm (830) has a first end and a second end. The first end of the center member arm is fixedly attached to the center member (812). The center member (812) and the center member arm (830) is arranged in a non-parallel manner. The connecting arm (840) has a first end and a second end. The first end of the connecting arm (840) is pivotably attached to the second end of the center member arm (830). The second end of the connecting arm (840) is pivotably attached to the control arm (822) of the remote control motor (821).

Abstract translation: 遥控飞机（100）具有中心构件（112）和转向组件。 转向组件包括滑架（120），遥控马达（121），中心构件（112）和连接臂。 滑架（120）可枢转地附接到中心构件（112）。 遥控马达具有控制臂（122）并设置在托架（120）内。 中心构件臂（830）具有第一端和第二端。 中心构件臂的第一端固定地附接到中心构件（812）。 中心构件（812）和中心构件臂（830）以非平行的方式布置。 连接臂（840）具有第一端和第二端。 连接臂（840）的第一端可枢转地附接到中心构件臂（830）的第二端。 连接臂（840）的第二端可枢转地附接到遥控马达（821）的控制臂（822）。

公开(公告)号：WO1994009877A1

公开(公告)日：1994-05-11

申请号：PCT/FI1993000437

申请日：1993-10-26

Applicant: KAISIO, Jukka, Petri ,  KUKKONEN, Jari, Kalevi

IPC: A63H27/04

CPC classification number: A63H33/18 ,  A63H27/04

Abstract: A throw and fly device used as a toy, for recreational purposes and as sporting equipment. In a device constructed according to the present invention the base-part (1), the axle (2) and the flange (3) form a spool for the string (4). When thrown the device glides and the string (4) unwinds from the said spool accelerating the speed of rotation of the device. The energy thereby stored in the form of rotational movement returns the device back to the user and the device is ready for a new flight.

Abstract translation: 用作玩具的扔和飞行设备，用于娱乐目的和作为运动设备。 在根据本发明构造的装置中，基部（1），轴（2）和凸缘（3）形成用于绳（4）的线轴。 当抛出装置时，装置滑出并且弦线（4）从所述线轴展开，加速装置的旋转速度。 因此以旋转运动的形式存储的能量将设备返回给用户，并且设备准备好进行新的飞行。

公开(公告)号：WO2015150470A1

公开(公告)日：2015-10-08

申请号：PCT/EP2015/057210

申请日：2015-04-01

Applicant: KITEMILL AS

Inventor： BU, Olav Aleksander

IPC: B64C31/06

CPC classification number: A63H27/04 ,  B64C31/06 ,  F03D5/00 ,  F05B2240/917 ,  F05B2240/921 ,  Y02E10/70 ,  Y02E10/728

Abstract: The invention relates to a tethered aircraft and the control of such tethered aircrafts, for example for use in Airborne Wind Energy (AWE) applications. Tethered aircrafts can use bridles (15) distributed along the span-direction to improve the structural integrity and reduce weight, but this results in them becoming roll-limited to some extent, making normal banking and rolling inapplicable to yaw the aircraft. The invention provides solutions to yaw a roll-limited aircraft and to control the degree of roll-limitation from the bridles (15), which render the rudder and lo several other vertical control surfaces unnecessary in turning and controlling yaw of the aircraft. These can therefore be omitted with the advantages of less drag, less weight and simpler design.

Abstract translation: 本发明涉及一种有束缚的飞行器以及这种系留飞行器的控制，例如用于机载风能（AWE）应用中。 连接飞机可以使用沿跨度方向分布的桁架（15）来提高结构完整性并减轻重量，但这导致它们在某种程度上受到滚动限制，使得正常的滚动和滚动不适用于偏航飞机。 本发明提供了用于偏转滚动限制飞机的解决方案，并且控制来自襟翼（15）的滚动限制的程度，这使得方向舵和其他几个垂直控制表面在转动和控制飞行器的偏航方面是不必要的。 因此，可以省略阻力减小，重量轻，设计简单的优点。

公开(公告)号：WO2013155414A1

公开(公告)日：2013-10-17

申请号：PCT/US2013/036371

申请日：2013-04-12

Applicant: MATTEL, INC.

Inventor： CHUANG, Peter ,  VERBERA, Steven

IPC: A63H18/00 ,  A63H18/02 ,  A63H27/14 ,  A63H33/00

CPC classification number: A63H19/24 ,  A63H21/04 ,  A63H27/04

Abstract: A carrier (80, 280) and a conventional toy vehicle (70) have structures (78, 86, 286) to releasably connect the two together. The carrier is configured to support the vehicle to run along a T shaped portion (42b, 42a) of monorail track (40). The carrier has a main housing (82, 282) having the mating structure and a through channel (84, 284) on upper (82a, 282a) and lower (82b, 282b) sides. Rollers (94, 294) support the carrier to move on the upper running surface (43) of the track while other structures (97, 297) extend beneath the running surface to capture the surface in the through channel. Weights (92, 292) are supported from the main housing in legs (88, 288) below the main housing, through channel and running surface.

Abstract translation: 载体（80,280）和常规玩具车（70）具有将两者可释放地连接在一起的结构（78,86,286）。 载体构造成支撑车辆沿着单轨轨道（40）的T形部分（42b，42a）行进。 载体具有具有配合结构的主壳体（82,282）和在上部（82a，282a）和下部（82b，282b）侧上的通道（84,284）。 辊（94,294）支撑载体在轨道的上运行表面（43）上移动，而其他结构（97,297）在运行表面下方延伸以捕获通道中的表面。 重物（92,292）通过通道和运行表面从主壳体下方的腿部（88,288）从主壳体支撑。

公开(公告)号：WO2013106152A1

公开(公告)日：2013-07-18

申请号：PCT/US2012/069004

申请日：2012-12-11

Applicant: GONZALEZ, Alejandro Doring

Inventor： GONZALEZ, Alejandro Doring

IPC: A63H27/00 ,  A63H27/10 ,  A63H29/24 ,  A63H33/00

CPC classification number: A63H27/10 ,  A63H27/04 ,  A63H31/00 ,  A63H2027/1041 ,  A63H2027/1066

Abstract: A balloon toy includes a balloon; a balloon string tethered to the balloon; and a balloon raising and lowering assembly including: a housing including a handle; a balloon string reel rotatably carried within the housing and carrying the balloon string; an electric motor carried within the housing; a power source carried within the housing for powering the electric motor; a gear assembly including a plurality of gears carried with the housing and operable coupling the electric motor to the balloon string reel for driving rotation of the balloon string reel; a biasing member including a biasing force that urges the gear assembly together so that the plurality of gears are engaged for driving rotation of the balloon string reel for drawing in the balloon string and helium-field balloon and allows the plurality of gears to slip relative to each other if tension on the balloon string is too high.

Abstract translation: 气球玩具包括气球; 气球弦拴在气球上; 以及气球升降组件，包括：包括手柄的壳体; 可旋转地承载在壳体内并携带气球弦的气球弦线盘; 承载在壳体内的电动马达; 在壳体内承载的用于为电动机提供动力的电源; 齿轮组件，其包括与所述壳体一起承载的多个齿轮，并且可操作地将所述电动机耦合到所述气球绳卷轴，以驱动所述气球绳卷轴的旋转; 偏压构件，其包括将齿轮组件推压到一起的偏压力，使得多个齿轮接合以驱动用于吸入气球串和氦气球的气球绳卷轴的旋转，并允许多个齿轮相对于 彼此之间如果气球弦上的张力太高。

公开(公告)号：WO99048579A2

公开(公告)日：1999-09-30

申请号：PCT/US1999/005652

申请日：1999-03-15

IPC: A63H27/04 ,  A63H27/08 ,  A63H

CPC classification number: A63H27/08 ,  A63H27/04

Abstract: A remotely controlled aircraft has a center member and a steering assembly. The steering assembly comprises a carriage, a remote control motor, a center member and a connecting arm. The carriage pivotably is attached to the center member. The remote control motor has a control arm and is disposed within the carriage. The center member arm has a first end and a second end. The first end of the center member arm is fixedly attached to the center member. The center member and the center member arm is arranged in a non-parallel manner. The connecting arm has a first end and a second end. The first end of the connecting arm is pivotably attached to the second end of the center member arm. The second end of the connecting arm is pivotably attached to the control arm of the remote control motor.

Abstract translation: 遥控飞机具有中心构件和转向组件。 转向组件包括滑架，遥控马达，中心构件和连接臂。 托架可枢转地附接到中心构件。 遥控马达具有控制臂并设置在滑架内。 中心构件臂具有第一端和第二端。 中心构件臂的第一端固定地附接到中心构件。 中心构件和中心构件臂以不平行的方式布置。 连接臂具有第一端和第二端。 连接臂的第一端可枢转地附接到中心构件臂的第二端。 连接臂的第二端可枢转地安装在遥控马达的控制臂上。