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    • 2. 发明授权
    • Model aircraft propulsion
    • 模型飞机推进
    • US3908305A
    • 1975-09-30
    • US42268873
    • 1973-12-07
    • SCHROEDER LLOYD A
    • SCHROEDER LLOYD A
    • A63H27/00A63H27/14A63H27/24A63H27/02A63H33/20
    • A63H27/14A63H27/02
    • A power pod is releasably coupled with a model aircraft, such as a model glider plane, to initially power the aircraft into flight and to thereafter separate from the aircraft under the influence of gravity. In the preferred embodiments of the invention, an adaptor element is affixed to the underside of the model aircraft fuselage, and the power pod itself is releasably coupled with the adaptor. The releasable coupling of the power pod with the adaptor is structured such that the power pod remains coupled with the adaptor to thereby power the model aircraft into flight as long as the power pod is providing a forward thrust. In one embodiment, the power pod separates from the adaptor when operation of the power pod ceases; in another embodiment, the power pod remains coupled with the adaptor after operation of the power pod ceases with the pod separating from the adaptor upon command of a remote control radio signal. Upon separation of the power pod from the adaptor, a parachute stored within the pod is deployed by means of a rip cord connected at one end to the model aircraft. The rip cord includes a replaceable, breakable link which breaks as the pod and the deployed parachute fall away from the model aircraft. The power pod includes an adjustable engine mounting plate for permitting the angle of thrust to be established at optimum inclination. The adaptor includes a layer of deformable, resilient material which permits the adaptor to mount without modification to different fuselage configurations. The parachute is attached to the power pod in such a way that the power pod lands in an orientation which minimizes any risk of damage to the pod upon impact with the ground.
    • 动力舱可释放地与示范飞机(例如模型滑翔机)共同起飞,以使飞机起飞使其飞行,然后在重力作用下与飞行器分离。 在本发明的优选实施例中,适配器元件固定到模型飞行器机身的下侧,并且动力箱本身可释放地与适配器联接。 动力舱与适配器的可释放的联接被构造成使得动力舱与适配器保持联接,从而只要动力舱提供向前的推力,模型飞机就能飞行。 在一个实施例中,当功率盒的操作停止时,电源盒与适配器分离; 在另一个实施例中,根据遥控无线电信号的命令,在功率盒的操作之后,电源盒保持与适配器耦合。 在将动力舱与适配器分离时,存储在舱内的降落伞通过在一端连接到模型飞机的裂缝部署。 裂缝包括一个可更换的,易断裂的环节,随着荚和部署的降落伞远离模型飞机而破裂。 动力箱包括可调节的发动机安装板,用于允许以最佳倾角建立推力角。 适配器包括可变形的弹性材料层,其允许适配器安装而不改变到不同的机身配置。 降落伞以这样的方式附接到动力舱,使得动力舱降落到使得在与地面碰撞时损坏舱架的任何风险最小化的方向上。
    • 8. 发明申请
    • Air swimming toy with driving device
    • 空气游泳玩具带驱动装置
    • US20130252502A1
    • 2013-09-26
    • US13573206
    • 2012-08-29
    • Randy Cheng
    • Randy Cheng
    • A63H27/22A63H27/24
    • A63H27/10A63H30/04A63H2027/1066
    • An air swimming toy includes a toy body, a driving device including an air propeller supported at a bottom side of the toy body for creating an air dynamic underneath the toy body, and a remote controller remotely controlling the driving device to operate the air propeller, wherein the air propeller is activated to rotate in order to control an altitude of the toy body via the air dynamic. In particular, when a controllable air pressure underneath the toy body is lesser than a surrounding air pressure, the toy body is elevated in the air, and when the controllable air pressure is higher than the surrounding air pressure, the toy body is dropped down in the air.
    • 一种空气游泳玩具,包括:玩具主体,包括支撑在玩具主体底部的空气推进器的驱动装置,用于产生玩具主体下方的空气动力;遥控器,远程控制驱动装置以操作空气推进器; 其中空气螺旋桨被激活以旋转,以便经由空气动力来控制玩具身体的高度。 特别地,当玩具身体下面的可控空气压力小于周围空气压力时,玩具本体在空气中升高,并且当可控空气压力高于周围空气压力时,玩具体落下 空气。
    • 9. 发明授权
    • Electric powered flying wing toy
    • 电动飞翼玩具
    • US07377832B2
    • 2008-05-27
    • US10754738
    • 2004-01-08
    • Mark Spencer Chamberlain
    • Mark Spencer Chamberlain
    • A63H27/24
    • A63H27/02A63H30/04
    • A radio-controlled electrically-powered model flying wing aircraft having a pusher propeller at the rear wing root powered by an electric motor mounted in a streamlined electric motor housing that extends into the wing and blends smoothly into the wing surface at the center wing chord. The motor housing, motor and propeller extend beyond the wing trailing edges to ensure efficient propeller operation and to reduce propeller-induced noise. A battery is secured in a resilient pouch and protected completely inside the wing root, serviceable from the bottom wing surface by removing a quick release flap. Major structural elements are composed of impact resistant, flexible, and resilient materials.
    • 一种无人电控制的电动动力飞行飞行器,其在后翼部具有推动螺旋桨,其由安装在流线型电动机壳体中的电动机驱动,该电动机壳体延伸到机翼中并且在中心翼弦处平滑地融合到机翼表面中。 电动机壳体,电动机和螺旋桨延伸超过机翼后缘,以确保有效的螺旋桨运行并减少螺旋桨引起的噪音。 电池被固定在弹性袋中,并完全保护在翼根内部,通过移除快速释放挡板可从底翼表面起作用。 主要结构元件由耐冲击,柔性和弹性材料组成。