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1. 发明授权

US06550715B1 Miniature vertical takeoff and landing aircraft 失效
标题翻译：微型垂直起降飞机
公开(公告)号：US06550715B1
公开(公告)日：2003-04-22
申请号：US10005746
申请日：2001-12-07
申请人： John Reynolds , Eric P. Young , Joseph Wurts , Eric Knutson
发明人： John Reynolds , Eric P. Young , Joseph Wurts , Eric Knutson
IPC分类号： B64C2706
CPC分类号： B64C39/028 , A63H27/12 , B64C27/20 , B64C2201/027 , B64C2201/042 , B64C2201/108
摘要： A vertical takeoff and landing aircraft is disclosed that includes a support structure having a motor mounted vertically thereto, with the motor having a propeller for rotation in a horizontal plane. A power supply for the motor is mounted to the support structure below the motor and electrical coupled thereto. A plurality of fins are attached by their first end to the power and extending radially outward therefrom. Vertical posts have there first ends attached to the second end of the fins and extend upward to the plane of rotation of the propeller. A ring is mounted horizontally to the second ends of the plurality of vertical posts surrounding the propeller. The torque produced by the drag of fins as the aircraft rotates in the opposite direction reacting the torque of the propeller equal to the torque of the propeller necessary to achieve hover. The rotational inertia of aircraft is made equal to the rotational inertia of the propeller.
摘要翻译：公开了一种垂直起降飞机，其包括具有垂直安装的马达的支撑结构，电动机具有用于在水平面中旋转的螺旋桨。用于电动机的电源安装到电动机下方的电气耦合的支撑结构上。多个翅片通过其第一端附接到动力并从其径向向外延伸。垂直柱的第一端附接到翅片的第二端，并向上延伸到螺旋桨的旋转平面。环绕水平地安装在围绕螺旋桨的多个垂直柱的第二端。当飞机沿相反方向旋转时，翼片拖动产生的扭矩使螺旋桨的扭矩等于实现悬停所需螺旋桨的扭矩。使飞机的转动惯量等于螺旋桨的旋转惯量。

2. 发明授权

US06626399B2 Miniature aircraft catapult 有权
标题翻译：微型飞机弹射器
公开(公告)号：US06626399B2
公开(公告)日：2003-09-30
申请号：US10025937
申请日：2001-12-26
申请人： Eric P. Young , John Reynolds , Mathew Curran , Joseph Wurts , Danny Gast
发明人： Eric P. Young , John Reynolds , Mathew Curran , Joseph Wurts , Danny Gast
IPC分类号： B64F106
CPC分类号： B64F1/06 , A63H27/14
摘要： A catapult for launching an aircraft is disclosed including a rail assembly having first and second ends. A support structure is provided for supporting the rail assembly above the ground at various upward angles. A container having an open end is releasably mounted on the first end of the rail assembly, the container for mounting the aircraft therein with a portion of the front end of the aircraft extending out of the open end. A device is provided for extracting the aircraft from the container and moving it from the first end to the second end of the rail assembly and release it when reaching the second end.
摘要翻译：公开了一种用于发射飞行器的弹射器，其包括具有第一端和第二端的导轨组件。提供了一种支撑结构，用于以各种向上的角度将轨道组件支撑在地面上方。具有开口端的容器可释放地安装在轨道组件的第一端上，用于将飞机安装在其中的容器具有飞行器前端的一部分延伸出开口端。提供一种用于从容器中提取飞行器并将其从轨道组件的第一端移动到第二端并且在到达第二端时将其释放的装置。

3. 发明授权

US06565041B1 Parachute assembly for a miniature aircraft 失效
标题翻译：降落伞装配的微型飞机
公开(公告)号：US06565041B1
公开(公告)日：2003-05-20
申请号：US10028956
申请日：2001-12-27
申请人： Eric P. Young , John Reynolds , Mathew Curran , Danny Gast , Joseph Wurts
发明人： Eric P. Young , John Reynolds , Mathew Curran , Danny Gast , Joseph Wurts
IPC分类号： B64D1780
CPC分类号： B64D17/40 , B64C39/024 , B64C39/028 , B64C2201/028 , B64C2201/042 , B64C2201/165 , B64C2201/185 , B64D17/54 , B64D17/76 , B64D17/80
摘要： A parachute system for a miniature aircraft having a storable parachute mounted on an upper surface of the aircraft. The system includes a canopy having a stored condition and an expanded condition. A plurality of suspension lines have first ends connected to the periphery of the canopy and second ends connected to an elastic member. First and second risers are connected by their first ends to the upper surface of the aircraft between the front end and center of gravity on either side of the longitudinal axis and by their second ends to the elastic member. A restraint system releasably restrains the parachute in the stored condition on the top surface of the aircraft; and a release system coupled to the restraint system releases the parachute upon command such that aerodynamic forces will cause the parachute to open.
摘要翻译：用于具有安装在飞行器的上表面上的可存放降落伞的微型飞机的降落伞系统。该系统包括具有存储条件和扩展状态的遮篷。多个悬挂线具有连接到顶盖的周边的第一端和连接到弹性构件的第二端。第一和第二立管通过其第一端连接到飞行器的上表面，在纵轴的任一侧上的前端和重心之间，并且通过其第二端连接到弹性构件。约束系统可释放地将降落伞限制在飞机顶表面上的储存状态; 并且联接到约束系统的释放系统根据命令释放降落伞，使得空气动力将使降落伞打开。

4. 发明授权

US06460445B1 Playload dispensing system 失效
标题翻译：播放点胶系统
公开(公告)号：US06460445B1
公开(公告)日：2002-10-08
申请号：US10038424
申请日：2002-01-07
申请人： Eric P. Young , John Reynolds , Brian Hershberger
发明人： Eric P. Young , John Reynolds , Brian Hershberger
IPC分类号： B64D104
CPC分类号： B64D1/06
摘要： A payload dispensing system for an aircraft is disclosed that includes a housing mounted to the aircraft. A hollow shaft is mounted to the housing having an open first end and a closed off second end with a hole therethrough. The payload includes an aperture having a first end on an external surface thereof and a second end in the interior therein. A wire cable releasably secures the payload to the housing such that the hollow shaft extends into the aperture of the payload. A compression spring is mounted at least partially within the hollow shaft, having a first end in contact with the second end of the hollow shaft and a second end in contact with the second end of the aperture within the payload, the spring having a compressed position when the hollow shaft is within the aperture in the payload and asserts a force tending to separate the payload from the aircraft. A cable cutter is used to cut the cable to release the payload from the housing, such that the spring forces the payload away from the aircraft and the hollow shaft guides the payload during separation.
摘要翻译：公开了一种用于飞机的有效载荷分配系统，其包括安装到飞行器的壳体。空心轴安装到壳体上，其具有敞开的第一端和封闭的第二端，其中穿过孔。有效载荷包括其外表面上具有第一端并且其内部具有第二端的孔。线缆可释放地将有效载荷固定到壳体，使得空心轴延伸到有效载荷的孔中。压缩弹簧至少部分地安装在中空轴内，其具有与中空轴的第二端接触的第一端和与有效载荷内的孔的第二端接触的第二端，弹簧具有压缩位置当空心轴在有效载荷内的孔内时，并且确定趋向于将有效载荷与飞行器分开的力。电缆切割器用于切割电缆以从壳体释放有效载荷，使得弹簧迫使有效载荷远离飞行器，空心轴在分离期间引导有效载荷。

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