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    • 7. 发明授权
    • Rapidly-convertible roadable aircraft
    • 快速可转换的可行驶飞机
    • US06786450B1
    • 2004-09-07
    • US10082994
    • 2002-02-26
    • Harry Einstein
    • Harry Einstein
    • B64C356
    • B64C37/00B64C3/56B64C5/12B64C39/12Y02T50/14
    • A pusher canard aircraft convertible for road use. Canard outer sections are removable and are stored within the aircraft fuselage and the outer main wing sections rotate horizontally for storage on the fuselage top. The fuselage is designed as a lifting body which gives the aircraft three lifting surfaces. The lifting body takes advantage of ground effect, resulting in a lower landing speed. In road mode the vehicle as a 2 or 4 passenger model is smaller than a full size automobile. Hydraulic motor wheels propel the aircraft/vehicle for road use. An internal combustion engine within the fuselage drives the propeller for air operation. The propeller is disengaged, not removed, for land operation and the engine is used to drive an hydraulic pump to power the motor wheels for road use. A single nose wheel or two front wheels are used for both steering in landing/taxiing and for road use. In road mode, the appearance is as much like a van than as an aircraft. In flying mode, the appearance is not to unconventional.
    • 一个推进者的野营飞机可转换为道路使用。 加拿大外部部件是可移动的,并存储在飞机机身内,外部主翼部分水平转动以存储在机身顶部。 机身设计为提升机体,为飞机提供三个提升面。 提升体利用地面效应,降低着陆速度。 在道路模式下,作为2或4乘客模型的车辆小于全尺寸汽车。 液压马达轮驱动飞机/车辆进行道路使用。 机身内部的内燃机驱动螺旋桨进行空运。 螺旋桨脱离,不拆卸,用于陆上作业,发动机用于驱动液压泵为马达轮驱动道路使用。 单个前轮或两个前轮用于在着陆/滑行和道路使用中的转向。 在道路模式下,外观像一架面包车一样像飞机一样。 在飞行模式下,外观不是非常规的。
    • 8. 发明授权
    • Pusher type auto-plane
    • 推进式自动平面
    • US4627585A
    • 1986-12-09
    • US624521
    • 1984-06-25
    • Harry Einstein
    • Harry Einstein
    • B64C37/00B64C3/56
    • B64C37/00B60F5/02
    • An improved auto-plane has been invented which has been adapted for air travel and road travel using a Pusher type design. The present invention auto-plane has two main wings which are cut approximately parallel to an imaginary fuselage centerline at about two-thirds the distance in from the wing's outer tip to the imaginary centerline, one of the two main wings being hinged along its cut and above its top surface at a height sufficient to allow both of the two wings to be folded inward 180.degree. with one resting atop the other. The auto-plane includes a rear stabilizer system which can be retracted forward to reduce the overall length for road use, a Pusher type propeller, and a Pusher type aviation engine which is located within the fuselage to drive the propeller. Landing wheels are located on the underside of the fuselage in an aviation landing relationship, e.g. tricycle, and aviation controls are located within the fuselage to control the aviation engine, propeller and elevons and rudders. An independent land vehicle engine is located within the fuselage and connected to drive one or more of the wheels for land use. In an alternative embodiment, each wing is cut twice, once about one-quarter the distance in and once about three-quarters in, with hinges to allow unique double (spiral) folding to permit compact stocking of the twice folded wings.
    • 已经发明了一种改进的自动飞机,其已经适用于使用Pusher型设计的空中旅行和道路行驶。 本发明的自动平面具有两个主翼,其大致平行于虚拟的机身中心线,大约是从翼的外端到虚拟中心线的距离的三分之二,两个主翼中的一个沿其切口铰接, 在其上表面上方的高度足以允许两个翼片向内折叠180°,一个在另一个之上。 自动平面包括可以向前缩回的后稳定器系统,以减少道路使用的总长度,推进式推进器和位于机身内的推动式航空发动机以驱动螺旋桨。 着陆轮位于机身的下侧,具有航空着陆关系,例如。 三轮车和航空控制器位于机身内,用于控制航空发动机,螺旋桨,电梯和方向舵。 独立的陆地车辆发动机位于机身内并连接以驱动一个或多个车轮用于土地使用。 在替代实施例中,每个翼片被切割两次,一次约四分之一的距离,并且一度约四分之三英寸,具有铰链,以允许独特的双(螺旋形)折叠以允许紧凑的两倍折叠的翼片的放置。