Point take-off and landing of unmanned flying objects

    公开(公告)号:US09637245B2

    公开(公告)日:2017-05-02

    申请号:US14401430

    申请日:2013-04-23

    Applicant: Meir Yoffe

    Inventor: Meir Yoffe

    CPC classification number: B64F1/02 B64C2201/182

    Abstract: Point take-off and landing systems for an unmanned flying object. In one embodiment, the flying object is guided along a flight trajectory and approaches a landing body such that a latching element, coupled with a suspension cable suspended from the flying body, latches with a receiving latch, coupled with an extendable retractable beam projecting horizontally from a landing body side surface. A cable release/retraction mechanism engages and then releases/retracts the suspension cable. The beam is as maneuvered to haul the flying object onto a landing surface. In another embodiment, the flying object is guided along a flight trajectory and approaches a landing body such that a latching element, coupled with a suspension cable suspended from the flying body, latches with a receiving cable, supported by cable supports projecting vertically from a landing body top surface. A cable release/retraction mechanism releases/retracts the suspension cable, hauling the flying object onto the landing surface.

    Point Take-Off and Landing of Unmanned Flying Objects
    2.
    发明申请
    Point Take-Off and Landing of Unmanned Flying Objects 审中-公开
    点起飞和着陆无人飞行物体

    公开(公告)号:US20150129716A1

    公开(公告)日:2015-05-14

    申请号:US14401430

    申请日:2013-04-23

    Applicant: Meir Yoffe

    Inventor: Meir Yoffe

    CPC classification number: B64F1/02 B64C2201/182

    Abstract: Point take-off and landing systems for an unmanned flying object. In one embodiment, the flying object is guided along a flight trajectory and approaches a landing body such that a latching element, coupled with a suspension cable suspended from the flying body, latches with a receiving latch, coupled with an extendable retractable beam projecting horizontally from a landing body side surface. A cable release/retraction mechanism engages and then releases/retracts the suspension cable. The beam is as maneuvered to haul the flying object onto a landing surface. In another embodiment, the flying object is guided along a flight trajectory and approaches a landing body such that a latching element, coupled with a suspension cable suspended from the flying body, latches with a receiving cable, supported by cable supports projecting vertically from a landing body top surface. A cable release/retraction mechanism releases/retracts the suspension cable, hauling the flying object onto the landing surface.

    Abstract translation: 用于无人驾驶飞行物体的起飞和着陆系统。 在一个实施例中,飞行物体沿着飞行轨迹被引导并且接近着陆体,使得与悬挂在飞行体上的悬挂缆索相耦合的闩锁元件与接收闩锁相结合,该可伸缩梁与从 着陆体侧面。 电缆释放/收回机构接合然后释放/缩回悬挂电缆。 梁被操纵以将飞行物体运送到着陆面上。 在另一个实施例中,飞行物体沿着飞行轨迹被引导并且接近着陆体,使得与悬挂在飞行体上的悬挂缆索相耦合的闩锁元件与接收缆线锁定,缆线支架由垂直地从平台突出的电缆支架 身体顶面。 电缆释放/收回机构释放/缩回悬挂电缆,将飞行物体拖到着陆面上。

    Point-landing method for non vertical take off and landing flying objects
    3.
    发明授权
    Point-landing method for non vertical take off and landing flying objects 失效
    非垂直起飞和着陆飞行物体的点着陆方法

    公开(公告)号:US4790497A

    公开(公告)日:1988-12-13

    申请号:US58815

    申请日:1987-06-05

    Applicant: Meir Yoffe

    Inventor: Meir Yoffe

    CPC classification number: B64F1/02 B64C2201/182

    Abstract: The present invention relates to a point landing method for a flying object, e.g., an aircraft (manned or unmanned), a helicopter, a missile, in a location which may be stationary, e.g., a ground plot or the roof of a building or a moving one, e.g., a car, ship, train.

    Abstract translation: 本发明涉及一种用于飞行物体的点着陆方法,例如飞行器(载人或无人驾驶),直升机,导弹,位于可能是静止的位置,例如地面或建筑物的屋顶,或 一个移动的,例如汽车,船只,火车。

    Accessory for vehicle
    4.
    发明申请
    Accessory for vehicle 审中-公开
    车辆附件

    公开(公告)号:US20080099622A1

    公开(公告)日:2008-05-01

    申请号:US11812301

    申请日:2007-06-18

    Applicant: Meir Yoffe

    Inventor: Meir Yoffe

    CPC classification number: F41F5/00 B64D1/02 B64D7/00

    Abstract: External store systems and assemblies for a carrier vehicle are provided. In some embodiments, the system includes a plurality of external store elements, each external store element comprising a plurality of surfaces defining an exterior thereof, the surfaces comprising at least one face, and a mounting arrangement configured for enabling reversible mounting of the elements to form at least one external store assembly having at least one of electrical continuity and aerodynamic conformality between adjacent external store elements, and for reversibly attaching the external store elements to a carrier vehicle.

    Abstract translation: 提供了用于运载工具的外部存储系统和组件。 在一些实施例中,系统包括多个外部存储元件,每个外部存储元件包括限定其外部的多个表面,所述表面包括至少一个表面,以及安装装置,其被配置为使元件能够可逆地安装以形成 至少一个外部存储组件具有相邻的外部存储元件之间的电连续性和空气动力学一致性中的至少一个,并且用于将外部存储元件可逆地附接到载体车辆。

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