Multicopters with variable flight characteristics

    公开(公告)号:US10407162B2

    公开(公告)日:2019-09-10

    申请号:US15112386

    申请日:2015-01-20

    Applicant: Robodub Inc.

    Inventor: Suvro Datta

    Abstract: An aircraft (40a) is provided that includes a plurality of arms (41, 42, 43, 44) with selected arms having the ability to either adjust their length, have arm segments operative to move about an articulated joint in two or three dimensions, or have one arm operative to adjust an angle between the one arm and another arm, or any combination of the foregoing. Thrust generators are repositionably mounted on selected arms, and a control system enables automated, on¬board, or remote control of the thrust generators, repositioning of the thrust generators on the arms, adjustment in the length of the selected arms, the movement of selected arms about the articulated joints, and adjustment of the angle between two or more arms, all while maintaining directional control of the aircraft in flight or on the ground. The aircraft has operational capabilities that exceed existing designs and facilitates manned and unmanned delivery of cargo and transportation of passengers.

    MULTICOPTERS WITH VARIABLE FLIGHT CHARACTERISTICS
    2.
    发明申请
    MULTICOPTERS WITH VARIABLE FLIGHT CHARACTERISTICS 审中-公开
    具有可变飞行特性的多功能飞机

    公开(公告)号:US20160340028A1

    公开(公告)日:2016-11-24

    申请号:US15112386

    申请日:2015-01-20

    Applicant: Robodub Inc.

    Inventor: Suvro Datta

    Abstract: An aircraft (40a) is provided that includes a plurality of arms (41, 42, 43, 44) with selected arms having the ability to either adjust their length, have arm segments operative to move about an articulated joint in two or three dimensions, or have one arm operative to adjust an angle between the one arm and another arm, or any combination of the foregoing. Thrust generators are repositionably mounted on selected arms, and a control system enables automated, on-board, or remote control of the thrust generators, repositioning of the thrust generators on the arms, adjustment in the length of the selected arms, the movement of selected arms about the articulated joints, and adjustment of the angle between two or more arms, all while maintaining directional control of the aircraft in flight or on the ground. The aircraft has operational capabilities that exceed existing designs and facilitates manned and unmanned delivery of cargo and transportation of passengers.

    Abstract translation: 提供了一种飞机(40a),其包括多个臂(41,42,43,44),其中选定的臂具有调节其长度的能力,具有操作以在两个或三个维度上围绕铰接接头移动的臂段, 或者具有可操作的一个臂来调节一个臂和另一个臂之间的角度,或者前述的任何组合。 推力发生器可重新定位地安装在所选择的臂上,并且控制系统实现对推力发生器的自动化,板载或遥控控制,将推力发生器重新定位在臂上,调节所选臂的长度, 关于铰接接头的臂,以及两个或更多个臂之间的角度的调整,同时保持飞行中或在地面上的飞行器的方向控制。 飞机具有超过现有设计的运行能力,并有助于人员和无人驾驶的货物和运输乘客。

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