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    Injection molded wing structure for aerial vehicles
    1.
    发明授权
    Injection molded wing structure for aerial vehicles 有权

    公开(公告)号：US10933971B2

    公开(公告)日：2021-03-02

    申请号：US15836782

    申请日：2017-12-08

    Applicant: X Development LLC

    Inventor： Adam Woodworth ,  Adem Rudin ,  Stephen Benson

    IPC: B64C3/24 ,  B64C3/18 ,  B64C29/02 ,  B64C39/02

    Abstract: An example method of manufacturing a wing includes providing a wing frame. The wing frame includes a primary spar, a drag spar, a plurality of transverse frame elements having at least one spar joiner, and a plurality of mounting elements. The primary spar is coupled to the drag spar via the at least one spar joiner. The method further includes placing the wing frame into a mold, wherein the mold defines a shape of the wing. The method also includes injecting the mold with an air-filled matrix material, such that the air-filled matrix material substantially encases the wing frame and fills the defined shape of the wing, and such that the plurality of transverse frame elements provide torsional rigidity to the wing.

    ENERGY DISPERSION PLUG FOR UAV
    2.
    发明申请
    ENERGY DISPERSION PLUG FOR UAV 审中-公开

    公开(公告)号：US20190144097A1

    公开(公告)日：2019-05-16

    申请号：US15815428

    申请日：2017-11-16

    Applicant: X Development LLC

    Inventor： Stephen Benson ,  Adam Woodworth ,  Michael Nowakowski ,  James Schmalzried ,  Adem Rudin

    IPC: B64C1/06 ,  B64C39/02

    Abstract: An energy dispersion plug for use in an unmanned aerial vehicle (UAV) includes a blunt head section, a wedge section, and a rim section. The blunt head section has an outer side for receiving an impact force and an inner side opposite the outer side. The wedge section has a base end and a distal end opposite the base end. The wedge section extends at the base end from the inner side of the blunt head section towards the distal end and the distal end has a smaller cross-sectional area than the base end. The wedge section is shaped and sized to fit into an open end of a hollow structural member of the UAV and to transfer impact energy incident upon the blunt head section into the hollow structural member to shatter the hollow structural member into fragments.

    Injection Molded Wing Structure for Aerial Vehicles
    3.
    发明申请
    Injection Molded Wing Structure for Aerial Vehicles 审中-公开

    公开(公告)号：US20190176958A1

    公开(公告)日：2019-06-13

    申请号：US15836782

    申请日：2017-12-08

    Applicant: X Development LLC

    Inventor： Adam Woodworth ,  Adem Rudin ,  Stephen Benson

    IPC: B64C3/24 ,  B64C3/18

    Abstract: An example method of manufacturing a wing includes providing a wing frame. The wing frame includes a primary spar, a drag spar, a plurality of transverse frame elements having at least one spar joiner, and a plurality of mounting elements. The primary spar is coupled to the drag spar via the at least one spar joiner. The method further includes placing the wing frame into a mold, wherein the mold defines a shape of the wing. The method also includes injecting the mold with an air-filled matrix material, such that the air-filled matrix material substantially encases the wing frame and fills the defined shape of the wing, and such that the plurality of transverse frame elements provide torsional rigidity to the wing.

    WING STRUCTURE AND ATTACHMENT TO FRAME FOR UNMANNED AERIAL VEHICLES
    6.
    发明申请
    WING STRUCTURE AND ATTACHMENT TO FRAME FOR UNMANNED AERIAL VEHICLES 审中-公开

    公开(公告)号：US20190161185A1

    公开(公告)日：2019-05-30

    申请号：US15823129

    申请日：2017-11-27

    Applicant: X Development LLC

    Inventor： Adam Woodworth ,  Adem Rudin ,  Stephen Benson

    IPC: B64C39/02

    Abstract: Systems for wing structure and attachment to frame for Unmanned Autonomous Vehicle (UAV) are disclosed herein. In one embodiment, a UAV includes an H-frame having a wing spar secured to two or more boom carriers. The wing spar includes two or more mounting locations, where each of the two or more mounting locations of the wing spar secures a horizontal propulsion unit. The boom carriers include a plurality of mounting locations, each of the plurality of mounting locations of the boom carriers securing a vertical propulsion unit. The UAV also includes a pre-formed wing shell attached to the H-frame.

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