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    AERIAL VEHICLE WITH DEPLOYABLE COMPONENTS
    1.
    发明申请
    AERIAL VEHICLE WITH DEPLOYABLE COMPONENTS 审中-公开
    具有可部署组件的空中车辆

    公开(公告)号：WO2017082954A1

    公开(公告)日：2017-05-18

    申请号：PCT/US2016/028649

    申请日：2016-04-21

    Applicant: AREA-I INC.

    Inventor： ALLEY, Nicholas Robert ,  STEELE, Joshua Lemming ,  WILLIAMS, Jesse Owen ,  KUEHME, Daniel ,  PHILLIPS, Jonathan Caleb

    IPC: B64C3/56

    CPC classification number: B64C3/40 ,  B64C1/36 ,  B64C3/54 ,  B64C3/546 ,  B64C3/56 ,  B64C5/02 ,  B64C5/12 ,  B64C5/16 ,  B64C11/28 ,  B64C13/24 ,  B64C13/30 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/102 ,  B64C2201/12 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2211/00 ,  Y02T50/14 ,  Y02T50/44

    Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.

    Abstract translation: 公开了一种具有可展开组件（UAVDC）的无人驾驶飞行器。 UAVDC可以包括机身，至少一个机翼和至少一个控制表面。 在一些实施例中，UAVDC可以进一步包括推进装置和/或模块化有效载荷。 UAVDC可以以多种配置来配置。 例如，在紧凑布置中，UAVDC可以包括抵靠机身存放的至少一个机翼和抵靠机身存放的至少一个控制表面。 在展开布置中，UAVDC可以包括从机身展开的至少一个翼和从机身展开的至少一个控制表面。 在扩展布置中，UAVDC可包括伸缩的至少一个翼以增加展开布置的翼展。

    FOLDABLE PROPELLER BLADE WITH LOCKING MECHANISM
    2.
    发明申请
    FOLDABLE PROPELLER BLADE WITH LOCKING MECHANISM 审中-公开

    公开(公告)号：WO2018183535A1

    公开(公告)日：2018-10-04

    申请号：PCT/US2018/024891

    申请日：2018-03-28

    Applicant: AREA-I INC.

    Inventor： ALLEY, Nicholas ,  STEELE, Joshua ,  WILLIAMS, Jesse ,  KUEHME, Daniel

    IPC: B64C11/28 ,  B64C39/02

    Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement. The UAVDC may also comprise a foldable propeller blade with a locking mechanism. Foldable propeller blades may have a stowed configuration and a deployed configuration, and the foldable propeller blades may pivot about a hinge to move between configurations. A foldable propeller blade in a deployed configuration may experience forward folding motion due to forces acting upon it. A locking mechanism-for example, a ratchet and pawl-may lock a foldable propeller blade into a configuration. In a locked arrangement, a UAVDC may comprise at least one foldable propeller that locks into place to prevent forward folding tendency.

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