To provide an unmanned aerial vehicle with deployable components (UAVDC).SOLUTION: An unmanned aerial vehicle with deployable components (UAVDC) may comprise a fuselage, a wing 110, and a control surface 120. The UAVDC may further comprise propulsion means 135 and/or a modular payload 140. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the wing stowed against the fuselage and the control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the wing deployed from the fuselage and the control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the wing telescoped in a nested manner to increase a wingspan of the deployed arrangement.SELECTED DRAWING: Figure 1C

    【課題】展開可能な構成要素を備えた無人航空機(UAVDC)を提供する。【解決手段】UAVDCは、胴体と、翼110と、制御面120とを備え得る。UAVDCは、推進手段135および/またはモジュール式ペイロード140をさらに備え得る。UAVDCは、複数の配置で構成され得る。例えば、コンパクト配置では、UAVDCは、胴体に寄せて格納された翼と、胴体に寄せて格納された制御面とを備え得る。展開配置では、UAVDCは、胴体から展開された翼と、胴体から展開された制御面とを備え得る。伸張配置では、UAVDCは展開配置の翼幅を増加させるために入れ子式に伸長された翼を備え得る。【選択図】図1C


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    Title :

    AERIAL VEHICLE WITH DEPLOYABLE COMPONENTS


    Additional title:

    展開可能な構成要素を備えた航空機



    Publication date :

    2019-05-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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