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    REMOTELY OR AUTONOMOUSLY PILOTED REDUCED SIZE AIRCRAFT WITH VERTICAL TAKE-OFF AND LANDING CAPABILITIES
    4.
    发明申请
    REMOTELY OR AUTONOMOUSLY PILOTED REDUCED SIZE AIRCRAFT WITH VERTICAL TAKE-OFF AND LANDING CAPABILITIES 审中-公开
    远程或自动直升机减少尺寸的飞机具有垂直起落架能力

    公开(公告)号：US20150225079A1

    公开(公告)日：2015-08-13

    申请号：US14054080

    申请日：2013-10-15

    Applicant: Douglas L. Starck ,  Errica M. Starck

    Inventor： Douglas L. Starck ,  Errica M. Starck

    IPC: B64C29/00 ,  B64C39/10 ,  B64D27/16

    CPC classification number: B64C39/10 ,  B64C29/0066 ,  B64C39/024 ,  B64C2039/105 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/22 ,  B64D27/16 ,  Y02T50/12 ,  Y02T50/44

    Abstract: An aircraft having a vertical take-off and landing (“VTOL”) propulsion system aircraft, smaller than a standard manned aircraft and remotely or autonomously piloted. The aircraft comprises a symmetrical airfoil shape for the center body section that consists of ribs and spars maintaining an open area in the center. Situated within the open area of the center of the aircraft resides a duct system consisting of a ducted fan and five outlet vents. The main outlet vent functions as the exhaust exiting the aft portion of the aircraft, with the remaining four ducts used for the VTOL capabilities exiting the underside of the aircraft. The aircraft can have a range of wingspan, which can be scaled to satisfy needs and requirements, with a blended wing body that incorporates the inlet and duct system.

    Abstract translation: 具有垂直起飞和着陆（“VTOL”）推进系统飞机的飞机，小于标准载人飞机，远程或自主驾驶。 该飞行器包括对称的翼型形状，用于中心体部分，其由在中心保持开放区域的肋和翼梁组成。 位于飞机中心开放区域内的管道系统由管道风扇和五个出风孔组成。 主出口排气口作为离开飞机尾部的排气口，剩余的四个管道用于从飞机底面离开的垂直起降能力。 飞机可以具有一系列的翼展，其可以通过混合的翼体结合入口和管道系统而被缩放以满足需要和要求。

    Aircraft with topside only spoilers
    10.
    发明授权
    Aircraft with topside only spoilers 有权
    飞机只有顶部只有扰流板

    公开(公告)号：US07108230B2

    公开(公告)日：2006-09-19

    申请号：US10456176

    申请日：2003-06-06

    Applicant: Walter D. Clark

    Inventor： Walter D. Clark

    IPC: B64C3/58

    CPC classification number: B64C1/0009 ,  B64C5/08 ,  B64C9/12 ,  B64C9/32 ,  B64C9/323 ,  B64C9/34 ,  B64C39/024 ,  B64C2001/0045 ,  B64C2039/105 ,  B64C2201/028 ,  B64C2201/127 ,  B64C2201/22 ,  Y02T50/12 ,  Y02T50/32 ,  Y02T50/44

    Abstract: An aircraft with swept back wings and spoilers inlaid into the top surface near the tips of the wings. The aircraft also includes an elevator formed in the center back portion of the aircraft, which is also aft of the spoilers. It is aft to allow an auxiliary control in the elevator signal to cancel the unwanted pitch up moment caused by the spoilers only going up and being aft of the center of gravity of the aircraft. Roll is achieved with these spoilers by the direct action of the lift dumping on one side or the other and by taking advantage of the transformation of yaw into roll by the sweep back of the wings.

    Abstract translation: 一架飞机将翅膀和扰流板扫到靠近机翼尖端的顶面。 飞机还包括形成在飞行器的中心后部的电梯，其也是扰流板的后部。 这是为了允许电梯信号中的辅助控制来消除由扰流板仅上升并且处于飞机重心的后方引起的不期望的俯仰上升时刻。 通过电梯倾倒在一侧或另一侧上的直接作用，并且通过翼的扫掠利用偏转转动的优点，利用这些扰流板实现滚动。

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