Aircraft coupling mechanism
    1.
    发明授权

    公开(公告)号:US11724804B2

    公开(公告)日:2023-08-15

    申请号:US16381759

    申请日:2019-04-11

    CPC classification number: B64C37/02 B64C39/024 B64C2211/00 B64U10/13 B64U30/20

    Abstract: A male part and a female part can reversibly couple aircraft to one another using an attachment mechanism. The male part includes a wall forming a shaft and is operable to attach to a first aircraft. The female part includes a wall forming a cavity and is operable to attach to a second aircraft. The attachment mechanism can regulate a mechanical engagement between the shaft on the male part and the cavity on the female part while the first aircraft and the second aircraft are airborne or on land. The attachment mechanism is operable to switch between an engaged position and a disengaged position. In the engaged position, the attachment mechanism initiates the mechanical engagement to rigidly attach the first and the second aircraft to one another. In the disengaged position, the attachment mechanism discontinues the mechanical engagement to detach the first and the second aircraft from one another.

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