DISCONNECT ASSEMBLY FOR AN AERIAL DELIVERY APPARATUS

    公开(公告)号:US20190202569A1

    公开(公告)日:2019-07-04

    申请号:US15937805

    申请日:2018-03-27

    CPC classification number: B64D17/383 F16B21/12

    Abstract: A disconnect assembly configured to disconnect a parachute of an aerial delivery apparatus from a payload includes a detector device, a disconnect device, and a transmit cable. The detector device is configured to detect that the aerial delivery apparatus has landed, the disconnect device is configured to provide a releasable connection between the parachute and the payload, and the transmit cable is configured to transmit a mechanical trigger force from the detector device to the disconnect device. When the detector device detects that the aerial delivery apparatus has landed, the transmit cable transmits a mechanical trigger force from the detector device to the disconnect device and the disconnect device releases the connection between the parachute and the payload.

    AIRDROP PLATFORMS
    2.
    发明申请
    AIRDROP PLATFORMS 审中-公开
    机场平台

    公开(公告)号:US20150375861A1

    公开(公告)日:2015-12-31

    申请号:US14329102

    申请日:2014-07-11

    CPC classification number: B64D1/14 B64D17/22

    Abstract: An airdrop platform comprises a load-carrying base (10) having an upper surface and a lower surface. The upper surface includes attachment points (14) for one or more parachutes. The load-carrying base (10) is formed from a material, such as a glass fibre reinforced plastics material in the form of a grating, which is such as to flex to absorb energy on changes of the energy of the platform under the forces applied to the base (10) on parachute opening and on landing.

    Abstract translation: 空心平台包括具有上表面和下表面的承载基座(10)。 上表面包括用于一个或多个降落伞的附接点(14)。 承载基座(10)由诸如玻璃形式的玻璃纤维增​​强塑料材料形成,该材料能够在施加的力的作用下弯曲以吸收能量对平台能量的变化 在降落伞开放和着陆时到基地(10)。

    AERIAL DELIVERY PLATFORMS
    3.
    发明申请
    AERIAL DELIVERY PLATFORMS 审中-公开
    航空运输平台

    公开(公告)号:US20160075437A1

    公开(公告)日:2016-03-17

    申请号:US14850159

    申请日:2015-09-10

    CPC classification number: B64D17/22 B64D1/14 B64D9/00

    Abstract: An aerial delivery platform comprises first and second modules (10a, 10b) each having a respective load-bearing surface (14). The modules (10a, 10b) are hinged together for relative flexing movement about an axis (24) between the modules (10a, 10b). A superstructure of interconnected struts (25, 26, 27, 28, 29) is connected to, and is upstanding from, the modules (10a, 10b) to hold the modules (10a, 10b) with the load bearing surfaces (14) co-planar when loaded and during descent but being elastically deformable to permit limited relative flexing movement between the modules (10a, 10b) under the loads applied by parachute opening and on landing to assist in the absorption the energy transferred to the platform.

    Abstract translation: 空中交付平台包括第一和第二模块(10a,10b),每个模块具有相应的承载表面(14)。 模块(10a,10b)铰接在一起,用于围绕模块(10a,10b)之间的轴线(24)的相对弯曲运动。 互连支柱(25,26,27,28,29)的上部结构连接到模块(10a,10b)并且从模块(10a,10b)直立,以将模块(10a,10b)与承载表面(14)共同 在加载和下降期间但是可弹性变形以允许在由降落伞开口施加的负载和着陆下的模块(10a,10b)之间的有限的相对弯曲运动的平面以帮助吸收传递到平台的能量。

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