SPACE SUIT PROTECTIVE OVERCOVER
    1.
    发明申请
    SPACE SUIT PROTECTIVE OVERCOVER 审中-公开
    空间适合保护OVERCOVER

    公开(公告)号:US20080060101A1

    公开(公告)日:2008-03-13

    申请号:US11848443

    申请日:2007-08-31

    Applicant: David CADOGAN

    Inventor: David CADOGAN

    CPC classification number: B64G6/00 B64G1/52

    Abstract: A protective cover for a space suit, suitable for use in lunar or Mars visits which provides protection to the space suit against dust and organic contaminants while withstanding the rigors of contact with lunar or Martian rocks and equipment and not degrade or tear. The cover can be easily donned and doffed without contaminating the space suit. High strength coated fabrics which are functional in the thermal extremes of the lunar and Mars environments are suitable materials for the protective covers.

    Abstract translation: 适用于月球或火星探测的太空服防护罩,可防止太空服防尘和有机污染物,同时承受与月球或火星岩和设备的接触严酷,不会降解或撕裂。 盖子可以很容易地穿戴和脱落,而不会污染太空服。 在月球和火星环境的热极限中起作用的高强度涂层织物是保护罩的合适材料。

    Deployable, rigidizable wing
    2.
    发明申请
    Deployable, rigidizable wing 审中-公开
    可部署,可固化翼

    公开(公告)号:US20050151007A1

    公开(公告)日:2005-07-14

    申请号:US10770130

    申请日:2004-02-03

    CPC classification number: B64C39/024 B64C3/56 B64C2201/105

    Abstract: A novel design and construction method for an inflatable, rigidizable wing for a terrestrial or planetary flying vehicle. The wing is caused to deploy from an initially packed condition and to assume its functional shape by means of an inflation gas. After inflation, the wing is rigidized by any of several means, such that the inflation gas is no longer required. The composite wing is fabricated from a base reinforcement material, often a fabric, which is coated with a polymer resin that hardens when exposed to a curing mechanism. Several activation mechanisms exist by which to initiate rigidization of such a structure, including elevated temperature, ultraviolet light, and chemical constituents of the inflation gas. The resultant wing has fundamental advantages compared to existing inflatable wings, including improved stiffness, and reduced susceptibility to structural failure in response to puncture.

    Abstract translation: 一种用于陆地或行星飞行器的可充气,可固定翼的新颖设计和施工方法。 使机翼从初始包装状态部署,并通过充气气体承担其功能形状。 在膨胀之后,机翼通过几种手段中的任何一种来固定,使得不再需要膨胀气体。 复合翼片由基底增强材料制成,通常是织物,其涂覆有当暴露于固化机构时硬化的聚合物树脂。 存在几种启动机制,其通过其启动这种结构的刚性化,包括升高的温度,紫外线和膨胀气体的化学成分。 所得到的翼片与现有的充气翼相比具有基本的优点,包括改善的刚度,以及降低响应于穿刺的结构失效的敏感性。

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