Insulation package for insulating a cabin of a vehicle
    1.
    发明授权
    Insulation package for insulating a cabin of a vehicle 有权
    用于绝缘车辆舱室的绝缘包装

    公开(公告)号:US08882041B2

    公开(公告)日:2014-11-11

    申请号:US12816524

    申请日:2010-06-16

    IPC分类号: B64C1/40

    摘要: An insulation package is provided for insulating a cabin of a vehicle that includes, but is not limited to at least one wrapping foil and at least one core layer of an insulation material. The wrapping foil envelopes the core layer at least in some regions and includes, but is not limited to at least one opening for feeding-through a holding element. On the wrapping foil a fastening element is arranged that is designed to establish a mechanical connection with the holding element fed through the opening. This can be a positive-locking or a non-positive-locking connection. By integrating the fastening element in the insulation package, the expenditure for separate fasteners can be saved so that the installation time and the different components can be reduced.

    摘要翻译: 提供一种用于绝缘车辆的绝缘包装,其包括但不限于至少一个包裹箔和绝缘材料的至少一个芯层。 包裹箔至少在一些区域包封芯层,并且包括但不限于用于馈送保持元件的至少一个开口。 在包裹箔上布置有紧固元件,其被设计成与通过开口馈送的保持元件建立机械连接。 这可以是正锁定或非正锁定连接。 通过将紧固元件集成在绝缘包装中,可以节省单独紧固件的费用,从而可以减少安装时间和不同的部件。

    Insulation package arrangement for insulating the interior of an aircraft fuselage
    5.
    发明授权
    Insulation package arrangement for insulating the interior of an aircraft fuselage 有权
    用于绝缘飞机机身内部的绝缘包装

    公开(公告)号:US08011619B2

    公开(公告)日:2011-09-06

    申请号:US10596982

    申请日:2005-01-05

    IPC分类号: B64C1/40

    摘要: The design and attachment of an insulation package near the fuselage structure to protect the cabin region of an aircraft against fire acting on the insulation package from outside the aircraft environment, thus clearly facilitating evacuation of the passengers from the vehicle. The insulation package arrangement may comprise several fuselage insulation packages of an elongated form. These packages may adjoin the aircraft fuselage structure in the direction of the longitudinal axis of the aircraft. They may be completely enclosed by a burn-through-proof foil which is arranged in a space enclosed by interior paneling and by the panels of the outer skin. The longitudinal end of the fuselage insulation package continues outward with a flat insulation end section is attached which is attached to a rib-attachment region arranged below the respective longitudinal sides of a rib and near the stringer by means of burn-through-proof attachment elements arranged on the inside of the aircraft with respect to the insulation.

    摘要翻译: 在机身结构附近设计和附接绝缘包,以保护飞机的舱区免受飞机环境外的作用在绝缘包装上的火,从而明显促进乘客从车辆的撤离。 绝缘包装件可以包括几个细长形式的机身绝缘包装。 这些包装件可以在飞行器的纵向轴线方向上与飞机机身结构相邻。 它们可以被布置在由内部镶片和外部皮肤的面板封闭的空间中的耐烧穿箔完全包围。 机身绝缘包装的纵向端部向外延伸,并且安装有平坦的绝缘端部,该平坦的绝缘端部附接到布置在肋的相应纵向侧下方并且靠近桁条下方的肋连接区域,其中通过防烧结附接元件 相对于绝缘体布置在飞行器的内部。