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1. 发明授权

US07883056B2 Insulation arrangement for the internal insulation of a vehicle 有权
标题翻译：车辆内部绝缘的绝缘布置
公开(公告)号：US07883056B2
公开(公告)日：2011-02-08
申请号：US10596418
申请日：2005-01-05
申请人： Rainer Mueller , Peter Turanski , Wilko Oestereich , Thorsten Reinelt
发明人： Rainer Mueller , Peter Turanski , Wilko Oestereich , Thorsten Reinelt
IPC分类号： B64C1/40
CPC分类号： B64C1/40 , Y10T428/234
摘要： The present invention relates to an insulation structure for the internal insulation of a vehicle. The insulation structure is improved in such a way that using it a fire incursion of the flames of a source of fire acting from outside the vehicle environment into the vehicle interior is excluded as much as possible, an increase of the fire protection safety for separate interior regions lying proximal to a structure external skin being implemented by the type of the film insulation of the insulation package. The insulation structure comprises an insulation package (3), in which an insulation core (1) is embedded, and a film (11). The insulation package (3) is positioned inside an intermediate space which encloses internal paneling and an external skin. It is completely enclosed by the film (11). The film (11) is implemented using a burn-through safe film material, which is an obstruction to a flaming fire, to which a film surface region of this film is subjected during an occurring fire catastrophe.
摘要翻译：本发明涉及一种用于车辆内部绝缘的绝缘结构。绝缘结构的改进使得使用火焰从车辆环境外部到达车辆内部的火源起火被排除在尽可能之外，增加了对于单独内部的防火安全性通过绝缘包装的膜绝缘体的类型来实现靠近结构外皮的区域。绝缘结构包括其中嵌入绝缘芯（1）的绝缘封装（3）和薄膜（11）。绝缘包装（3）位于包围内部镶板和外部皮肤的中间空间的内部。它被电影（11）完全包围。胶片（11）使用穿透安全膜材料来实现，该烧穿安全膜材料是在发生的火灾灾难期间该膜的膜表面区域经受的火焰的阻塞。

2. 发明申请

US20060284014A1 Insulation package arrangement for insulating the interior of an aircraft fuselage 有权
标题翻译：用于绝缘飞机机身内部的绝缘包装
公开(公告)号：US20060284014A1
公开(公告)日：2006-12-21
申请号：US10596982
申请日：2005-01-05
申请人： Rainer Muller , Peter Turanski , Wilko Oestereich , Thorsten Reinelt
发明人： Rainer Muller , Peter Turanski , Wilko Oestereich , Thorsten Reinelt
IPC分类号： B64C1/00
CPC分类号： B64C1/40 , A62C2/06 , A62C3/08 , B64D25/00
摘要： The design and attachment of an insulation package according to an exemplary embodiment, which may be installed near the fuselage structure, is believed protect the cabin region of an aircraft against fire whose flames act 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 longitudinally adjoin a support surface of the stringers which are attached to the aircraft fuselage, or longitudinally adjoin an inner area of a panel of outer skin and are attached to both longitudinal sides of the ribs. Furthermore, those insulation packages 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 design of a fuselage insulation package may be implemented with burn-through-proof insulation of a larger cross section and/or a burn-through-proof barrier layer of a smaller cross section which are arranged within the fuselage insulation package either singly or in combination. In this arrangement, the insulation or the barrier layer extends near to or adjacent to an interior wall region of the foil wall. As an alternative only that insulation which on the longitudinal end of the fuselage insulation package continues outward with a flat insulation end section is attached outside of and adjacent to the foil circumference of the fuselage insulation package. Said end section of insulation is attached to a rib-attachment region which is arranged below the respective longitudinal sides of a rib and near the stringer by means of burn-through-proof attachment elements.
摘要翻译：根据示例性实施例的可以安装在机身结构附近的绝缘包装的设计和附接被认为是保护飞机的舱区免受其火焰从飞机环境外部作用在绝缘包装上的火，从而明显地促进乘客从车辆撤离。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。它们可以纵向邻接连接到飞行器机身的纵梁的支撑表面，或者纵向毗邻外皮的面板的内部区域并且连接到肋的两个纵向侧。此外，这些绝缘包装可以被布置在由内部镶板和外部皮肤的面板封闭的空间中的耐烧穿箔完全包围。机身绝缘包装的设计可以通过较小截面的耐燃烧绝缘和/或较小横截面的耐烧穿隔离层来实施，该隔热层单独设置在机身绝缘包装内组合。在这种布置中，绝缘或阻挡层在箔壁的内壁区域附近或邻近延伸。作为替代，只有在机身绝缘包装的纵向端部上的平坦的绝缘端部向外延伸的绝缘体被安装在机身绝缘包装的箔片周边并与之相邻。所述绝缘体的所述端部附接到肋附接区域，所述肋附接区域布置在肋条的相应纵向侧下方并且通过耐烧穿附接元件靠近所述纵梁。

3. 发明授权

US08011619B2 Insulation package arrangement for insulating the interior of an aircraft fuselage 有权
标题翻译：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
申请人： Rainer Mueller , Peter Turanski , Wilko Oestereich , Thorsten Reinelt
发明人： Rainer Mueller , Peter Turanski , Wilko Oestereich , Thorsten Reinelt
IPC分类号： B64C1/40
CPC分类号： B64C1/40 , A62C2/06 , A62C3/08 , B64D25/00
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。

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