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1. 发明授权

US07785694B2 Panel arrangement for an interior lining of a passenger cabin in an aircraft 有权
标题翻译：飞机上客舱内衬的面板布置
公开(公告)号：US07785694B2
公开(公告)日：2010-08-31
申请号：US10596981
申请日：2005-01-05
申请人： Rainer Müller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
发明人： Rainer Müller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
IPC分类号： B32B3/12 , B32B5/16
CPC分类号： B64C1/40 , A62C2/06 , A62C3/08 , A62C8/06 , A62C8/08 , B64C1/067 , Y10S428/92 , Y10S428/921 , Y10T428/236 , Y10T428/24149 , Y10T428/24917 , Y10T428/253
摘要： The invention relates to an arrangement for lining the interior of a passenger vehicle such as an airplane including a honeycomb formation of several honeycombs arranged side by side. At its end, the honeycomb body is supported by a cover layer supported above and below the honeycomb formation such that by means of two cover layers glued onto the honeycomb formation, a layer design of the honeycomb paneling is created, which layer design is arranged so as to extend parallel to the outer skin of the aircraft and follow the curvature of the outer skin. The honeycomb formation used is made of paper or aramide honeycombs or of a mixed combination of both honeycomb types; on whose cross section of the honeycomb body a CFK cover layer is positioned to both ends of the honeycomb bodies. As an alternative, further CFK insulation layers are glued onto the outer surface of the respective cover layer supported above and below the honeycomb formation, which cover layers comprise a CFK or GFK. Moreover, the layer design of the honeycomb paneling may comprise further honeycomb formations which are additionally stacked on and glued to the honeycomb formation used.
摘要翻译：本发明涉及一种用于衬垫乘客车辆的内部的装置，例如飞机，其包括并排布置的几个蜂窝的蜂窝结构。蜂窝体的端部由蜂窝结构体的上下支撑的覆盖层支承，通过粘合在蜂窝结构体上的两层覆盖层，形成蜂窝板的层设计，该层的设计被布置为平行于飞行器的外皮并且遵循外皮的曲率。使用的蜂窝结构体由纸或芳族聚酰胺蜂窝体或两种蜂窝类型的混合组合制成; 在蜂窝体的横截面上，CFK覆盖层位于蜂窝体的两端。作为替代方案，将另外的CFK绝缘层胶合到支撑在蜂窝结构上方和下方的相应覆盖层的外表面上，覆盖层包括CFK或GFK。此外，蜂窝板的层设计可以包括另外堆叠在所使用的蜂窝结构上并粘合到蜂窝结构上的蜂窝结构。

2. 发明申请

US20070023572A1 Fuselage 审中-公开
标题翻译：机身
公开(公告)号：US20070023572A1
公开(公告)日：2007-02-01
申请号：US10596979
申请日：2005-01-05
申请人： Rainer Muller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
发明人： Rainer Muller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
IPC分类号： B64C1/10
CPC分类号： B64C1/066 , B32B15/08 , B64C2001/0072 , B64C2001/0081 , Y02T50/43
摘要： The fuselage according to an exemplary embodiment is conceived in such a way as to prevent the spread of flames produced by a source of fire and acting on the fuselage from outside the aircraft environment. The fuselage concept takes into account materials or material combinations that will scarcely allow protection of the cabin area of an aircraft (upon emergency landing) to be violated by flames spreading from outside the aircraft environment, which may facilitate an evacuation of passengers from the aircraft. An aircraft fuselage, whose fuselage structure, in addition to other structural elements that are components of the mechanical strength bracing of the fuselage and help absorb its forces, encompasses an exterior skin consisting of various respective materials, which are designed to be resistant to shear, and incorporated as a bearing element into the mechanical strength bracing to absorb and transfer the forces and torques acting thereupon. The exterior skin is fabricated from a burn-through resistant semi-finished material consisting of a non-metallic material or a fireproof metallic material, wherein the semi-finished material can be molded through further processing. Also, the exterior skin may be realized by a semi-finished material combining a non-metallic material and a metallic material, wherein the produced exterior skin product is a hybrid material that can be molded and joined through further processing.
摘要翻译：根据示例性实施例的机身构想为防止由火源产生的火焰的扩散并且从飞机环境外部作用在机身上。机身概念考虑到材料或材料组合，几乎不允许保护飞机机舱区域（在紧急着陆时）被从飞机环境外部扩散的火焰所侵犯，这可能有助于乘客从飞机上撤离。飞机机身的机身结构除了作为机身的机械强度支撑部件并有助于吸收其力的其他结构元件之外，还包括由各种各样的材料构成的外部皮肤，其被设计成耐剪切，并且作为轴承元件并入到机械强度支撑件中以吸收和传递作用在其上的力和转矩。外部皮肤是由耐金属的半成品由非金属材料或耐火金属材料制成，其中半成品可以通过进一步加工成型。此外，外部皮肤可以通过组合非金属材料和金属材料的半成品材料来实现，其中所制造的外部皮肤产品是可以通过进一步加工而被模制和连接的混合材料。

3. 发明申请

US20090026787A1 INSULATION STRUCTURE FOR THE INTERNAL INSULATION OF A VEHICLE 审中-公开
标题翻译：车辆内部绝缘的绝缘结构
公开(公告)号：US20090026787A1
公开(公告)日：2009-01-29
申请号：US10596993
申请日：2005-01-05
申请人： Rainer Muller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
发明人： Rainer Muller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
IPC分类号： B60R13/01
CPC分类号： B60R13/0815 , A62C2/06 , B64C1/40
摘要： The present invention relates to an insulation structure for the internal insulation of a vehicle. The insulation structure will contribute to ensuring the fire protection for interior regions of the vehicle from a (conceivable) fire incursion from outside the vehicle environment, so that evacuation of the passengers from the vehicle is made significantly easier. Intended modifications to a typical insulation package will implement an elevation of the fire protection safety for separated interior regions lying proximal to a structure external skin.The insulation structure for the internal insulation of a vehicle comprises an insulation package, which is implemented using an insulation, and a film, which is positioned inside an intermediate space that includes internal paneling and an external skin of the vehicle. The insulation package is implemented homogeneously using a first insulation, whose insulation material is burn-through safe. Otherwise, the insulation package is constructed using distinct insulation regions, which are implemented using the first insulation and a second insulation, whose insulation material is burn-through unsafe. These insulation regions are positioned along a finite series and laid next to one another up to a terminating insulation region, whose insulation material is exchanged in alternating sequence. Otherwise, the insulation package is implemented homogeneously using a second insulation, whose insulation material is burn-through unsafe (fire endangered, flammable), multiple burn-through safe barrier layers being integrated in the second insulation.
摘要翻译：本发明涉及一种用于车辆内部绝缘的绝缘结构。绝缘结构将有助于确保车辆内部区域的防火从车辆环境以外的（可想到的）火灾中侵入，从而使得乘客从车辆撤离变得更加容易。对典型绝缘包装进行的修改将实现靠近结构外部皮肤的分离的内部区域的防火安全性的提升。用于车辆内部绝缘的绝缘结构包括使用绝缘体实现的绝缘包装，以及位于包括车辆的内部镶板和外部皮肤的中间空间内的膜。使用第一绝缘体均匀地实现绝缘封装，其绝缘材料是耐燃烧安全的。否则，使用不同的绝缘区域构建绝缘封装，绝缘区域使用第一绝缘层和第二绝缘层实现，其绝缘材料是烧穿不安全的。这些绝缘区域沿着有限系列定位，彼此相邻，直到终止绝缘区域，其绝缘材料以交替的顺序交换。否则，使用第二绝缘体（其绝缘材料是燃烧不安全（火灾濒危，易燃））的多个穿透安全阻挡层被集成在第二绝缘体中的绝缘包装被均匀地实施。

4. 发明申请

US20070018042A1 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：US20070018042A1
公开(公告)日：2007-01-25
申请号：US10596418
申请日：2005-01-05
申请人： Rainer Muller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
发明人： Rainer Muller , Peter Turanski , Wilko Oestereich , Reinelt Thorsten
IPC分类号： B64C30/00
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，增加了用于分开的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。

5. 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。

6. 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。

7. 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。

8. 发明申请

US20120208005A1 USE OF INORGANIC PARTICLES TO PRODUCE A BARRIER LAYER ON AIRCRAFT COMPONENTS 审中-公开
标题翻译：使用无机颗粒在飞机组件上生产障碍层
公开(公告)号：US20120208005A1
公开(公告)日：2012-08-16
申请号：US13456549
申请日：2012-04-26
申请人： Peter Turanski , Heinz-Peter Busch , Berend Schoke , Wilko Östereich
发明人： Peter Turanski , Heinz-Peter Busch , Berend Schoke , Wilko Östereich
IPC分类号： B32B5/16 , B29C65/14
CPC分类号： C08J5/24 , B29C70/585 , B32B3/12 , B32B5/02 , B32B5/024 , B32B29/02 , B32B2250/40 , B32B2255/02 , B32B2255/20 , B32B2260/021 , B32B2260/046 , B32B2264/104 , B32B2307/306 , B32B2307/3065 , B32B2605/003 , B32B2605/18 , Y02T50/43 , Y10T428/251
摘要： The present invention relates to a plastics material component for an aircraft, comprising (i) a substrate, which comprises one or more thermosetting plastics materials, and (ii) one or more layers which are applied to the substrate, at least one layer S1 comprising mica.
摘要翻译：本发明涉及一种用于飞行器的塑料材料部件，其包括（i）基底，其包括一种或多种热固性塑料材料，和（ii）施加到基底上的一层或多层，至少一层S1包括云母

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