METHOD FOR PROTECTING THE SURFACE OF AN AIRCRAFT AGAINST CONTAMINATION WITH INSECT RESIDUES AND/OR ICING
    1.
    发明申请
    METHOD FOR PROTECTING THE SURFACE OF AN AIRCRAFT AGAINST CONTAMINATION WITH INSECT RESIDUES AND/OR ICING 有权
    保护航空器表面防止污染物和/或污染物的方法

    公开(公告)号:US20120160963A1

    公开(公告)日:2012-06-28

    申请号:US13320842

    申请日:2010-05-18

    摘要: Method of protecting a part of a surface of an aircraft against contamination with insect residues and/or against icing, comprising the following steps:b) coating the part of the surface to be protected with a coating that can, within a period of ≦3 hours from take-off of the aircraft and in normal flying conditions, reduce the adhesion to the part of the surface to be protected until detachment occurs on the basis of (i) temperature change and/or (ii) UV radiation and/or (iii) addition of a decomposing component and/or (iv) difference in air humidity,b) exposing the part of the surface to be protected to (i) a temperature change and/or (ii) UV irradiation (iii) and/or addition of a decomposing component and/or (iv) a difference in air humidity, so that the coating together with any contaminants and/or icing thereon detaches.

    摘要翻译: 保护飞机表面的一部分免受昆虫残留物和/或结冰的污染的方法,包括以下步骤:b)用可涂覆的涂层涂覆待保护表面的一部分, 基于(i)温度变化和/或(ii)紫外线辐射和/或(ii)UV辐射和/或(ii)UV辐射和/或 (iii)分解成分的添加和/或(iv)空气湿度差异,b)将被保护表面的部分暴露于(i)温度变化和/或(ii)紫外线照射(iii)和/ 或添加分解成分和/或(iv)空气湿度差异,使涂层与其上的任何污染物和/或结冰分离。

    Method for protecting the surface of an aircraft against contamination with insect residues and/or icing
    2.
    发明授权
    Method for protecting the surface of an aircraft against contamination with insect residues and/or icing 有权
    用于保护飞机表面免受昆虫残留物和/或结冰污染的方法

    公开(公告)号:US09555901B2

    公开(公告)日:2017-01-31

    申请号:US13320842

    申请日:2010-05-18

    摘要: A method of protecting a part of a surface of an aircraft against contamination with insect residues and/or against icing is described. The method includes the following steps: a) coating the part of the surface to be protected with a coating that can, within a period of ≦3 hours from take-off of the aircraft and in normal flying conditions, reduce the adhesion to the part of the surface to be protected until detachment occurs on the basis of (i) temperature change and/or (ii) UV radiation and/or (iii) addition of a decomposing component and/or (iv) difference in air humidity, and b) exposing the part of the surface to be protected to (i) a temperature change and/or (ii) UV irradiation (iii) and/or addition of a decomposing component and/or (iv) a difference in air humidity, so that the coating together with any contaminants and/or icing thereon detaches.

    摘要翻译: 保护飞机表面的一部分免受昆虫残留物和/或结冰的污染的方法,包括以下步骤:b)用可涂覆的涂层涂覆待保护表面的一部分, 基于(i)温度变化和/或(ii)紫外线辐射和/或(ii)UV辐射和/或(ii)UV辐射和/或 (iii)分解成分的添加和/或(iv)空气湿度差异,b)将被保护表面的部分暴露于(i)温度变化和/或(ii)紫外线照射(iii)和/ 或添加分解成分和/或(iv)空气湿度差异,使涂层与其上的任何污染物和/或结冰分离。

    Arrangement for coating interior trim components in passenger aircraft while complying with relevant fire protection standards and at the same time improving thermal comfort
    3.
    发明申请
    Arrangement for coating interior trim components in passenger aircraft while complying with relevant fire protection standards and at the same time improving thermal comfort 审中-公开
    在符合相关防火标准的同时,对乘客机内饰件进行涂装,同时提高热舒适性

    公开(公告)号:US20050230544A1

    公开(公告)日:2005-10-20

    申请号:US11106784

    申请日:2005-04-15

    IPC分类号: B62D25/14 B64C1/06 B64C1/40

    CPC分类号: B64C1/40 B64C1/066

    摘要: The application describes an arrangement for coating interior trim components in passenger aircraft while complying with relevant fire protection standards and at the same time improving thermal comfort, with a layer arrangement which comprises a transparent layer and further functional layers, wherein the layer arrangement can be applied to the interior trim components, in particular to the side of the cabin wall which faces the passenger. At least in some regions, a rear coating that faces away from the interior of the cabin of the passenger aircraft has been applied to the transparent layer. Due to the rear coating of the transparent layer, the thermal comfort of passengers which are seated in the window regions of the cabin is believed to be enhanced. Furthermore, the rear coating may make it possible to comply with the relevant fire protection standards even with the use of foils made of polyolephines, for example polyethylene foils or polypropylene foils, which are more economical when compared to PVF (polyvinyl fluoride) foils and/or PVDF (polyvinylidene fluoride) foils, to form the transparent layer with the rear coating. Furthermore, the application of the layer structure to the interior trim components including the transparent layer may also serve decorative design purposes.

    摘要翻译: 本申请描述了一种用于在符合相关防火标准的同时涂覆客机中的内饰件的布置,并且同时提高了热舒适性,其中层布置包括透明层和其它功能层,其中可以应用层布置 到内饰件,尤其是面向乘客的舱壁侧。 至少在一些区域中,背面覆盖着客机内部的后部涂层被涂覆到透明层上。 由于透明层的后部涂覆,被认为是增加了坐在车厢窗口区域中的乘客的热舒适度。 此外,即使使用由聚烯烃制成的箔,例如聚乙烯箔或聚丙烯箔,后涂层也可以符合相关的防火标准,与PVF(聚氟乙烯)箔和/ 或PVDF(聚偏二氟乙烯)箔,以形成具有后涂层的透明层。 此外,将层结构应用于包括透明层的内部装饰部件也可以用于装饰设计目的。