MODIFIED TUBULAR
    2.
    发明公开
    MODIFIED TUBULAR 有权
    改造ROHR

    公开(公告)号:EP2893121A2

    公开(公告)日:2015-07-15

    申请号:EP13722299.8

    申请日:2013-04-09

    IPC分类号: E21B17/10

    摘要: A positioning member (11) for a tubular (10) is formed using a prefabricated fiber-reinforced resin shell (1) positioned upon a surface of the tubular and bonded to provide a protrusion upon the surface of the tubular. In a disclosed method a fiber-reinforced resin shell (1) is secured to an external surface of a tubular (10) thereby enclosing a cavity between the shell (1) and the surface of the tubular (10); a bonding agent is introduced through inlet ports (5) in a surface of the fiber-reinforced resin shell (1) to fill a cavity between the shell (1) and the surface of the tubular (10), and the bonding agent is cured.

    摘要翻译: 用于管状(10)的定位构件(11)使用预定的纤维增强树脂壳体(1)形成,所述预制纤维增强树脂壳体位于所述管状体的表面上并且被结合以在管状物的表面上提供突起。 在公开的方法中,纤维增强树脂壳体(1)固定到管状物(10)的外表面,从而在壳体(1)和管状物(10)的表面之间封闭空腔; 通过纤维增强树脂外壳(1)的表面中的入口(5)引入粘合剂,以填充壳体(1)和管状物(10)的表面之间的空腔,并且粘合剂固化 。

    Thermally conductive flexible adhesive for aerospace applications
    3.
    发明公开
    Thermally conductive flexible adhesive for aerospace applications 审中-公开
    Thermischleitfähiges柔软的HaftmittelfürLuftfahrtanwendungen

    公开(公告)号:EP2911483A1

    公开(公告)日:2015-08-26

    申请号:EP15151072.4

    申请日:2015-01-14

    摘要: Provided are methods of forming thermally conductive flexible bonds for use in electronic boards of unmanned spacecrafts and other types of aircraft. Also provided are methods of preparing adhesive materials to form these bonds including methods of preparing treated filler particles. In some aspects, an adhesive material includes filler particles having organofunctional groups, such as boron nitride particles treated in silane. These particles may be combined with a urethane modified epoxy to form the adhesive material. The weight ratio of the particles in the adhesive material may be about 40-60%. The adhesive material may be thermally cured using a temperature of less than 110°C to prevent damage to bonded electronic components. The cured adhesive may have a thermal conductivity of at least about 2 W/m K measured in vacuum and may have a glass transition temperature if less than -40°C.

    摘要翻译: 提供了形成用于无人飞船和其他类型的飞机的电子板的导热柔性键的方法。 还提供了制备粘合剂材料以形成这些键的方法,包括制备经处理的填料颗粒的方法。 在一些方面,粘合剂材料包括具有有机官能团的填料颗粒,例如在硅烷中处理的氮化硼颗粒。 这些颗粒可以与氨基甲酸酯改性的环氧树脂组合以形成粘合剂材料。 粘合剂材料中的颗粒的重量比可以为约40-60%。 粘合剂材料可以使用小于110℃的温度进行热固化,以防止粘结的电子部件的损坏。 固化的粘合剂可以具有在真空中测量的至少约2W / m K的热导率,并且如果小于-40℃可具有玻璃化转变温度。

    TEXTILES BEKLEIDUNGSSTÜCK MIT WENIGSTENS EINER MIT PROTEKTORELEMENTEN BELEGTEN SCHÜRFSCHUTZZONE UND VERFAHREN ZU DESSEN HERSTELLUNG
    9.
    发明公开
    TEXTILES BEKLEIDUNGSSTÜCK MIT WENIGSTENS EINER MIT PROTEKTORELEMENTEN BELEGTEN SCHÜRFSCHUTZZONE UND VERFAHREN ZU DESSEN HERSTELLUNG 审中-公开
    衣物搭配与保护的元素未使用切割保护区至少有一个与方法及其纺织品

    公开(公告)号:EP3171722A1

    公开(公告)日:2017-05-31

    申请号:EP15745174.1

    申请日:2015-07-24

    发明人: LAMBERTZ, Bodo

    IPC分类号: A41D13/015 A41D13/05

    摘要: In a method for producing a textile piece of clothing with at least one abrasion-prevention zone provided with protector elements, the following steps are provided: 1) supplying a textile carrier layer (1), which can be stretched and is supplied in the form of a flexible tube (1) which is open at both ends and into which is introduced, prior to the coating material (5) being applied, a supporting element (2), by means of which the flexible tube (1) is pre-stretched and tensioned in a crease-free manner in the abrasion-prevention zones provided. 2) Supplying a pasty, curable coating material (5); 3) applying a multiplicity of portions of the coating material (5) to a surface of the carrier layer in order to form the protector elements, wherein the portions of coating material (5) are arranged on the surface such that the portions do not overlap and only part of the surface of the carrier layer is covered by the coating material (5). For this purpose, use is made of a metallic mould plate (10, 20), which contains a multiplicity of concave mould cavities (11, 21) for forming the protector elements (101), said mould cavities being filled with the pasty coating substance (5), and which is positioned, by way of the surface (12, 22) provided with the openings of the mould cavities (11, 21), on the flexible tube (1), which is supported by the supporting plate (2). 4) Curing the coating material (5), using temperature, to form a multiplicity of hard protector elements on the carrier layer.

    摘要翻译: 在用于生产织物片的与设有保护器元件的至少一个磨损预防区服装的方法,提供了以下步骤:1)供给织物载体层(1),其可被拉伸,并且在形式供给 柔性管(1),所有这些是在两端和到所有被引入开放的,之前的涂层材料(5)被施加,支撑元件(2)借助于该挠性管(1)是预 拉伸和在所提供的磨损防止区域的无折皱的方式拉紧。 2)供给糊状,固化涂料(5); 3)在为了形成所述保护器元件施加涂层材料(5)的部分的多个到载体层的表面上,worin涂层材料的部分(5)被布置成检查没有的部分不重叠的表面上 且仅在载体层的表面的一部分被所述涂层材料(5)覆盖。 为了这个目的,使用由金属模具的板(10,20),其中包含凹模腔用于形成保护元件(101)的多个(11,21),所述模腔填充有糊状涂层物质 (5),和所有其被定位,通过2设置有柔性管(1)的模腔(11,21)的开口部的所有表面(12,22),其由所述支撑板支撑的方式( )。 4)固化涂层材料(5),使用的温度,以形成在载体层上硬保护元件的多重性。