首页> 外国专利> METHOD OF APPLYING A SULPHUR CONTAINING SEALING COMPOUND APPARATUS THEREFOR CORRESPONDINGLY TREATED AEROSPACE VEHICLE AND USE THEREOF

METHOD OF APPLYING A SULPHUR CONTAINING SEALING COMPOUND APPARATUS THEREFOR CORRESPONDINGLY TREATED AEROSPACE VEHICLE AND USE THEREOF

机译:相应处理的航空航天飞机上应用含硫密封复合设备的方法及其使用

摘要

The invention relates to a method of sealing coating or/and aerodynamic smoothing of at least one connecting element that protrudes from a surface or/and for sealing coating or/and aerodynamic smoothing of a surface at a gap or at an uneven connection site with a sulphur containing SCOD sealing compound at at least one application site especially on an aerospace component with at least one nozzle element and with at least one irradiation unit which is characterized in that i) a nozzle element contains a mixed sealing compound and is guided or/and mounted over the connecting element protruding from a surface over the gap or/and over the uneven connection site ii) the connecting element protruding from the surface the gap or the uneven connection site is covered fully with sealing compound the sealing compound forming a sealing compound cover essentially in the form of a sealing compound cap a coating or/and a mound shaped or bead shaped elevation iii) the nozzle element or at least a portion is raised if required from the surface having the sealing compound cover and iv) the curing of the sealing compound is initiated with the aid of at least one irradiation unit by energy input and by release of a latent catalyst or is brought about by direct activation of at least one reaction component such that the mixed sealing compound subsequently hardens or/and hardens further. The invention also relates to a corresponding apparatus to the aerospace vehicle treated in this way and to the use of the method and the apparatus.
机译:本发明涉及一种密封至少一个从表面突出的连接元件的涂层或/和空气动力学平整的方法,和/或用于在间隙或不平坦的连接部位处用至少一个连接元件密封涂层或/和空气动力学平整的方法。在具有至少一个喷嘴元件和至少一个辐照单元的至少一个应用场所,特别是在航空部件上的含硫的SCOD密封剂,其特征在于:i)喷嘴元件包含混合的密封剂并被引导或/和/或ii)连接元件从间隙或不平坦的连接部位的表面伸出,或者从不平坦的连接部位的表面伸出; ii)从间隙或不平坦的连接部位的表面伸出的连接元件完全用密封胶覆盖,形成密封胶盖的密封胶iii)喷嘴元件或至少在密封胶帽的形式上形成涂层或/和土墩形或珠形凸起如果需要的话,从具有密封剂覆盖物的表面上升高一部分,并且iv)借助于至少一个辐射单元通过能量输入和通过释放潜在的催化剂来引发密封剂的固化,或通过直接活化至少一种反应组分,使得混合的密封剂随后硬化或/和进一步硬化。本发明还涉及以这种方式处理的航空航天器的相应设备以及该方法和设备的用途。

著录项

  • 公开/公告号IN201727031784A

    专利类型

  • 公开/公告日2017-11-10

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN201727031784

  • 申请日2017-09-08

  • 分类号C09K3/10;

  • 国家 IN

  • 入库时间 2022-08-21 13:38:16

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号