首页> 外国专利> METHOD AND DEVICE FOR STRENGTHENING THE BASIS OR FABRIC IN THE CENTRAL STRUCTURE OF A COMPONENT, FOR example, FOR AIR OR SPACE AIRCRAFT, COMPONENT, FOR EXAMPLE, FOR AIR OR SPACE AIRCRAFT AND AIRCRAFT

METHOD AND DEVICE FOR STRENGTHENING THE BASIS OR FABRIC IN THE CENTRAL STRUCTURE OF A COMPONENT, FOR example, FOR AIR OR SPACE AIRCRAFT, COMPONENT, FOR EXAMPLE, FOR AIR OR SPACE AIRCRAFT AND AIRCRAFT

机译:用于增强组件的中央结构的基础或结构的方法和设备,例如,用于空中或空间飞机的组件,例如用于空中或空间飞机和飞机的组件的组件

摘要

1. A method of hardening a base or textile of a central structure (2) of a component, for example, an air or spacecraft, comprising the following steps: (i) feeding a continuous semi-finished product (6) by a feeding means (12) into a cylindrical container (17) of a conveying means (15) ), which includes several cylindrical containers (17); (ii) cutting along the length of the continuous semi-finished product (6) using cutting means (13) to obtain a segment of the reinforcing semi-finished product (7), which enters the cylindrical container (17); (iii ) t attaching the cylindrical container (17) to the processing means (14); (iv) sharpening a segment of the reinforcing semi-finished product (7) using the processing means (14); (v) transporting the cylindrical container (17) to the base or textile to strengthen the central structure (2) ) and (vi) firing a pointed semi-finished product (7) into the warp or textile of the central structure (2) using a means for firing the rods (16) .2. A method of hardening a base or textile of a central structure (2) of a component, for example, an air or spacecraft, comprising the following steps: (i ') feeding a continuous semi-finished product (6) by a feeding means (12) into a cylindrical container (17) of a conveying means (15) , which includes several cylindrical containers (17); (ii ') sharpening the free end of the continuous semi-finished product (7) using processing means (14); (iii') cutting along the length of the pointed continuous semi-finished product (6) using a cutting medium CTBA (13) to receive segment reinforcing semifinished product (7) which enters into the cylindrical container (17); (iv ') t
机译:1.一种硬化部件(例如,航空器或航天器)的中央结构(2)的基底或织物的方法,该方法包括以下步骤:(i)通过进料来喂入连续的半成品(6)装置(12)放入输送装置(15)的圆柱形容器(17)中,该输送装置包括几个圆柱形容器(17); (ii)使用切割装置(13)沿着连续的半成品(6)的长度切割,以获得增强的半成品(7)的一部分,其进入圆柱形容器(17); (iii)将圆柱形容器(17)附接到处理装置(14)上; (iv)使用加工装置(14)将增强半成品(7)的一部分磨锐; (v)将圆柱形容器(17)运输到底部或织物以增强中央结构(2)),并且(vi)将尖的半成品(7)烧成中央结构(2)的经线或织物使用击发杆(16)的装置.2。一种使部件例如飞机或航天器的中央结构(2)的基底或织物硬化的方法,该方法包括以下步骤:(i′)通过进给装置进给连续的半成品(6) (12)装入输送装置(15)的圆柱形容器(17),该输送装置包括几个圆柱形容器(17); (ii′)使用加工装置(14)使连续的半成品(7)的自由端变尖; (iii')使用切削介质CTBA(13)沿着尖的连续半成品(6)的长度进行切割,以接收进入圆柱形容器(17)的分段增强半成品(7); (iv')t

著录项

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