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System for making reinforced by carbon fibers and process for the manufacture, for aeronautical applications structures.

机译:用碳纤维增强的制造系统和制造工艺,用于航空应用结构。

摘要

PRESENTED EQUIPMENT AND A METHOD FOR THE MANUFACTURE OF STRUCTURES Monolithic integrals, ADOPTING LAYER FIBER reinforcing impregnated with thermoset resin, consisting of: the computer base (4), which determines the shape of the structure, the cover (8) such equipment; Two lateral supports (6) enclosed in an outer bag (16) made of nylon or similar subject and TANTOS support elements (7) as are required; BREATHING EQUIPMENT (17); A SHEET OF A FILM (18); FILLER SEALER (15); VALVES application of vacuum (14); A TUBULAR FILM (10); TUBULAR BAG (11). The invention SIMPLIFIES manufacturing, particularly important in the field of aviation where there is the need for standards VERY LOW WEIGHT, HIGH EFFICIENCY AND HIGH QUALITY STRUCTURAL PROCESS.
机译:提出的设备和结构的制造方法单片整体,用热固性树脂浸渍的适配层纤维增强件,包括:确定结构形状的计算机基座(4),这种设备的盖子(8);需要两个装在尼龙或类似物体制成的外袋(16)中的侧向支撑件(6)和TANTOS支撑件(7);呼吸设备(17);电影胶片(18);填料密封器(15);真空阀的应用(14)​​;管状薄膜(10);管状袋(11)。本发明简化了制造,这在需要非常低重量,高效率和高质量结构过程的标准的航空领域中尤其重要。

著录项

  • 公开/公告号ES2132155T3

    专利类型

  • 公开/公告日1999-08-16

    原文格式PDF

  • 申请/专利权人 FINMECCANICA S.P.A.;

    申请/专利号ES19930111893T

  • 发明设计人 INSERRA IMPARATO SABATO;

    申请日1993-07-24

  • 分类号B29D24/00;B29C43/36;

  • 国家 ES

  • 入库时间 2022-08-22 02:24:25

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