首页> 外国专利> COMPOSITE MATERIAL BLADE WITH BILONGERON STRUCTURE AND BICYCLE, AND LAMINATED SANDWICH LAMINATED COATING, AND METHOD OF MANUFACTURING THE SAME

COMPOSITE MATERIAL BLADE WITH BILONGERON STRUCTURE AND BICYCLE, AND LAMINATED SANDWICH LAMINATED COATING, AND METHOD OF MANUFACTURING THE SAME

机译:具有Bilongeron结构和自行车的复合材料叶片,以及夹层的夹心层合涂层和制造相同材料的方法

摘要

P THE COMPOSITE MATERIAL BLADE WITH BILONGERON STRUCTURE 1, 2 AND BICYCLE 3, 4, AND WITH COATINGS 5, 6 SANDWICH LAMINATE OF HONEYCOMB 53, 54, 63, 64 ACCORDING TO THE INVENTION PRESENTS A FRONT LONGERON 1 C-SECTION ATTACHMENT BORDER, A CENTRAL LONGERON 2 WITH TWO INSOLES 22, 23 AT THE END OF A TRANSVERSE SHAFT 21 FILLED WITH 24 HOLDS FILLED IN SANDWICH BETWEEN LATERAL SHEETS 25, AND LAMINATED COATINGS 25 PANELS OF HONEYCOMB NAMES TAKEN IN SANDWICH BETWEEN EXTERNAL TABLES 51, 61 AND INTERNAL 52, 62 FORMED BY STACK OF FIBER TISSUE LAYERS, IN ORDER TO DELIMIT TWO CAISSONS 3, 4 FILLED WITH CORES 7, 8 OF VERY LIGHT FOAM . / P P INSOLES 22, 23 ARE INTEGRATED WITH COATINGS 5, 6 THAT ARE CONNECTED AT LEVEL OF LEAK EDGE BY A RIDER 9 WITH FOAM CORNER. / P P APPLICATION TO EQUIPMENT HELICOPTERS FOR MILITARY USE AND CIVIL HELICOPTERS WITH LARGE DIMENSIONAL BLADES. / P
机译:

根据本发明,具有Bilongeron结构1、2和自行车3、4,以及涂层5、6的夹层复合材料蜂窝板53、54、63、64的蜂窝状复合材料叶片呈现出LONLONON的前部1个C形截面附着边缘,带有两个鞋底22的中央LONGERON 2,位于横向轴21末端的23,在侧板25之间夹有24档填充物的夹层板,以及在25层夹层中分别由蜂窝板名称和外部表51夹在中间的表板52、62由纤维组织层的堆叠构成,以按顺序划分两个箱3、4,并填充有非常轻的泡沫的孔7、8。

22号,23号底漆与5号,6号涂料集成在一起,而5号,6号涂料的边缘由带泡沫角的RIDER 9连接。

应用于军事用途的直升机以及具有大尺寸叶片的民用直升机。

著录项

  • 公开/公告号FR2602739A1

    专利类型

  • 公开/公告日1988-02-19

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE;AEROSPATIALE STE NATIONALE INDLE;

    申请/专利号FR19860010882

  • 发明设计人 BOST MICHEL;MICHEL BOST;

    申请日1986-07-28

  • 分类号B64C3/18;B64C3/20;B64C3/24;B64C27/04;

  • 国家 FR

  • 入库时间 2022-08-22 06:51:03

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