首页> 外国专利> Formation sheet metal blade helicopter e.g. - involves stretching blank whilst applying to mandrel with final reduced edge radii obtained by folding

Formation sheet metal blade helicopter e.g. - involves stretching blank whilst applying to mandrel with final reduced edge radii obtained by folding

机译:钣金叶片直升机-涉及拉伸毛坯,同时将其施加到心轴上,并通过折叠获得最终减小的边缘半径

摘要

The process may be used to form blades for wind-generators or helicopters from sheet metal. It involves subjecting a blank (17) to a transverse drawing operation whilst applying it to a mandrel (22) forming a central curved leading edge. The radius (r') of the mandrel is greater than that finally required. The angle of the mandrel opening may also exceed that of the finished work in respect of both the leading and trailing edges, the mandrel also having significant extra length (L'). The trailing edge may have a face (26) normal to the longitudinal axis (P').
机译:该工艺可用于由金属板形成用于风力发电机或直升机的叶片。它涉及对坯件(17)进行横向拉伸操作,同时将其施加到形成中心弯曲前缘的心轴(22)上。心轴的半径(r')大于最终需要的半径。就前缘和后缘而言,心轴开口的角度也可以超过完成的工件的角度,心轴还具有明显的额外长度(L')。后缘可具有垂直于纵轴(P')的面(26)。

著录项

  • 公开/公告号FR2508826A1

    专利类型

  • 公开/公告日1983-01-07

    原文格式PDF

  • 申请/专利权人 LAMBOLEY GILBERT;

    申请/专利号FR19810013250

  • 发明设计人

    申请日1981-07-06

  • 分类号B21D53/78;

  • 国家 FR

  • 入库时间 2022-08-22 10:00:48

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