首页> 外国专利> Wing tip or propeller blade tip attachment comprises hollow cylinder with chamfered end and spiral slit to reduce drag

Wing tip or propeller blade tip attachment comprises hollow cylinder with chamfered end and spiral slit to reduce drag

机译:机翼末梢或螺旋桨叶片末梢附件包括带有倒角端的中空圆柱体和螺旋形狭缝,以减少阻力

摘要

The attachment for the tip of a wing or propeller blade is in the shape of a goose quill, with a chamfered forward end making a leading edge (1) and an oval opening on a cylindrical cavity with a spiral slit. The slit can be divided into a number of sections, and the attachment, which is made from aluminium alloy or titanium for aircraft use, can be fitted with a de-icing system. The attachment can be fixed or pivoted to the wing or propeller blade tip.
机译:机翼或螺旋桨叶片尖端的附件为鹅毛笔形状,其斜切的前端形成前缘(1),并在带有螺旋形狭缝的圆柱形空腔上形成椭圆形的开口。缝隙可分为多个部分,飞机用铝合金或钛制成的附件可装有除冰系统。附件可以固定或枢转至机翼或螺旋桨叶片的尖端。

著录项

  • 公开/公告号FR2823541A1

    专利类型

  • 公开/公告日2002-10-18

    原文格式PDF

  • 申请/专利权人 HUGUES CHRISTIAN;

    申请/专利号FR20010004998

  • 发明设计人 HUGUES CHRISTIAN;

    申请日2001-04-11

  • 分类号F15D1/10;B64C23/00;B64C3/10;

  • 国家 FR

  • 入库时间 2022-08-22 00:24:07

相似文献

  • 专利
  • 外文文献
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