首页> 外国专利> Inflatable ultra light glider, has inflatable tubes reinforced by semi-rigid slats and joined for forming flapping wings, where flapping of wing is obtained by elastic deformation of structure of wing

Inflatable ultra light glider, has inflatable tubes reinforced by semi-rigid slats and joined for forming flapping wings, where flapping of wing is obtained by elastic deformation of structure of wing

机译:充气式超轻滑翔机,具有由半刚性板条增强并连接以形成扑翼的充气管,其中,扑翼是通过机翼结构的弹性变形获得的

摘要

The glider has flapping wings formed by joining inflatable tubes (1). The inflatable tubes are parallel to each other and reinforced by semi-rigid slats (2), where the slats are made of carbon or glass fiber. The diameter of the tube is 40 cm. The flapping of the wing is obtained by elastic deformation of a structure of the wing. The deformation is opposed by traction exerted on an oscillating lever arm system (3).
机译:滑翔机具有通过连接充气管(1)形成的拍打翼。充气管彼此平行,并由半刚性板条(2)加固,其中板条由碳纤维或玻璃纤维制成。管的直径为40厘米。机翼的拍打是通过机翼结构的弹性变形获得的。该变形通过施加在摆动杠杆臂系统(3)上的牵引力来抵消。

著录项

  • 公开/公告号FR2935681A1

    专利类型

  • 公开/公告日2010-03-12

    原文格式PDF

  • 申请/专利权人 ROQUES CHRISTOPHE;

    申请/专利号FR20080004990

  • 发明设计人 ROQUES CHRISTOPHE;

    申请日2008-09-11

  • 分类号B64C33/02;B64C3;B64C31/032;

  • 国家 FR

  • 入库时间 2022-08-21 18:26:42

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