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DETAILABLE/SUCCESSFUL FLIGHT TRANSLATES

机译:详情/成功的航班翻译

摘要

A retractable airfoil assembly (20) augments the wing surface area (28) of an aircraft (22) enabling it to fly without stalling at reduced speeds during takeoff and landing. The airfoil assembly includes flexible sails (42, 44) and a furling mast (24) for extending and retracting the sails. The furling mast includes a furling drum mounted for clockwise and counterclockwise rotation on a static tube (50). The flexible sail assembly also includes guide tracks (80) located along a leading edge (101) or tailing edge (40) of the wings. The tracks guide the flexible sails during extension and retraction. A drive cable (26) extends and retracts the sails (42, 44) along the guide tracks and maintains tension in the sails while they are extended.
机译:可伸缩翼型组件(20)增加了飞机(22)的机翼表面积(28),使其能够在起飞和降落期间以降低的速度飞行而不会失速。翼型组件包括柔性帆(42、44)和用于伸展和缩回帆的收帆桅杆(24)。收卷桅杆包括收卷鼓,该收卷鼓安装成可在静态管(50)上顺时针和逆时针旋转。柔性帆组件还包括沿着机翼的前缘(101)或尾缘(40)定位的导轨(80)。轨道在伸展和缩回期间引导柔性帆。驱动缆线(26)沿着导轨使帆(42、44)延伸和缩回,并在帆伸展时保持帆中的张力。

著录项

  • 公开/公告号DE69830717D1

    专利类型

  • 公开/公告日2005-08-04

    原文格式PDF

  • 申请/专利权人 WAGNER FRED A.;

    申请/专利号DE19986030717T

  • 发明设计人 WAGNER III;

    申请日1998-04-08

  • 分类号B64C3/54;

  • 国家 DE

  • 入库时间 2022-08-21 21:58:52

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