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Glider with a variable lift-to-drag ratio

机译:升降阻力比可变的滑翔机

摘要

1. A gliding flight apparatus with variable glide factor formed from individual profiles (1, 2, 3) arranged one behind the other in the main flight direction and directly associated one with another in the sense of a multiple slotted wing, between which profiles are provided openings (wing slots) actuatable by the jumper through a rigging system for the purpose of changing the air currents, characterized in that the parts of the individual profiles (1, 2, 3) situated in the front region can be pulled downward by means or an actuating line (19) belonging to the rigging system, in the sense of an enlargement of the curvature the actuating line (19) being constructed as a loop whose front part (front line 9) is provided for pulling down the profile front parts and whose rear part (tail line 9) for pulling down the profile rear parts and closing the wing slots.
机译:1.一种具有可变滑移因子的滑行飞行装置,其由各个轮廓(1、2、3)形成,这些轮廓在主飞行方向上一个接一个地排列,并且在多个开缝机翼的意义上彼此直接相关,在它们之间分布有多个轮廓提供的开口(机翼槽)可通过跨接系统通过跳线操纵,以改变气流,其特征在于,位于前部区域的各个型材(1、2、3)的部分可通过以下方式拉低或属于索具系统的操纵线(19),在曲率增大的意义上,操纵线(19)构造成环,其前部(前线9)用于拉下型材前部其后部(尾线9)用于拉下型材后部并关闭机翼插槽。

著录项

  • 公开/公告号EP0109448A1

    专利类型

  • 公开/公告日1984-05-30

    原文格式PDF

  • 申请/专利权人 KIEF HORST DR. MED.;

    申请/专利号EP19820105648

  • 发明设计人 KIEF HORST DR. MED.;

    申请日1982-08-03

  • 分类号B64C31/02;B64D17/00;

  • 国家 EP

  • 入库时间 2022-08-22 08:58:06

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