首页> 外国专利> High lift wing flaps for aeroplane wings - can be swung from body stored position to leading and trailing edges

High lift wing flaps for aeroplane wings - can be swung from body stored position to leading and trailing edges

机译:飞机机翼的高升力机翼襟翼-可从机身存放位置摆动到前缘和后缘

摘要

The wing flaps are normally stored flush with the aircraft fuselage. Sliding links at one end of the flaps engage with slots which are parallel to the wing edges. Sliding links mounted at the other end of the flaps engage with slots parallel to the side of the fuselage. When one end of the flaps is moved outward towards the wing tip, the other end will be brought nearer to the wing edge. Alternatively, the flaps can be swung from their position flush with the fuselage, about a hinge point to the wind edges or the flaps can consist of sections which extend telescopically. The arrangement allows the use of optimal flap area for landing and take-off or for normal flight.
机译:机翼襟翼通常与飞机机身齐平存放。襟翼一端的滑杆与平行于机翼边缘的狭槽接合。安装在襟翼另一端的滑动连杆与平行于机身侧面的插槽接合。当襟翼的一端朝机翼末端向外移动时,另一端将靠近机翼边缘。替代地,襟翼可以从其与机身齐平的位置围绕铰链点摆动到风边缘,或者襟翼可以由可伸缩地延伸的部分组成。该布置允许将最佳襟翼区域用于着陆和起飞或正常飞行。

著录项

  • 公开/公告号DE2353245A1

    专利类型

  • 公开/公告日1975-04-30

    原文格式PDF

  • 申请/专利权人 DORNIER GMBH;

    申请/专利号DE19732353245

  • 发明设计人 OBERDOERFFERELMARDIPL.-ING.;

    申请日1973-10-24

  • 分类号B64C3/50;

  • 国家 DE

  • 入库时间 2022-08-23 03:57:25

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