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Aircraft wing grid is for main wing of which blades are torsion and bending-proof and tensioned between two similarly formed plates

机译:飞机机翼格栅用于主翼,其叶片是抗扭和抗弯曲的,并且在两个相似形成的板之间张紧

摘要

The aircraft wing grid (1) is for a main wing (6) of which the blades (2) are torsion and bending-proof and tensioned between two similarly formed plates (3,4). The first plate formed as the end (3) or intermediate plate is held by at least one tractive brace (5) and at least one pressure brace. The second plate formed as a basic plate is connectable with the support structure of the main wing. At least one of the braces is integrated in one of the blades. The brace is formed diagonally for accommodation of the impelling forces of the blades. The braces not integrated in the blades are arranged either on the under side or on the upper side of the blades, as tractive or pressure units.
机译:飞机机翼格栅(1)用于主翼(6),其叶片(2)是抗扭和抗弯曲的,并且在两个类似形成的板(3,4)之间张紧。形成为端板(3)或中间板的第一板由至少一个牵引支架(5)和至少一个压力支架保持。形成为基础板的第二板可与主翼的支撑结构连接。至少一个支架集成在一个刀片中。支撑件倾斜地形成以适应叶片的推动力。未集成在叶片中的支架作为牵引或压力装置布置在叶片的下侧或上侧。

著录项

  • 公开/公告号CH693949A5

    专利类型

  • 公开/公告日2004-05-14

    原文格式PDF

  • 申请/专利权人 STENGELE IVO;

    申请/专利号CH19990001030

  • 发明设计人 STENGELE IVO;

    申请日1999-06-01

  • 分类号B64C23/06;B64C3/18;

  • 国家 CH

  • 入库时间 2022-08-21 22:43:49

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