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Structure of the wing of model airplane for scholarship

机译:奖学金飞机模型的机翼结构

摘要

The present invention relates to a wing structure of a training model airplane in which the second upper half angle of the front wing of the training model airplane is not deformed by external force, and is provided with a front wing support for supporting the front wing by tying a rubber band on the upper surface of the model airplane body, and the front wing. In the structure of the wing blades of the training model aircraft having a plurality of direct barrels assembled on both sides of the support via a first aluminum tube and a U-shaped blade connected to the end of the straight bar, the U-shaped blades ( 7) the U-shaped blade having a connecting member (7a) formed with a fitting groove (7b) is fitted between the U-shaped blade (7) and the straight shoulder (4) between the U-shaped blade (7) It is manufactured by molding integrally with (7), characterized in that the connecting member (7a) and the U-shaped blade (7) forms a secondary upper half angle (β). The present invention eliminates the hassle of having to accurately form the secondary upper half angle β.
机译:训练飞机的机翼结构技术领域本发明涉及一种训练飞机的机翼结构,其中训练飞机的前机翼的第二上半角不因外力而变形,并且设有用于通过以下方式支撑前机翼的前机翼支撑件。将橡皮筋绑在飞机模型机身的前表面和前机翼上。在训练模型飞机的机翼叶片的结构中,具有多个直接枪管,这些直接枪管通过第一铝管和连接到直杆端部的U形叶片组装在支架的两侧,U形叶片(7)在U形刀片(7)与U形刀片(7)之间的直肩(4)之间嵌合有具有形成有嵌合槽(7b)的连接部件(7a)的U形刀片。它是通过与(7)一体成型而制造的,其特征在于,连接构件(7a)和U形刀片(7)形成第二上半角(β)。本发明消除了必须精确地形成副上半角β的麻烦。

著录项

  • 公开/公告号KR200441151Y1

    专利类型

  • 公开/公告日2008-07-29

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20070005598U

  • 发明设计人 이훈상;

    申请日2007-04-05

  • 分类号A63H27/18;

  • 国家 KR

  • 入库时间 2022-08-21 19:51:24

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