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Principle of construction and method for the construction of small - aircraft

机译:小型飞机的构造原理和构造方法

摘要

The present invention relates to a principle of construction and method for the construction of small air vehicles which are constructed in a modular fashion from individual components and an efficient and cost-effective production of the components and a simple construction of aircraft with the flight principles surfaces of aircraft, a screwdriver, trike and para trike enable. They are constructed from:a uniform, shaped base body (1) in a closed, a stable lightweight construction with only functionally related openings, comprising seats, the dashboard, the elements of the control and base elements of the electrical / electronic system, as a rear end of a partition wall (26) between the elevator car and an engine compartment is accessible from the outside, as well as a plurality of flanges (17, 18, 21) for receiving the necessary components, wherein a flange also a plurality of components can be latched to the covers (15, 19) of flanges for in the case of small - aircraft certain flight principles not necessary components;at the partition wall (26) is arranged from the outside of the motor with or without a gear (24), tanks, parts of the control and parts of the electrical / electronic system;according to the same principles individual components, which is designed for small - aircraft of all flight principles are required (2, 3, 4, 9, 10) andaccording to the same principles individual components, which is designed for small - aircraft of one or more of the flight principles are not necessary to.The further individual components are:Nose wheel cover (2), engine hood upper part (3) or ..
机译:小型航空器的构造原理和方法技术领域本发明涉及小型航空器的构造原理和方法,所述小型航空器以模块化的方式由各个部件构成,并且部件的有效和成本效益高的制造,以及具有飞行原理面的飞机的简单结构飞机,螺丝起子,三轮车和三轮车启用。它们由以下部件构成:均匀,成形的基体(1),呈封闭,稳定,轻巧的结构,仅具有功能相关的开口,包括座椅,仪表板,控制元件和电气/电子系统的基本元件,例如:电梯轿厢和发动机室之间的分隔壁(26)的后端以及用于接收必要部件的多个凸缘(17、18、21)可从外部进入,其中,凸缘还包括多个对于小型飞机,某些组件可以锁定在法兰盖(15、19)上,某些飞行原理不是必需的组件;在分隔壁(26)上,从电动机的外侧布置有无齿轮(24),油箱,控制部件和电气/电子系统部件;根据相同的原则,为小型飞机设计的单个组件-需要所有飞行原理的飞机(2、3、4、9、10 ),并根据相同的原理单个部件不是必需的,它是为一种或多种飞行原理的小型飞机而设计的。其他单独的部件为:前轮罩(2),发动机罩上部(3)或。

著录项

  • 公开/公告号DE102008044461A1

    专利类型

  • 公开/公告日2010-03-18

    原文格式PDF

  • 申请/专利权人

    申请/专利号DE20081044461

  • 发明设计人

    申请日2008-08-25

  • 分类号B64C1/00;B64C39/00;

  • 国家 DE

  • 入库时间 2022-08-21 18:28:45

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