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Wind tunnel balance and system with wings model and wind tunnel balance

机译:带有机翼模型的风洞平衡和系统以及风洞平衡

摘要

The present invention relates to a wind tunnel balance, with a channel wall of an adapter, which is designed for this purpose, the wind tunnel balance to a wall of a wind tunnel, to attach a actuators housing, which is connected to the channel wall adapter is connected, a plurality of force sensors, which between the actuators housing and the channel wall adapter are arranged, and which are designed for forces acting on the actuators housing, to be detected, a a swivel joint, via which a supporting surfaces model of an aircraft is pivotably coupled to the actuators, and a plurality of piezoelectric actuators, which are arranged in the actuators housing, and which are designed for a swivel joint mounted on the supporting surfaces model can be controlled in three spatial directions to deflect.
机译:风洞天平技术领域本发明涉及一种风洞天平,其具有为此目的而设计的适配器的通道壁,该风洞天平连接至风洞的壁,以安装致动器壳体,该致动器壳体连接至该通道壁。连接到适配器上,在执行机构壳体和通道壁适配器之间布置有多个力传感器,这些力传感器被设计成通过旋转接头检测作用在执行机构壳体上的力,通过该关节,传感器的支撑表面模型得以实现。飞机可枢转地连接到致动器,并且可以在三个空间方向上控制多个压电致动器,该压电致动器布置在致动器壳体中并且设计用于安装在支撑表面模型上的旋转接头。

著录项

  • 公开/公告号DE102013213675A1

    专利类型

  • 公开/公告日2015-01-15

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号DE201310213675

  • 发明设计人 MICHAEL KORDT;

    申请日2013-07-12

  • 分类号G01M9/06;G01M9/08;

  • 国家 DE

  • 入库时间 2022-08-21 14:55:31

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