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Smart Aerodynamic Surface for a Typical Military Aircraft Using Shape Memory Elements

机译:使用形状记忆元件的典型军用飞机的智能空气动力学表面

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摘要

This work pertains to the development effort involved in the deployment of an additional winglike aerodynamic surface referred to as a "mousche" for the naval version of a typical military aircraft. The mousche is attached to the forebody of the naval aircraft. It is deployed only during landing (and retracted at all other times) in order to improve the landing characteristics of the aircraft on the aircraft carrier. The mousche is designed and constructed out of carbon-fiber-reinforced plastic to withstand the full load and is deployed using the actuator bank containing the arrays of shape memory alloy elements. The shape memory alloy actuator bank moves a distance of 15 mm while generating a net actuator force of over 2000 kg. This force is used to deploy the additional aerodynamic surface measuring 790 x 215 x 32 mm against a simulated lift and drag load acting simultaneously, i.e., a resultant lift load of 331.6 kg and a drag load of 33.16 kg acting at the center of gravity of the mousche. The shape memory alloy bank consists of 138 wires of about 1 mm in diameter and 650 mm in length. The actuation of these 138 wires is electronically and mechanically synchronized. The mousche has been analyzed using finite element method codes for the combined lift and drag load. Experimental and analysis values have matched well. The electronics circuit assembly of the smart actuator drive electronics that powers the shape memory alloy actuator bank has been designed and developed in the form of mother- and daughterboards. Each daughterboard has six miniaturized dc-dc converters, and the required power and control signals are routed to the motherboard. The smart actuator drive electronics have been integrated to carry out the full load test. The National Instruments 6009 data acquisition module along with graphical user interface software Lab VIEW are used to conduct the experiments and to effect the closed-loop position control of the mousche.
机译:这项工作涉及为典型的军用飞机的海军型部署附加的翼状空气动力学表面(称为“慕斯”)所涉及的开发工作。麝香被附接到海军飞机的前身。它仅在着陆时才部署(在所有其他时间都缩回),以改善飞机在航空母舰上的着陆特性。慕斯由碳纤维增强塑料设计和制造,可承受全部载荷,并使用包含形状记忆合金元素阵列的执行器组进行部署。形状记忆合金致动器排移动15 mm的距离,同时产生超过2000 kg的净致动器力。该力用于抵抗同时作用的模拟升力和阻力载荷,即790 x 215 x 32 mm的附加空气动力学表面,即,产生的331.6 kg升力载荷和33.16 kg的阻力载荷作用于重心。慕斯。形状记忆合金库由138条直径约1毫米,长度650毫米的金属丝组成。这138条线的驱动是电子和机械同步的。已经使用有限元方法代码分析了混合起重和阻力载荷的乳胶。实验和分析值非常吻合。为形状记忆合金致动器组提供动力的智能致动器驱动电子设备的电子电路组件已经以母板和子板的形式设计和开发。每个子板都有六个微型DC-DC转换器,所需的电源和控制信号被路由到母板上。集成了智能执行器驱动电子设备以执行满负荷测试。 National Instruments 6009数据采集模块与图形用户界面软件Lab VIEW一起用于进行实验并实现对乳胶圈的闭环位置控制。

著录项

  • 来源
    《Journal of Aircraft》 |2011年第6期|p.1968-1977|共10页
  • 作者单位

    Council of Scientific and Industrial Research, National Aerospace Laboratories, Bangalore 560 017, India;

    Council of Scientific and Industrial Research, National Aerospace Laboratories, Bangalore 560 017, India;

    Council of Scientific and Industrial Research, National Aerospace Laboratories, Bangalore 560 017, India;

    Council of Scientific and Industrial Research, National Aerospace Laboratories, Bangalore 560 017, India;

    Council of Scientific and Industrial Research, National Aerospace Laboratories, Bangalore 560 017, India;

    Council of Scientific and Industrial Research, National Aerospace Laboratories, Bangalore 560 017, India;

    Council of Scientific and Industrial Research, National Aerospace Laboratories, Bangalore 560 017, India;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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