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首页> 外文期刊>Journal of aerospace engineering >Performance Optimization of Forward-Flight and Lift-Up Phases in a Cycloidal Rotor Using an Active Control Mechanism
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Performance Optimization of Forward-Flight and Lift-Up Phases in a Cycloidal Rotor Using an Active Control Mechanism

机译:使用主动控制机制在摆线转子中的正向和升降阶段的性能优化

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摘要

Cycloidal rotors have revealed a noticeable potential to be further enhanced when running at different operating conditions. The present work demonstrates the active control methodology in order to achieve improved performances in cycloidal rotors operating in forward-flight and lift-up phases. The proposed optimization analysis comprises computational fluid dynamics (CFD) simulations for the numerical database and an artificial neural network (ANN) to propose optimum operating states in each of the mentioned flying phases instead of the hover state under ground effects. CFD predictions were conducted for various operating conditions of pitching oscillations and rotating speeds at each forward or lift-up speed. By training the ANN algorithm using the database attained from CFD simulations, the optimization process was further surveyed for each corresponding flying mode. The targeting concept is to operate with an active mode of employing pitching angles rather than using constant oscillations at all rotation speeds. The ANN approach effectively proposed an optimized pitching schedule for both forward and lift-up phases after analyzing a wide range of parameters in order to reach an optimum aerodynamic efficiency. Because the blade and flow properties are all considered at each specific point on the continuous azimuth of the circular (360 degrees) trajectory, the mutual collaboration of CFD and ANN analysis showed to be advantageous for enhanced operations. (C) 2021 American Society of Civil Engineers.
机译:在不同的操作条件下运行时,摆线转子揭示了在运行时进一步增强的明显电位。目前的作品展示了主动控制方法,以实现在正飞行和提升阶段操作的摆线转子中的改进性能。所提出的优化分析包括用于数值数据库的计算流体动力学(CFD)模拟和人工神经网络(ANN),以在接地效果下提出每个提到的飞行阶段而不是悬停状态的最佳操作状态。对各种俯仰振荡的各种操作条件进行CFD预测,并以各个向上或升降速度旋转速度。通过使用从CFD仿真实现的数据库训练ANN算法,为每个相应的飞行模式进行了进一步调查优化过程。靶向概念是用采用俯仰角的活动模式操作,而不是在所有旋转速度下使用恒定振荡。在分析广泛的参数之后,ANN方法有效地提出了前向和提升相的优化节目时间表,以达到最佳的空气动力学效率。因为叶片和流动性质全部考虑圆形(360度)轨迹的连续方位角上的每个特定点,所以CFD和ANN分析的相互协作显示出于增强的操作是有利的。 (c)2021年美国土木工程师协会。

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  • 来源
    《Journal of aerospace engineering》 |2021年第4期|04021039.1-04021039.18|共18页
  • 作者单位

    Univ Beira Interior Ctr Mech & Aerosp Sci & Technol P-3000011 Covilha Portugal;

    Univ Beira Interior Ctr Mech & Aerosp Sci & Technol Aggregat P-3000011 Covilha Portugal;

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