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A Novel Smart Spring Concept For Helicopter Blade Vibration And Noise Suppression

机译:直升机叶片振动和噪声抑制的新型智能弹簧概念

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This paper demonstrates the ability of the Smart Spring to suppress helicopter blade vibration through numerical simulation and experimental investigation. Mechanical shaker tests on a Bell-212 helicopter blade section verified the impedance control properties and the ability to suppress blade vibration using the Smart Spring proof-of-concept hardware. More importantly, the tests conducted in a wind tunnel proved the performance of the Smart Spring under highly varying unsteady excitation conditions. These tests confirmed that the Smart Spring system is able to actively suppress helicopter vibration through adaptive control of blade impedance properties.
机译:本文通过数值模拟和实验研究证明了智能弹簧抑制直升机叶片振动的能力。在Bell-212直升机桨叶部分进行的机械振动试验证明了使用Smart Spring概念验证硬件的阻抗控制特性和抑制桨叶振动的能力。更重要的是,在风洞中进行的测试证明了Smart Spring在变化很大的不稳定激励条件下的性能。这些测试证实,智能弹簧系统能够通过对叶片阻抗特性的自适应控制来主动抑制直升机的振动。

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