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ACTIVE CONTROL OF TRANSMISSION NOISE IN A BELL 407 HELICOPTER

机译:贝尔407直升机的传输噪声主动控制。

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Cabin noise is a major source of discomfort for helicopter passengers. One of the main sources of noise is the main rotor drive and gearbox assembly, whose structural vibrations are primarily transmitted through supporting struts and mounts to the airframe, which then radiates sound into the cabin. The vibration and resulting noise occur mainly at discrete gear meshing frequencies in the frequency range kHz. The objective of this work was to establish the feasibility of an active control system to reduce multi-harmonic transmission noise in helicopter cabins. The system development, implementation and testing were conducted on a Bell 407 aircraft.
机译:机舱噪音是直升机乘客不舒服的主要原因。噪声的主要来源之一是主旋翼驱动器和变速箱组件,其结构振动主要通过支撑杆传递并安装到机身,然后将声音辐射到机舱中。振动和产生的噪声主要发生在频率范围为kHz的离散齿轮啮合频率处。这项工作的目的是确定一种主动控制系统的可行性,以减少直升机机舱内的多谐波传输噪声。系统开发,实施和测试是在Bell 407飞机上进行的。

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