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The Potential For Aircraft Noise Reduction Through Active Suppression From A Ground-based System

机译:通过主动抑制地面系统降低飞机噪声的潜力

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The feasibility of devising ground-based active noise suppression systems for aircraft which are on the ground and in the air is considered. Detailed numerical calculations are given for various geometries involving an aircraft, sound cancelling sources, reference microphones as well as correction microphones. The calculations are for broadband noise based on a frequency spectrum typical of a jet aircraft. For an aircraft on the ground (during engine run-up and during takeoff from a runway), calculations indicate that noise suppression is both feasible and practical. For an aircraft in the air, while noise suppression is feasible, it is not necessarily practical due to the fact that the most advantageous locations for the suppressing control sources are midway between the ground and the flight path. However, this may not preclude a limited application for very confined areas and for aircraft at relatively low altitudes. Published by Elsevier B.V. on behalf of IM ACS.
机译:考虑为地面和空中飞机设计基于地面的有源噪声抑制系统的可行性。给出了涉及飞机,消声源,参考麦克风以及修正麦克风的各种几何形状的详细数值计算。该计算是针对基于喷气飞机典型频谱的宽带噪声进行的。对于地面上的飞机(在发动机启动期间和从跑道起飞期间),计算表明,抑制噪声既可行又实用。对于空中的飞机,虽然抑制噪声是可行的,但由于抑制控制源最有利的位置是在地面与飞行路径之间的中间位置,因此不一定实用。但是,这可能不排除在非常狭窄的区域和相对低空的飞机上有有限的应用。由Elsevier B.V.代表IM ACS发布。

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