飞机舱室主观舒适性声振耦合机理与模型研究
批准号:
52072242
项目类别:
面上项目
资助金额:
58.0 万元
负责人:
黄煜
依托单位:
学科分类:
运载系统智能化
结题年份:
2024
批准年份:
2020
项目状态:
已结题
项目参与者:
黄煜
中文摘要
面向我国大型客机舱室人因工程、噪声振动设计的需求,针对飞机舱室噪声和振动舒适性评价的技术瓶颈,研究大型客机舱室噪声和振动对舒适性的耦合效应机理及模型。通过实航测试,获取大型客机典型工况、典型舱段及典型剖面的噪声和振动实测数据。分析数据的时频特性,并根据人耳听觉和人体振动感知特性,研究虚拟样本的合成方法,扩展飞机舱室噪声振动的实验样本空间。研究样本精细化统一度量方法,发展适用于大型客机舱内噪声和振动特性的主观评价实验技术。通过主观评价实验,研究大型客机舱室噪声和振动对舒适性的影响规律,揭示噪声和振动对舒适性的耦合效应机理,最终建立主客观融合的大型客机舱室声振复合不舒适度评价模型,并通过验证实验分析该模型的准确性、鲁棒性和适用范围。研究成果将为我国大型客机舱室的降噪减振设计,以及适航标准中噪声和振动舒适性相关内容的制定,提供理论基础与技术支撑。
英文摘要
The human factors engineering, and noise and vibration designs are in great demands in the large passenger aircraft cabin in China. To overcome the technical bottleneck of the comfort evaluation of aircraft cabin noise and vibration, we will study the mechanism and model of coupling effects of noise and vibration on the comfort of large passenger aircraft cabins. Field measurements will obtain the noise and vibration data of typical operating conditions, cabins and sections of large passenger aircraft. The time-frequency characteristics of the data will be analyzed, and the synthetic method of virtual samples will be studied by considering the aspects of auditory hearing and vibration perception. A subjective evaluation experimental technique for noise and vibration in large passenger aircraft cabins will be developed by using the sample synthesis method and the elegant and unified metric method. The effects of noise and vibration on the comfort of large passenger aircraft cabins will be studied through subjective evaluation experiments. The mechanism of coupling effects of noise and vibration on comfort will be revealed. Finally, we will establish the total discomfort model of combined noise and vibration for the large passenger aircraft cabins from the subjective and objective integration. We will also analyze the accuracy, robustness, and applicability of the model through the verification experiment. The research will provide theoretical and technical support for the design of noise and vibration control in the cabin of large passenger aircraft in China, and formulate regulations of noise and vibration comfort in airworthiness standards.
面向我国大型客机舱室人因工程、噪声振动设计的需求,针对飞机舱室噪声和振动舒适性评价的技术瓶颈,研究了大型客机舱室噪声和振动对舒适性的耦合效应机理及模型。通过实航测试,获取了大型客机典型工况、典型舱段及典型剖面的噪声和振动实测数据。分析了数据的时频特性,并根据人耳听觉和人体振动感知特性,研究了虚拟样本的合成方法,扩展了飞机舱室噪声振动的实验样本空间。研究了样本精细化统一度量方法,发展了适用于大型客机舱内噪声和振动特性的主观评价实验技术。通过主观评价实验,研究了大型客机舱室噪声和振动对舒适性的影响规律,揭示了噪声和振动对舒适性的耦合效应机理,最终建立了主客观融合的大型客机舱室声振复合不舒适度评价模型,并通过验证实验分析了该模型的准确性、鲁棒性和适用范围。研究成果为我国大型客机舱室的降噪减振设计,以及适航标准中噪声和振动舒适性相关内容的制定,提供了理论基础与技术支撑。
正面情绪的声波调控机理和技术研究
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批准号:19ZR1424500
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项目类别:省市级项目
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资助金额:0.0万元
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批准年份:2019
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负责人:黄煜
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依托单位:
中高频垂直振动环境下正坐人体的舒适度和生物动力响应研究
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批准号:11402147
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项目类别:青年科学基金项目
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资助金额:30.0万元
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批准年份:2014
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负责人:黄煜
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依托单位:
国内基金
海外基金