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飞机噪声计算通用模型研究
引用本文:刘 洲 蔡良才 方 华 邵 斌 杜宜霖 孙 捷. 飞机噪声计算通用模型研究[J]. 振动与冲击, 2012, 31(17): 124-128. DOI:  
作者姓名:刘 洲 蔡良才 方 华 邵 斌 杜宜霖 孙 捷
作者单位:1.空军工程大学工程学院 机场建筑工程系,陕西 西安 710038;2.环境保护部环境工程评估中心,北京 100012
摘    要:
为完善和规范现行的飞机噪声计算方法,根据飞行航线的几何特点,基于“直线段”和“曲线段”这两个基本的航线元素提出了航线分解的思想,阐述了其基本原理,建立了系统的飞机噪声计算通用模型,并实例验证了该模型的可行性和实用性。该模型解决了实际噪声环境影响评价工作中的相关技术问题,规范了噪声计算方法,使整个评价工作更直观、更智能、更科学。

关 键 词:飞机噪声   计算模型   航线分解   有效感觉噪声级(LEPN) 
收稿时间:2011-05-26
修稿时间:2011-10-12

A general model for aircraft noise calculation
LIU Zhou,CAI Liang-cai,FANG Hua,SHAO Bin,DU Yi-lin,SUN Jie. A general model for aircraft noise calculation[J]. Journal of Vibration and Shock, 2012, 31(17): 124-128. DOI:  
Authors:LIU Zhou  CAI Liang-cai  FANG Hua  SHAO Bin  DU Yi-lin  SUN Jie
Affiliation:1. Airfield Construction Engineering Department, Engineering College,Air Force Engineering University, Xi’an 710038, P.R.China 2. Environment Engineering Evaluation Center, Environment Protection Department, Beijing, 100012
Abstract:
In order to perfect and standardize the current aircraft noise calculation method.Here,the basic theory for disassembling a flight path based on geometrical elements of beeline segment and curve one was presented,a systematic and general aircraft noise calculation model was built.An example was used to prove the feasibility and practicability of the model.With the proposed model,some technical problems in actual estimation of aircraft noise were solved,the calculation method was standardized and the whole assessing process became more intuitive,intelligent and scientific.
Keywords:aircraft noise  calculation model  disassembling a flight path  effective perceived noise level
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