振动与冲击
振動與遲擊
진동여충격
JOURNAL OF VIBRATION AND SHOCK
2014年
2期
152-157
,共6页
刘翠伟%李玉星%王武昌%谢祝祝
劉翠偉%李玉星%王武昌%謝祝祝
류취위%리옥성%왕무창%사축축
输气管道%音波法泄漏检测%气动噪声%联合仿真%瞬态流场%等效声源
輸氣管道%音波法洩漏檢測%氣動譟聲%聯閤倣真%瞬態流場%等效聲源
수기관도%음파법설루검측%기동조성%연합방진%순태류장%등효성원
gas pipeline%leak detection and location based on acoustic method%aero-acoustic noise%CFD and SYSNOISE simulation%transient flow field%equivalent sound source
为区分输气管道泄漏音波与阀门噪声,为输气管道音波法泄漏检测提供理论依据及数据库、控制阀门噪声提供解决办法,从音波产生机理角度采用CFD软件耦合专业声学软件方法对输气管道气体流经阀门产生的气动噪声进行研究,建立气动噪声模型,探究气动噪声产生机理及传播、衰减规律。在CFD(Computational Fluid Dynamics)软件中采用大涡湍流模型对气体流经阀门时的瞬态流场求解分析,获得流场分布如脉动压力、脉动速度数据;将CFD计算所得数据导入专业声学软件进行联合仿真,生成气动噪声源项,包括偶极子声源及四极子声源,建立气动噪声产生传播模型,求解输气管道气体流经阀门的气动噪声。
為區分輸氣管道洩漏音波與閥門譟聲,為輸氣管道音波法洩漏檢測提供理論依據及數據庫、控製閥門譟聲提供解決辦法,從音波產生機理角度採用CFD軟件耦閤專業聲學軟件方法對輸氣管道氣體流經閥門產生的氣動譟聲進行研究,建立氣動譟聲模型,探究氣動譟聲產生機理及傳播、衰減規律。在CFD(Computational Fluid Dynamics)軟件中採用大渦湍流模型對氣體流經閥門時的瞬態流場求解分析,穫得流場分佈如脈動壓力、脈動速度數據;將CFD計算所得數據導入專業聲學軟件進行聯閤倣真,生成氣動譟聲源項,包括偶極子聲源及四極子聲源,建立氣動譟聲產生傳播模型,求解輸氣管道氣體流經閥門的氣動譟聲。
위구분수기관도설루음파여벌문조성,위수기관도음파법설루검측제공이론의거급수거고、공제벌문조성제공해결판법,종음파산생궤리각도채용CFD연건우합전업성학연건방법대수기관도기체류경벌문산생적기동조성진행연구,건립기동조성모형,탐구기동조성산생궤리급전파、쇠감규률。재CFD(Computational Fluid Dynamics)연건중채용대와단류모형대기체류경벌문시적순태류장구해분석,획득류장분포여맥동압력、맥동속도수거;장CFD계산소득수거도입전업성학연건진행연합방진,생성기동조성원항,포괄우겁자성원급사겁자성원,건립기동조성산생전파모형,구해수기관도기체류경벌문적기동조성。
In order to distinguish leakage noise and valve noise,a theoretical basis and a database for leak detection and location based on acoustic method were provided and the method to control valve noise was introduced.The aero-noise induced by gas flow through valves in gas pipelines was studied from the view point of sound generation mechanism and an aero-noise model was built from which the rules governing the aero-noise generation,transmission and attenuation were concluded.The transient flow field with fluctuating pressure and fluctuating velocity was obtained with the help of large eddy simulation model by using computational fluid dynamics software when gas flows through valves in gas-pipelines.Then the data were imported into acoustic BEM software SYSNOISE to carry through numerical analysis,to generate noise source terms,including the dipole source and quadrupole source,to build the aero-noise model and finally to solve the aero-acoustics problems.