气力输砂试验系统惯性分离元件性能研究  被引量:2

Research on the performance of impact inertia separator in sand/dust test system feeding by air

在线阅读下载全文

作  者:李宏伟[1,2] 刘景江[2] 韩海波[2] 刘静[2] 石金侠[2] 

机构地区:[1]北京航空航天大学航空科学与工程学院,北京100191 [2]白城兵器试验中心,吉林白城137001

出  处:《计算机与应用化学》2013年第3期319-321,共3页Computers and Applied Chemistry

摘  要:为研究气力输砂系统中惯性分离元件的性能,采用欧拉-拉格朗日方法数值模拟了平面形底边、三角形底边和半圆形底边3种分离元件的流场和颗粒撞击特性,并对比分析了不同风速时,3种分离元件的分离效率和阻力特性。研究结果表明,分离元件底边形状对气流阻力、颗粒运动轨迹及其与壁面碰撞次数有很大影响,平面底边分离元件的分离效率随风速的提高下降幅度较大,因而仅适用于低速情况;三角形底边元件分离效率及其对风速的适应性均有很大改善;而半圆形底边分离元件分离效率最佳,并且基本不受来流速度影响。因此,当风速较高时应考虑优先采用三角形底边或半圆形底边分离元件。研究结果对类似气力输砂系统分离器的设计及优化具有指导意义。In order to obtain the performance of inertia separator in the sand/dust test system, the flow field and particles' impact characters about three kinds of separate components are studied by numerical simulation based on Euler-Lagrange method, then the separate efficiency and resistance characters under various main flow velocity are analyzed. The results indicated that, the shape of separate components' bottom affect the air flow resistance, the moving trajectories of particles, the amount of impact between particles and separator wall seriously. The separate efficiency of separate component with a flat bottom decreased obviously along with the increase of air velocity, so this kind of component should be used only in the occasions where the air velocity is low. The efficiency and the flexibility to the air velocity of separate component with a triangle bottom are improved greatly. The separate efficiency of component with a semicircular bottom is the highest among these three kinds of components studied in this paper, and is affected by the incoming air flow velocity slightly. So the component with a triangle or semicircular bottom is recommended to be used in case of the air velocity is relative high. The study results provide reference for the design and optimization of separator which is purposed to be used in similar pneumatic feeding system.

关 键 词:气力输砂 惯性分离器 气固两相流 CFD 砂尘试验 

分 类 号:V211[航空宇航科学与技术—航空宇航推进理论与工程] TK223[动力工程及工程热物理—动力机械及工程]

 

参考文献:

正在载入数据...

 

二级参考文献:

正在载入数据...

 

耦合文献:

正在载入数据...

 

引证文献:

正在载入数据...

 

二级引证文献:

正在载入数据...

 

同被引文献:

正在载入数据...

 

相关期刊文献:

正在载入数据...

相关的主题
相关的作者对象
相关的机构对象