首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   4篇
  免费   0篇
  国内免费   2篇
航空   6篇
  2024年   1篇
  2023年   1篇
  2021年   1篇
  2020年   1篇
  2018年   1篇
  2015年   1篇
排序方式: 共有6条查询结果,搜索用时 15 毫秒
1
1.
    
In this paper, the effect of different amount of protrusion on various parameters in rotor–stator system was experimentally studied by measuring CO2 concentration and pressure, in order to obtain the optimal protrusion amount.The parameters of different dimensionless sealing flow were measured under the condition that the annulus Reynolds number was 4.39 × 105 and the rotating Reynolds number was 1.05 × 106.The results show that the change of the amount of protru...  相似文献   
2.
齿间凸起对直通篦齿封严特性影响的数值研究   总被引:1,自引:3,他引:1  
为提升篦齿的密封性能,对在齿间光滑衬套上增加矩形凸起的直通篦齿的流动特性进行了数值研究,分析了压比、凸起的尺寸和轴向位置对篦齿泄漏特性的影响。和光滑齿相比,凸起破坏了壁面射流附面层的连续性,改变了流体在齿腔中的流动方向,有效地提高了通道的密封性能,降低了通道的泄漏量。结果表明,当压比为2时,含有凸起结构的篦齿的泄漏系数较光滑齿降低了13%,当压比增加到4时,泄漏系数更是降低了18%;凸起的高度越大宽度越小,凸起对篦齿密封性能的提高就越明显;凸起和下级齿之间的轴向距离越短,凸起对流入下级齿的气体流动方向改变就越大,密封性能也就越好。  相似文献   
3.
《中国航空学报》2024,37(9):59-71
Analysing the influence mechanism of the riblet protrusion height on turbulent drag components is more beneficial in organising the vortical structure over the riblet surface.Therefore,the Large Eddy Simulation(LES)is used to investigate the vortex structure over the rib-let surface with different protrusion heights.Then,the variations of Reynolds stress and viscous shear stress in a turbulent channel are analysed.As a result,the drag reduction rate increases from 3.4%when the riblets are completely submerged in the turbulent boundary layer to 7.9%when the protrusion height is 11.2.Further analysis shows that the protrusion height affects the streamwise vortices and the normal diffusivity of spanwise and normal vortices,thus driving the variation of Reynolds stress.Compared with the smooth surface,the vorticity strength and the number of streamwise vortices are weakened near the wall but increase in the logarithmic layer with increased protrusion height.Meanwhile,the normal diffusivity of spanwise vorticity decreases with the increase of protrusion height,and the normal diffusivity of normal vorticity is the smallest when the protrusion height is 11.2.Moreover,the protrusion height affects the velocity gradient of the riblet tip and riblet valley,thus driving the variation of viscous shear stress.With the increase of protrusion height,the velocity gradient of the riblet tip increases dramatically but decreases in the riblet valley.  相似文献   
4.
    
《中国航空学报》2021,34(4):320-331
The windage loss caused by protrusion in a rotor–stator cavity has been studied in detail, and there are abundant fitting formulas that have been summarized to calculate the moment coefficients. Some other theorists have emphasized its effect on the sealing efficiency, proposing that installation of protrusion could alleviate gas ingestion. However, the protrusion shape which is an influential factor on the sealing efficiency has not been focused in previous research. Using the experimental method of measuring CO2 volume fraction, cavity pressure, and power consumption, we investigated the effects of several typical protrusion shapes on various parameters for two sealing structures, in order to obtain the optimal shape. Results showed that a variation of the protrusion shape had little impact on the static pressure, but the total pressure and the sealing efficiency increased in different degrees. Furthermore, even though the hexagon shape resulted in the highest sealing efficiency, we observed that the drop shape had the best overall performance in all of the eight models, which could result in higher efficiency of the turbine cavity. The combination of a radial seal structure and protrusion could improve sealing efficiency better.  相似文献   
5.
Nan CAO  Xiang LUO  Zeyu WU  Jie WEN 《中国航空学报》2018,31(11):2057-2072
This paper presents an experimental investigation on the effect of protrusion radial position and height on the sealing performance and flow structure in the rotor-stator cavity. The rotor-mounted protrusions are assembled at three radial positions and are set to three heights. The cavity is equipped with three rim seals: a radial seal, an axial seal and a seal with double fins on the stator. The annulus Reynolds number is set at 4.39×105 and the rotational Reynolds number ranges from 7.51×105 to 1.20×106. Heat and mass transfer analogy is applied. Pressure and CO2 concentration are measured. The experimental results show that in cavities with different rim seals, radial distributions of the sealing efficiency, pressure and swirl ratio are basically the same. The sealing performance is improved by protrusions compared with the cavity without protrusion and improves with the increase of protrusion radial position and height. The effect of protrusion increases with the increase of the rotational Reynolds number. The windage loss and the flow resistance introduced by protrusions are investigated. It is found that induced windage loss and flow resistance decrease with the increase of protrusion radial position but increase with the protrusion height.  相似文献   
6.
为了研究轮缘封严附近凸起的形状对封严效率的影响,采用测量二氧化碳体积分数、腔内压力的实验方法,研究了几种典型的凸起形状对封严效率、腔内压力、腔内流场和无量纲最小封严流量的影响,目的是获得最佳的凸起形状。结果表明,凸起形状的变化对腔内的静压影响不大,封严环附近的静压变化几乎可以忽略不计。而总压和封严效率将随着凸起形状的变化而不同。安装凸起会整体提升腔内的旋流比。当凸起形状为六面体时,腔内的总压和封严效率最大,其无量纲最小封严流量相比于光滑盘平均减少了32%。  相似文献   
1
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号