首页 | 本学科首页   官方微博 | 高级检索  
     检索      

Particle deposition patterns on high-pressure turbine vanes with aggressive inlet swirl
作者姓名:Xing YANG  Zihan HAO  Zhenping FENG
作者单位:Shaanxi Engineering Laboratory of Turbomachinery and Power Equipment, Institute of Turbomachinery, School of Energy and Power Engineering, Xi’an Jiaotong University
基金项目:co-supported by the National Nature Science Foundation of China (No. 51906185);
摘    要:Characteristics of particle migration and deposition were numerically investigated in presence of aggressive swirl at the turbine inlet. The isolated effects of the inlet swirl were considered in detail by shifting the circumferential position of the swirl and by implementing positive and negative swirling directions. Particles were released from the turbine inlet and the resulting deposition on the vanes was determined by using the critical velocity model in a range of particle diameters from 1...

收稿时间:18 October 2020

Particle deposition patterns on high-pressure turbine vanes with aggressive inlet swirl
Xing YANG,Zihan HAO,Zhenping FENG.Particle deposition patterns on high-pressure turbine vanes with aggressive inlet swirl[J].Chinese Journal of Aeronautics,2022,35(3):75-89.
Institution:Shaanxi Engineering Laboratory of Turbomachinery and Power Equipment, Institute of Turbomachinery, School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an 710049, China
Abstract:Characteristics of particle migration and deposition were numerically investigated in presence of aggressive swirl at the turbine inlet. The isolated effects of the inlet swirl were considered in detail by shifting the circumferential position of the swirl and by implementing positive and negative swirling directions. Particles were released from the turbine inlet and the resulting deposition on the vanes was determined by using the critical velocity model in a range of particle diameters from 1 to 25 μm. Results show that the particles are more likely to move outwards to the boundary walls of the passage by the action of the swirling flow. However, this could be relieved by increasing the particle size. An imbalance problem of the deposition is found between the adjacent vanes, which could introduce additional inlet non-uniformities towards the downstream rotor and thus accelerate performance degradation of the turbine stage. Overall, the negative swirl case has higher overall capture efficiency within the entire turbine than the positive swirl case for larger particles, and when the inlet swirl is shifted to the mid-passage of the turbine, more deposits could be produced in comparison with the case in which the swirl aims at the vane leading edge.
Keywords:Combustor-turbine interaction  Gas turbine  Inlet swirl  Numerical simulation  Particle deposition
本文献已被 ScienceDirect 等数据库收录!
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