影响因子：6.4

所属单位：南京航空航天大学

发表刊物：Applied Thermal Engineering

项目来源：Lj重大专项

关键字：Gas turbine Thermal radiation Hot streak Blade heat load Transient numerical simulation

摘要：Hot Streak (HS) and thermal radiation are the two important factors affecting the heat transfer process in High Pressure (HP) turbine stage, while the previous investigations were limited in studying either of them independently. In order to investigate the combined effects of the HS and radiation, the present study is aimed at unsteady convection-radiation coupled simulations with regards to HS and uniform inlet conditions. Three dominant radiative factors were analyzed in details. Compared with the uniform cases, it is found that there are two high temperature regions in the rotor passages of HS cases. The maximum temperature increase of the vane surface is about 40 K caused by radiation. As the HS changes the temperature distribution, the radiative heat flux is redistributed and a portion of radiative heat flux transfer from the stator passage to the rotor passage. The turbine inlet radiation mainly affects on the guide vane, whereas the gas adiation has a more significant influence on the rotor blade heat load.

论文类型：期刊论文

学科门类：工学

文献类型：J

是否译文：否

发表时间：2018-04-23

收录刊物：SCI

合写作者：韩省思

第一作者：王天壹

通讯作者：宣益民