个人信息Personal Information
教授 博士生导师
招生学科专业:
动力工程及工程热物理 -- 【招收博士、硕士研究生】 -- 能源与动力学院
航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 能源与动力学院
能源动力 -- 【招收博士、硕士研究生】 -- 能源与动力学院
主要任职:江苏省“航空动力系统”重点实验室主任
其他任职:《航空发动机》副主编、《航空学报》中英文版编委、《推进技术》编委
毕业院校:南京航空航天大学
学历:南京航空航天大学
学位:工学博士学位
所在单位:能源与动力学院
办公地点:明故宫校区A10楼519房间、435房间
联系方式:mjkpe@nuaa.edu.cn
电子邮箱:
Experimental Investigation on Flow Characteristics of Turbine Plenum Chamber and Flow Resistance Model
点击次数:
所属单位:能源与动力学院
发表刊物:Tuijin Jishu
摘要:To obtain the flow characteristics of turbine plenum chamber such as the distribution of outflow and the flow resistance coefficient, a typical configuration, which has 4 air intakes and 125 exit holes located in two lines, was experimentally investigated. The ratio of inlet pressure to outlet pressure, the chamber height were changed in experiments, then the flow characteristics of turbine plenum varying with these parameters were obtained. It was found that the holes directly facing the entrance had the maximum flow rate, while flow rate decreased greatly in the region very near those holes. As the holes' circumferential locations were away from the entrance, their flow rate quickly recovered and remained alomost the same. Meanwhile the minimum outflow rate was observed in the holes located circumferentially at the middle region between every two inlet holes. However these maximum and minimum mass flow rates were only 9.34% and 3.29% of the total flow, respectively. It was also found that with the increasing of inlet pressure and chamber height, the mass flow rate going through turbine plenum chamber increased, while the distribution of circumferential outflow did not change. Compared against inlet pressure, chamber height affected flow characteristics much more faintly. Finally correlation equations about flow resistance were concluded in this paper, which took geometrical parameters and inflow/outflow aerodynamic parameters into account. One dimensional component of turbine plenum chamber for secondary air system was also developed based on those correlation equations, which can support the design and optimization of secondary air system. © 2017, Editorial Department of Journal of Propulsion Technology. All right reserved.
ISSN号:1001-4055
是否译文:否
发表时间:2017-02-01
合写作者:Yao, Tian,Jiang, Liang-Liang,Shan, Wen-Juan,Wang, Hai,Chai, Jun-Sheng,Lu, Hai-Ying
通讯作者:毛军逵