首页 | 本学科首页   官方微博 | 高级检索  
     

部分喷嘴关闭对预旋供气系统参数均匀性影响的计算
引用本文:雷昭,刘高文,顾伟. 部分喷嘴关闭对预旋供气系统参数均匀性影响的计算[J]. 航空动力学报, 2020, 35(5): 963-972. DOI: 10.13224/j.cnki.jasp.2020.05.008
作者姓名:雷昭  刘高文  顾伟
作者单位:西北工业大学动力与能源学院,西安710072,西北工业大学动力与能源学院,西安710072,中国航空发动机集团有限公司商用航空发动机有限责任公司,上海200241,西北工业大学动力与能源学院,西安710072
摘    要:为了研究部分喷嘴关闭对预旋供气系统的供气流量和供气温度及其均匀性的影响,采用稳态的固定转子相位法对180°旋转盘腔进行了数值模拟,并通过改变转子相位的稳态计算来近似模拟瞬态问题的时空变化特性。结果表明:在设计点工况(系统压比为1.32,旋转马赫数为0.678)下,喷嘴流通面积关闭14.3%时,引气总流量和供气总流量分别下降10.9%和9.9%。单个供气孔流量的波动幅度由1.1%增大为5.4%。供气的相对总温降低1 K左右,波动幅度由约0.5 K增大为1.5 K。

关 键 词:预旋供气系统  预旋喷嘴  主动控制  旋转盘腔  转子相位  不均匀性
收稿时间:2019-10-31

Numerical simulation of effects of partial nozzle closure on uniformity of parameters in pre-swirl air supply system
LEI Zhao,LIU Gaowen,GU Wei. Numerical simulation of effects of partial nozzle closure on uniformity of parameters in pre-swirl air supply system[J]. Journal of Aerospace Power, 2020, 35(5): 963-972. DOI: 10.13224/j.cnki.jasp.2020.05.008
Authors:LEI Zhao  LIU Gaowen  GU Wei
Abstract:In order to study the influence of the partial nozzle closure on the air supply mass flow rate, air supply temperature and circumferential uniformity of the air supply parameters of the pre-swirl air supply system, the steady-state method with frozen rotor approach was used to simulate the 180° rotating disk cavity model, and the time-space characteristics of transient problems were approximated by changing the rotor phase in the steady-state calculations. Results showed that: at the design point condition(system pressure ratio of 1.32 and rotating Mach number of 0.678), when the flow area of nozzle was closed by 14.3%, the total bleed air flow and total air supply flow decreased by 10.9% and 9.9%, respectively. The amplitude of fluctuation of the flow rate of a single supply hole increased from 1.1% to 5.4%. The relative total temperature of supply air decreased about 1 K, and the amplitude of fluctuation increased from 0.5 K to 1.5 K.
Keywords:pre-swirl air supply system  pre-swirl nozzle  active control  rotating disc cavity  rotor phase  non-uniformity
本文献已被 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载全文
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