TY - JOUR
T1 - 变循环发动机地面起动建模及控制规律设计方法
AU - Hao, Wang
AU - Wang, Zhanxue
AU - Zhang, Xiaobo
AU - Zhou, Li
AU - Wang, Jingkai
N1 - Publisher Copyright:
© 2022, Editorial Department of Journal of Aerospace Power. All right reserved.
PY - 2022/1
Y1 - 2022/1
N2 - To solve the problem of discontinuous isentropic efficiency of rotating components, a method of using correct torque instead of isentropic efficiency was proposed.The extrapolation method of low speed characteristics of rotating components was given, and the full speed characteristics of rotating components were obtained.A burner stability model considering ignition and burn stability was proposed.Finally, a component⁃level starting model of the variable cycle engine was established.Considering the eight variable parameters of the variable cycle engine, the differential evolution algorithm was used to optimize the starting process of the variable cycle engine in the double bypass and single bypass modes.The results showed that the starting time of the variable cycle engine in the double bypass and single bypass modes was 17.2 s and 12.8 s, respectively.In the double bypass mode, the fuel flow, nozzle throat area and outer bypass area of rear variable area bypass injector need to be adjusted.In the single bypass mode, the fuel flow, nozzle throat area and low pressure turbine inlet guide vane area need to be adjusted.When the free stream Mach number was equal to 0.04, the starting time of the variable cycle engine in the double bypass and single bypass modes was 0.2 s less than the static state.
AB - To solve the problem of discontinuous isentropic efficiency of rotating components, a method of using correct torque instead of isentropic efficiency was proposed.The extrapolation method of low speed characteristics of rotating components was given, and the full speed characteristics of rotating components were obtained.A burner stability model considering ignition and burn stability was proposed.Finally, a component⁃level starting model of the variable cycle engine was established.Considering the eight variable parameters of the variable cycle engine, the differential evolution algorithm was used to optimize the starting process of the variable cycle engine in the double bypass and single bypass modes.The results showed that the starting time of the variable cycle engine in the double bypass and single bypass modes was 17.2 s and 12.8 s, respectively.In the double bypass mode, the fuel flow, nozzle throat area and outer bypass area of rear variable area bypass injector need to be adjusted.In the single bypass mode, the fuel flow, nozzle throat area and low pressure turbine inlet guide vane area need to be adjusted.When the free stream Mach number was equal to 0.04, the starting time of the variable cycle engine in the double bypass and single bypass modes was 0.2 s less than the static state.
KW - Component characteristics
KW - Component⁃level starting model
KW - Control law design
KW - Differential evolution algorithm
KW - Variable cycle engine
UR - http://www.scopus.com/inward/record.url?scp=85124571999&partnerID=8YFLogxK
U2 - 10.13224/j.cnki.jasp.20210132
DO - 10.13224/j.cnki.jasp.20210132
M3 - 文章
AN - SCOPUS:85124571999
SN - 1000-8055
VL - 37
SP - 152
EP - 164
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 1
ER -