TY - GEN
T1 - Design of fault diagnosis system for pulse detonation engine
AU - Wang, Bin Kui
AU - Li, Jiang Hong
AU - Zhang, Wen Long
AU - Fan, Wei
AU - Wang, Ke
AU - Fu, Meng
N1 - Publisher Copyright:
© 2019 IEEE.
PY - 2019/7
Y1 - 2019/7
N2 - In order to explore the stable operating mechanism and operating boundary conditions of PDE, a failure diagnosis system was designed in this study. The inputs of the failure diagnosis system are as follows: engine control signals of the igniter and the solenoid valve, pressure signals and flame ion current signal of the detonation chamber, flow signal of the high-frequency flow-meter of the fuel and oxidizer channel. In each ignition cycle, the equivalence ratio of engine, the mixing time of fuel and oxidizer, the characteristics of the solenoid valve, the propagation speed of the combustion wave, the pressure of the detonation chamber, and other characteristic signals are accurately analyzed to obtain the engine operating status and the cause of the failure. In each second, statistics of the total number of engine ignitions, detonation success rate, and failure diagnosis results are implemented, then the statistical results, i.e., the signal waveforms and characteristic parameters of each ignition cycle, are transmitted to the human-computer interaction unit display. As a result, the engine operating parameters are visualized, the efficiency of failure diagnosis and operating boundary conditions exploration is improved.
AB - In order to explore the stable operating mechanism and operating boundary conditions of PDE, a failure diagnosis system was designed in this study. The inputs of the failure diagnosis system are as follows: engine control signals of the igniter and the solenoid valve, pressure signals and flame ion current signal of the detonation chamber, flow signal of the high-frequency flow-meter of the fuel and oxidizer channel. In each ignition cycle, the equivalence ratio of engine, the mixing time of fuel and oxidizer, the characteristics of the solenoid valve, the propagation speed of the combustion wave, the pressure of the detonation chamber, and other characteristic signals are accurately analyzed to obtain the engine operating status and the cause of the failure. In each second, statistics of the total number of engine ignitions, detonation success rate, and failure diagnosis results are implemented, then the statistical results, i.e., the signal waveforms and characteristic parameters of each ignition cycle, are transmitted to the human-computer interaction unit display. As a result, the engine operating parameters are visualized, the efficiency of failure diagnosis and operating boundary conditions exploration is improved.
KW - Equivalence ratio measurement
KW - Failure diagnosis
KW - Mixing time measurement
KW - Pulse detonation engine
KW - Solenoid valve
UR - http://www.scopus.com/inward/record.url?scp=85074856424&partnerID=8YFLogxK
U2 - 10.1109/ICMAE.2019.8880998
DO - 10.1109/ICMAE.2019.8880998
M3 - 会议稿件
AN - SCOPUS:85074856424
T3 - 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
SP - 292
EP - 296
BT - 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
Y2 - 22 July 2019 through 25 July 2019
ER -