In order to completely enhance the safety of liquid rocket engine turbopump
aiming at its start-up process
a method for vibration fault detection was presented.Firstly
the vibration data sampled by equal time interval were resampled and the data of equiangular interval were obtained to drive out the speed fluctuation influence on vibration features.Secondly
the vibration feature was selected and calculated.Finally
the nonlinear relational model between vibration feature and rotational speed was founded by support vector regression.Once the deviation between the new test data and the model is over a limit
it shows evidence of turbopump fault.The detection time of 2.2s test data is 0.0470s.It shows that the model can be used for the turbopump fault detection in start-up process.
Predicting method of safety life of reusable liquid rocket engine turbopump
Failure mechanism and improvement of ball bearing in aliquid rocket engine turbopump
Maintenance decision method of a turbofan engine based on fault detection
Fault detection for liquid-propellant rocket engine based on improved inductive monitoring system
Fault detection of aero-engine non-linear distributed control system based on T-S fuzzy model
Related Author
Dengfeng LIU
Xiaoqiu MA
Guozhu LIANG
Shijie LIU
ZHENG Yanwei
ZHANG Song
DENG Sier
LI Wenchao
Related Institution
Laboratory of Science and Technology on Cryogenic Liquid Propulsion,Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
School of Astronatuics,Beihang University
Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation