Drive Control Simulation and Experimental Studies on the Flow Characteristics of a Pump Injector

被引:5
作者
Ji, Haocheng [1 ]
Wei, Minxiang [1 ]
Liu, Rui [2 ,3 ]
Chang, Cheng [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing 210016, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Peoples R China
[3] Nanjing Tech Univ, Sch Mech & Power Engn, Nanjing 211816, Peoples R China
关键词
Aviation aircrafts; direct injection; flow characteristics; peak and hold drive; piston engine; pump injector; FUEL; ENGINE; SPRAY; KEROSENE; JET;
D O I
10.1109/ACCESS.2020.2975014
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
As a miniaturized direct injection (DI) solution, the pump injector is of great significance for small aviation piston engines, such as two-stroke heavy-fuel engines. The accurate control of the timing and amount of injections is an important application prerequisite. In this paper, the flow characteristics of a pump injector with different driving circuits and parameters are investigated. The effects of the power supply and freewheeling circuits on the opening and closing delays are theoretically studied.Aschematic of a self-designed logic control circuit is proposed, and it achieves peak and hold current control without software intervention. Simulations and experiments are carried out, and the drive current and flow characteristics in different states are measured. The results show that when driving a solenoid with a high internal resistance of 2.70 Omega, a single power supply is more suitable, and the variable-freewheeling circuit exhibits excellent performance in terms of control accuracy and energy recovery. Notably, the invariable-freewheeling circuit results in nonlinear flow characteristics, and the nonlinear segment corresponds to the drive current transitioning from the peak value to the hold value. In contrast, the variable-freewheeling circuit overcomes this problem. To comprehensively consider solenoid opening and closing delays, energy consumption and the linearity of the flow characteristics during injection, a peak current of 10 A and a hold current of 8 A are adopted.
引用
收藏
页码:35672 / 35681
页数:10
相关论文
共 29 条
[1]  
Ahern S., 2005, APPL AIR ASSIST DIRE
[2]  
[Anonymous], 2016, J1832201610 SAE
[3]  
[Anonymous], 2002, Appl. Note AP32029 TC1775 In~neon, V2, Patent No. 3029
[4]  
[Anonymous], 2016, INT CONF ADVAN COMPU
[5]  
Austin R., 2011, UNMANNED AIRCRAFT SY, V54
[6]   Experimental and numerical study if a spark ignition engine with air-assisted direct injection [J].
Boretti, A. ;
Jin, S-H ;
Brear, M. ;
Zakis, G. ;
Attard, W. ;
Watson, H. ;
Brewster, S. ;
Bryce, W. .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART D-JOURNAL OF AUTOMOBILE ENGINEERING, 2008, 222 (D6) :1103-1119
[7]   Development of a novel dual-coil fuel injector for direct-injection spark ignition engines [J].
Chen, Yong ;
Zhang, Zhendong .
INTERNATIONAL JOURNAL OF APPLIED ELECTROMAGNETICS AND MECHANICS, 2018, 56 (02) :301-316
[8]   Conversion of a Spark-Ignited Aircraft Engine to JP-8 Heavy Fuel for Use in Unmanned Aerial Vehicles [J].
Duddy, Brian J. ;
Lee, James ;
Walluk, Mark ;
Hallbach, David .
SAE INTERNATIONAL JOURNAL OF ENGINES, 2011, 4 (01) :82-93
[9]   Trajectory deviation of target jet of air-assisted spray under different conditions [J].
Gao, Hongli ;
Zhang, Fujun ;
Zhang, Zhenyu ;
Wang, Sufei ;
Wu, Hao .
FUEL, 2019, 249 :252-263
[10]   The Numerical Study of Compressed-Air Atomizer for Spark-ignited Jet Fuel Engine [J].
Garipov, M. D. ;
Zinnatullin, R. F. ;
Shayakhmetov, V. A. .
INTERNATIONAL CONFERENCE ON INDUSTRIAL ENGINEERING (ICIE 2017), 2017, 206 :305-311