| Citation: | SU Zhigang, ZHANG Lingxiao, DENG Tianet al. Fuel control law of small size turbofan engine[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(12): 2555-2562. doi: 10.13700/j.bh.1001-5965.2015.0829(in Chinese)
|
Focusing on the fuel control law of the small size turbofan engine DGEN380, a steady and transient component-level mathematical model was developed and simulated on MATLAB platform with analytic method. A special tool was used for modeling the rotating parts in order to get the components characteristics and draw the maps which can show the current operating point/line. In the steady model simulation process, the Newton-Raphson method and genetic algorithm were evaluated and compared for solving the working equations of the engine. The basic model was modified to overcome the limitations of simulation in the genetic algorithm. The Euler method was used to calculate the differential term for the transient model simulation. Based on the model, the fuel control law was studied, and the altitude characteristic was described as an example. The experimental results show that the Newton-Raphson method has high accuracy and speed, while the genetic algorithm has better adaptability with the model modification. The simulation results of the model and the control law fit the test data and theory well, as the error is maintained below 3%.
| [1] |
KONG X X, WANG X, TIAN D L, et al.An extrapolation approach for aeroengine's transient control law design[J].Chinese Journal of Aeronautics, 2013, 26(5):1106-1113. doi: 10.1016/j.cja.2013.04.027
|
| [2] |
冯海峰.航空涡轴发动机数学建模方法与控制规律研究[D].西安:西北工业大学, 2007:1-3.
FENG H F.Study of aero turbine engine mathematic model and control law[D].Xi'an:Northwestern Polytechnical University, 2007:1-3(in Chinese).
|
| [3] |
DUYAR A, GU Z, LITT J.A simplified dynamic model of the T700 turboshaft engine[J].Journal of the American Helicopter Society, 1995, 40(4):62-70. doi: 10.4050/JAHS.40.62
|
| [4] |
JAW L C, MATTINGLY J D.Aircraft engine control design, system analysis, and health monitoring[M].Reston:AIAA, 2009:187-201.
|
| [5] |
钱得峰.大涵道比民用涡扇发动机部件级建模技术研究[D].南京:南京航空航天大学, 2010:17-18.
QIAN D F.Research on component-level modeling technology for high bypass ratio civil turbofan engine[D].Nanjing:Nanjing University of Aeronautics and Astronautics, 2010:17-18(in Chinese).
|
| [6] |
蔡开龙, 谢寿生, 胡金海, 等.涡扇发动机燃油综合控制半实物仿真试验系统[J].推进技术, 2007, 28(4):422-427. http://www.cnki.com.cn/Article/CJFDTOTAL-TJJS200704018.htm
CAI K L, XIE S S, HU J H, et al.Semi-physical simulation experiment system of fuel integration control system for turbofan engine[J].Journal of Propulsion Technology, 2007, 28(4):422-427(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-TJJS200704018.htm
|
| [7] |
夏飞.基于MATLAB/Simulink的航空发动机建模与仿真研究[D].南京:南京航空航天大学, 2010:19-31.
XIA F.Modeling and simulation of aeroengines based on MATLAB/Simulink[D].Nanjing:Nanjing University of Aeronautics and Astronautics, 2010:19-31(in Chinese).
|
| [8] |
GAUDET S R.Development of a dynamic modeling and control system design methodology for gas turbine[D].Ottawa:Carleton University, 2007:52-58.
|
| [9] |
骆广琦.航空燃气涡轮发动机数值仿真[M].北京:国防工业出版社, 2007:70-90.
LUO G Q.Numerical simulation of aero gas turbine engine[M].Beijng:National Defence Industry Press, 2007:70-90(in Chinese).
|
| [10] |
梁宁宁.航空涡轴发动机建模与控制规律研究[D].南京:南京航空航天大学, 2011:14-15.
LIANG N N.Research on turboshaft engine modeling and control law[D].Nanjing:Nanjing University of Aeronautics and Astronautics, 2011:14-15(in Chinese).
|
| [11] |
苟学中, 周文祥, 黄金泉.变循环发动机部件级建模技术[J].航空动力学报, 2013, 28(1):104-111. http://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201301016.htm
GOU X Z, ZHOU W X, HUANG J Q.Component-level modeling technology for variable cycle engine[J].Journal of Aerospace Power, 2013, 28(1):104-111(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201301016.htm
|
| [12] |
葛海.大涵道比涡轮风扇发动机建模技术研究[D].南京:南京航空航天大学, 2013:33-35.
GE H.Research on modeling technology for high bypass ratio turbofan engine[D].Nanjing:Nanjing University of Aeronautics and Astronautics, 2013:33-35(in Chinese).
|
| [13] |
JOSHI G, KRISHNA M B.Solving system of nonlinear equations using genetic algorithm[C]//International Conference on Advances in Computing, Communications and Informatics.Piscataway, NJ:IEEE Press, 2014:1302-1308.
|
| [14] |
陈磊, 霍永亮.利用改进的遗传算法求解非线性方程组[J].西南师范大学学报(自然科学版), 2015, 40(1):23-27. http://www.cnki.com.cn/Article/CJFDTOTAL-XNZK201501005.htm
CHEN L, HUO Y L.On solution to nonlinear equation group by means of improved genetic algorithm[J].Journal of Southwest China Normal University (Natural Science Edition), 2015, 40(1):23-27(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-XNZK201501005.htm
|
| [15] |
ZHANG S Y, YU X, HU Y.Study of fuzzy control with Smith forecast and compensation for aeroengine[C]//International Conference on Information and Automation.Piscataway, NJ:IEEE Press, 2010:594-598.
|
| [16] |
田金虎, 乔渭阳, 彭生红.小涵道比涡扇发动机动态特性数值计算[J].航空动力学报, 2013, 28(9):1988-1996. http://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201309014.htm
TIAN J H, QIAO W Y, PENG S H.Numerical calculation of dynamic performance of low-bypass ratio turbofan engine[J].Journal of Aerospace Power, 2013, 28(9):1988-1996(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-HKDI201309014.htm
|
| [17] |
王鑫.航空发动机数学模型与控制规律研究[D].西安:西北工业大学, 2007:13-14. http://www.cnki.com.cn/Article/CJFDTOTAL-DKDX200504030.htm
WANG X.Study of aeroengine mathematic model and control law[D].Xi'an:Northwestern Polytechnical University, 2007:13-14(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-DKDX200504030.htm
|
| [18] |
樊思齐.航空发动机控制(下册)[M].西安:西北工业大学出版社, 2008:50-61.
FAN S Q.Aeroengine control (Ⅱ)[M].Xi'an:Northwestern Polytechnical University Press, 2008:50-61(in Chinese).
|
| [1] | WANG X D，WANG P，SONG Y F，et al. HRRP recognition of midcourse ballistic targets based on AF-BiTCN[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：349-359 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0025. |
| [2] | LIU He, WEI Cheng, ZHANG Zexu, SUN Bo, HU Zihang. Spacecraft Anomaly Detection Based on Filtered Autoencoder Envelope Analysis[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0832 |
| [3] | WANG L Y，HE H F，HE Y M，et al. Three-dimensional polarization filtering method of generalized oblique projection based on SVT[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：633-643 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0019. |
| [4] | WANG D，YANG J，XIONG K. Autonomous navigation method of satellite constellation based on adaptive UKF[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2655-2666 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0696. |
| [5] | SHI Chenfa, XIONG Zhi, JIANG Xu, LI Qijie, WANG Zhengchun. Cooperative Navigation for UAV Swarm Based on AHRS[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0343 |
| [6] | WAN Hongfa, LI Shanshan, LI Xinxing, TAN Xuli, PEI Xianyong. Analysis of observable degree of gravity aided inertial navigation[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0308 |
| [7] | YIN Q L，CHEN Q，WANG Z Y，et al. Trajectory programming method of gliding-guided projectiles for penetration[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3151-3161 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0049. |
| [8] | NIE Li, LI Chenliang, LIU Wangkui, SHEN Haidong, LIU Yanbin, CHEN Jinbao. Adaptive neural network based fixed-time command-filtered control for quadrotor unmanned aerial vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0403 |
| [9] | PAN C Z，HE G，LI Z J，et al. Adaptive filtered control for uncertain electro-hydraulic servo systems with time-varying output constraints[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1819-1828 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0497. |
| [10] | LI H，ZHONG H P，ZHANG P，et al. Multi-shift interferometric phase filtering method based on convolutional neural network[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：2043-2050 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0805. |
| [11] | LIU W，LIU C Y，GUO X K，et al. Deployment optimization method for missile early warning radar under complex and multi-directional missile threats[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（4）：1392-1404 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0486. |
| [12] | CHEN Hui, LIU Meng-bo, LIAN Feng, HAN Chong-zhao. Star convex irregular shape multi-extended target PMBM filter[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0766 |
| [13] | WANG Zhi-hui, XIANG Zhi-ning, GAO Ping. Research on Uncertainty in Kill Effectiveness of Anti-Ship Ballistic Missiles[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0774 |
| [14] | LIU S S，LI X，MAN H J，et al. Ballistic coefficient solution for non-cooperative targets and its application[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（5）：1036-1043 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0414. |
| [15] | MA Y F，DAI S W，WANG R，et al. Nonlinear spatial K-means clustering algorithm for detection of zero-speed interval in inertial pedestrian navigation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2841-2850 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0764. |
| [16] | ZHANG Yun-jie, ZHOU Jie-xin, ZHANG Feng-zhe, ZHOU Rui, ZOU Ting. Reachability Evaluation Method for Ballistic Missile Based on Extended Boundary Method[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0630 |
| [17] | JIN K D，CHAI H Z，SU C H，et al. Fading memory variational Bayesian adaptive filter based on variable attenuating factor[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：2989-2999 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0799. |
| [18] | SHU Hong-bin, YU Chuan-qiang, LIU Zhi-hao, TANG Sheng-jin, CHEN Jian-wei. State estimation of multi-axle special vehicles by fusion of neural network and unscented Kalman filter[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2022.0535 |
| [19] | DAI Hongde, ZHANG Xiaoyu, ZHENG Baidong, DAI Shaowu, ZHENG Weiwei. Inertial pedestrian navigation algorithm based on zero velocity update and attitude self-observation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1135-1144. doi: 10.13700/j.bh.1001-5965.2021.0037 |
| [20] | WU Lan, WU Yuanming, KONG Fanshi, LI Binquan. Traffic signal timing method based on deep reinforcement learning and extended Kalman filter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(8): 1353-1363. doi: 10.13700/j.bh.1001-5965.2021.0529 |
| 1. | 单新有，李映坤，许进升，朱敏，陈雄，何勇. 膏体推进剂近燃面区域的热解与燃烧过程. 火炸药学报. 2024(09): 830-839 .  | |
| 2. | 单新有，李映坤，武炎，陈雄，何勇. 基于MAC方法的膏体推进剂管道流动特性. 航空动力学报. 2023(10): 2430-2440 . |
Figures(11) / Tables(1)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
NIE Peng, ZHANG Daguo, CHEN Yanhai, et al. Carbon nanotubes thin film sensor and characterization of its strain sensing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(4): 677-684. doi: 10.13700/j.bh.1001-5965.2015.0271(in Chinese)
DownLoad:
