Research and application of steady flow intake control method in icing wind tunnel engine intake simulation system
-
摘要:
针对结冰风洞发动机进气部件试验稳流量进气控制难题,结合提供进气条件的发动机进气模拟系统的工作原理,提出采用卡尔曼滤波无模型自适应控制方法,通过建立系统动态线性化数据模型,利用卡尔曼滤波对实际动态流量输出做真值预估,估值与期望值的差值经过动态数据模型计算,得到调节系统抽气设备转速的输入量,进行稳流量进气控制,最后应用于某型号发动机进气部件防冰试验。试验结果表明:发动机进气模拟系统运行稳定可靠,输出的进气流量符合试验要求,进气稳流量控制精度达到0.1 kg/s。
-
关键词:
- 稳流量进气控制 /
- 发动机进气模拟系统 /
- 卡尔曼滤波无模型自适应控制 /
- 进气部件防冰试验 /
- 进气流量
Abstract:In view of the problem of steady flow intake control of engine intake components in icing wind tunnel, and by combining the working principle of engine intake simulation system available with intake conditions, the Kalman filter model-free adaptive control method was adopted; by establishing the system dynamic linearization data model, and using the Kalman filter to make a true value estimate of the actual dynamic flow output, the difference between the estimate and the expected value was calculated through the dynamic data model, the input amount of the speed of the pumping equipment of the system was obtained, and the steady flow intake control was carried out. Finally, it was applied to the anti-icing test of the intake components of a certain type of engine. The test results showed that the engine intake simulation system performed stably and reliably, the output intake flow met the test requirements, and the control accuracy of the intake air steady flow reached 0.1 kg/s.
-
-
[1] 林贵平, 卜雪琴, 申晓斌. 飞机结冰与防冰技术[M]. 北京: 北京航空航天大学出版社, 2016. [2] 常士楠. 大型飞机的防/除冰问题[C]//大型飞机关键技术高层论坛暨中国航空学会2007年学术年会论文集. 深圳: 中国航空学会, 2007: 469-475. [3] 宋建宇,吴晶峰,邱长波,等. 民用涡轴发动机进气系统结冰试验[J]. 航空动力学报,2020,35(5): 1089-1098. doi: 10.13224/j.cnki.jasp.2020.05.020SONG Jianyu,WU Jingfeng,QIU Changbo,et al. Civil turboshaft engine induction system icing test[J]. Journal of Aerospace Power,2020,35(5): 1089-1098. (in Chinese) doi: 10.13224/j.cnki.jasp.2020.05.020 [4] 綦蕾,李红琳,陈智强. 浅谈民用航空发动机适航技术新要求[J]. 航空动力,2020(1): 45-48.QI Lei,LI Honglin,CHEN Zhiqiang. New airworthiness technical requirements for civil aero engines[J]. Aerospace Power,2020(1): 45-48. (in Chinese) [5] 白尨,刘月平. 航空发动机进气系统结冰适航性条款研究[J]. 燃气涡轮试验与研究,2013,26(5): 41-45, 54. doi: 10.3969/j.issn.1672-2620.2013.05.008BAI Meng,LIU Yueping. Airworthiness standards on aero-engine induction system icing[J]. Gas Turbine Experiment and Research,2013,26(5): 41-45, 54. (in Chinese) doi: 10.3969/j.issn.1672-2620.2013.05.008 [6] 韩冰冰,李新,付涵,等. CCAR-25与CCAR-33适航审定关系分析[J]. 航空工程进展,2018,9(4): 537-543. doi: 10.16615/j.cnki.1674-8190.2018.04.011HAN Bingbing,LI Xin,FU Han,et al. Analysis of the relationship between CCAR-25 and CCAR-33 airworthiness[J]. Advances in Aeronautical Science and Engineering,2018,9(4): 537-543. (in Chinese) doi: 10.16615/j.cnki.1674-8190.2018.04.011 [7] 郭向东,柳庆林,赖庆仁,等. 大型结冰风洞气流场适航符合性验证[J]. 空气动力学学报,2021,39(2): 184-195. doi: 10.7638/kqdlxxb-2019.0086GUO Xiangdong,LIU Qinglin,LAI Qingren,et al. Airworthiness compliance verification of aerodynamic flowfield of a large-scale icing wind tunnel[J]. Acta Aerodynamica Sinica,2021,39(2): 184-195. (in Chinese) doi: 10.7638/kqdlxxb-2019.0086 [8] 易贤,王斌,李伟斌,等. 飞机结冰冰形测量方法研究进展[J]. 航空学报,2017,38(2): 520711.YI Xian,WANG Bin,LI Weibin,et al. Research progress on ice shape measurement approaches for aircraft icing[J]. Acta Aeronautica et Astronautica Sinica,2017,38(2): 520711. (in Chinese) [9] 赖庆仁,柳庆林,郭龙,等. 基于大型结冰风洞的航空发动机结冰与防冰试验技术[J]. 实验流体力学,2021,35(3): 1-8.LAI Qingren,LIU Qinglin,GUO Long,et al. Icing and anti-icing test technology of aero-engine based on large-scale icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics,2021,35(3): 1-8. (in Chinese) [10] 倪章松,刘森云,王桥,等. 3 m×2 m结冰风洞试验技术研究进展[J]. 实验流体力学,2019,33(6): 46-53.NI Zhangsong,LIU Senyun,WANG Qiao,et al. Research progress of test technologies for 3 m×2 m icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics,2019,33(6): 46-53. (in Chinese) [11] 熊建军,刘锡,冉林,等. 基于控制律的电加热防除冰系统设计与验证[J]. 测控技术,2021,40(2): 130-134,139. doi: 10.19708/j.ckjs.2020.07.276XIONG Jianjun,LIU Xi,RAN Lin,et al. Design and verification of electrical heating anti-icing/deicing system based on control law[J]. Measurement & Control Technology,2021,40(2): 130-134,139. (in Chinese) doi: 10.19708/j.ckjs.2020.07.276 [12] 冉林, 熊建军, 王梓旭, 等. 一种进气模拟系统、进气模拟方法和空模型压损模拟方法: CN113375891B[P]. 2022-05-17. [13] 王先炜,樊晓锋,林森什,等. 结冰对直升机进气系统压力损失影响的试验研究及分析[J]. 直升机技术,2021(4): 62-66.WANG Xianwei,FAN Xiaofeng,LIN Senshi,et al. Analysis and research on icing test for pressure loss of air intake system of helicopter[J]. Helicopter Technique,2021(4): 62-66. (in Chinese) [14] 卢行远,侯忠生. 基于改进卡尔曼滤波器的扰动抑制无模型自适应控制方案[J]. 控制理论与应用,2022,39(7): 1211-1218.LU Xingyuan,HOU Zhongsheng. Model free adaptive control with disturbance rejection based on modified Kalman filter[J]. Control Theory & Applications,2022,39(7): 1211-1218. (in Chinese) [15] 侯忠生. 非参数模型及其自适应控制理论[M]. 北京: 科学出版社, 1999. [16] 侯忠生,韩志刚. 非线性系统参数估计及与之对偶的自适应控制[J]. 自动化学报,1995,21(1): 122-125. doi: 10.16383/j.aas.1995.01.020HOU Zhongsheng,HAN Zhigang. Parameter estimation algorithm of nonlinear systems and its dual adaptive control[J]. Acta Automatica Sinica,1995,21(1): 122-125. (in Chinese) doi: 10.16383/j.aas.1995.01.020 [17] 侯忠生. 无模型自适应控制的现状与展望[J]. 控制理论与应用,2006,23(4): 586-592. doi: 10.3969/j.issn.1000-8152.2006.04.017HOU Zhongsheng. On model-free adaptive control: the state of the art and perspective[J]. Control Theory & Applications,2006,23(4): 586-592. (in Chinese) doi: 10.3969/j.issn.1000-8152.2006.04.017 [18] 邓望权,田震,王子楠,等. 基于PI与无模型自适应控制结合的燃气轮机转速控制方法[J]. 推进技术,2022,43(7): 404-412. doi: 10.13675/j.cnki.tjjs.210006DENG Wangquan,TIAN Zhen,WANG Zinan,et al. Speed control method of gas turbine based on combination of PI and model free adaptive control[J]. Journal of Propulsion Technology,2022,43(7): 404-412. (in Chinese) doi: 10.13675/j.cnki.tjjs.210006 [19] 田涛涛. 无模型自适应控制在无人驾驶汽车中的应用[D]. 北京: 北京交通大学, 2017.TIAN Taotao. Model-free adaptive control based on self-driving car[D]. Beijing: Beijing Jiaotong University, 2017. (in Chinese) [20] 彭丁聪. 卡尔曼滤波的基本原理及应用[J]. 软件导刊,2009,8(11): 32-34.PENG Dingcong. Basic principle and application of Kalman filter[J]. Software Guide,2009,8(11): 32-34. (in Chinese) [21] 李顶根,田瑞华,伍琳. 固冲发动机进气流量测量及卡尔曼滤波应用研究[J]. 航空兵器,2015,22(5): 66-68. doi: 10.3969/j.issn.1673-5048.2015.05.013LI Dinggen,TIAN Ruihua,WU Lin. Solid ramjet motor flow measurement and application of Kalman filter[J]. Aero Weaponry,2015,22(5): 66-68. (in Chinese) doi: 10.3969/j.issn.1673-5048.2015.05.013