| Citation: | JIANG Tianmu, ZHANG Xiaobo, WANG Zhanxue, et al. Control law design of lift fan starting based on time prediction[J]. Journal of Aerospace Power, 2023, 38（8）：2001-2014 doi: 10.13224/j.cnki.jasp.20230020
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To reduce the shaft driven lift fan starting time, a general control law design method was proposed for the shaft driven lift fan propulsion system. A prediction model of the remaining starting time based on trend extrapolation and with a reference to the lift fan speed curve was established. Based on the time prediction model and control law pointwise optimization design method, the starting process control law was optimized point by point, and the starting process control law can be obtained by performing multiple rounds of optimization and using the optimization results of each round to update the reference speed curve. This method was used to design the control law of the starting process with the low-pressure rotor speed at the initial state of 50%. The starting time was only 3.1 s, which was 22.5% shorter than that of the pointwise optimization method, and the starting process strictly met the safe working limit. Furthermore, multiple groups of starting process control laws with the initial speed of 90% and between 50% and 90% were designed, illustrating that this method is not only suitable for starting at low speeds, but also effective at high speeds.
| [1] |
WALKER G P, FULLER J W, WURTH S P. F-35B integrated flight-propulsion control development[R]. AIAA-2013-4243, 2013.
|
| [2] |
WURTH S P. F-35 propulsion system integration, development & verification[R]. AIAA-2018-3517, 2018.
|
| [3] |
刘帅. 短/垂起降飞机用推进系统性能模拟及三轴承偏转喷管设计技术研究[D]. 西安: 西北工业大学, 2016.
LIU Shuai. Investigation on short/vertical takeoff aircraft propulsion system performance simulation and three bearing deflection nozzle design technology[D]. Xi’an: Northwestern Polytechnical University, 2016. (in Chinese)
|
| [4] |
BEVILAQUA P. The shaft driven lift fan propulsion system for the joint strike fighter[C]//Proceedings of American Helicopter Society 53rd Annual Forum. Virgania, US: American Helicopter Society, 1997: 1634-1642.
|
| [5] |
高丽敏,马驰,李瑞宇. F-35B对转升力风扇研究进展[J]. 风机技术,2017,59(5): 49-57. doi: 10.16492/j.fjjs.2017.05.0009
GAO Limin,MA Chi,LI Ruiyu. Recent progress in the F-35B counter-rotating lift fan[J]. Chinese Journal of Turbomachinery,2017,59(5): 49-57. (in Chinese) doi: 10.16492/j.fjjs.2017.05.0009
|
| [6] |
BOUTON M T, SCHWERIN D M. Clutch coupled to gas turbine engine and method for cooling: US 10443663 B2[P]. 2019-10-15.
|
| [7] |
WIEGAND C. F-35 air vehicle technology overview[R]. AIAA-2018-3368, 2018.
|
| [8] |
HARRIS J J. F-35 flight control law design, development and verification[C]//Proceedings of 2018 Aviation Technology, Integration, and Operations Conference. Atlanta, US: AIAA, 2018:3516.
|
| [9] |
HAMSTRA J W. The F-35 Lightning Ⅱ: from concept to cockpit[M]. Reston, US: AIAA, 2019.
|
| [10] |
BEVILAQUA P. Joint strike fighter dual-cycle propulsion system[J]. Journal of Propulsion and Power,2005,21(5): 778-783. doi: 10.2514/1.15228
|
| [11] |
BEVILAQUA P. Future application of the JSF variable cycle[R]. AIAA-2003-2614, 2003.
|
| [12] |
ARNULFO L,PILIDIS P,YIN J,et al. Remote lift-fan engines[J]. Journal of Aerospace Engineering,2001,215(3): 155-163.
|
| [13] |
刘帅,王占学,周莉,等. 三轴承旋转喷管矢量偏转规律及流场特性研究[J]. 推进技术,2015,36(5): 656-663. doi: 10.13675/j.cnki.tjjs.2015.05.003
LIU Shuai,WANG Zhanxue,ZHOU Li,et al. Three bearing swivel nozzle vector deflection law study and fluid field calculation[J]. Journal of Propulsion Technology,2015,36(5): 656-663. (in Chinese) doi: 10.13675/j.cnki.tjjs.2015.05.003
|
| [14] |
符大伟,张海波. 带升力风扇的垂直起降推进系统建模研究[J]. 推进技术,2018,39(3): 685-694. doi: 10.13675/j.cnki.tjjs.2018.03.024
FU Dawei,ZHANG Haibo. Modeling of a STOVL propulsion system with a lift fan[J]. Journal of Propulsion Technology,2018,39(3): 685-694. (in Chinese) doi: 10.13675/j.cnki.tjjs.2018.03.024
|
| [15] |
任冰涛,李秋红,亢岚,等. 短距起飞/垂直降落发动机建模技术研究[J]. 航空动力学报,2015,30(10): 2531-2538. doi: 10.13224/j.cnki.jasp.2015.10.028
REN Bingtao,LI Qiuhong,KANG Lan,et al. Research of short take off and vertical landing engine modeling techniques[J]. Journal of Aerospace Power,2015,30(10): 2531-2538. (in Chinese) doi: 10.13224/j.cnki.jasp.2015.10.028
|
| [16] |
庞淑伟,李秋红,任冰涛,等. STOVL飞机发动机多变量控制方法[J]. 航空动力学报,2017,32(8): 2041-2048. doi: 10.13224/j.cnki.jasp.2017.08.030
PANG Shuwei,LI Qiuhong,REN Bingtao,et al. STOVL aircraft engine multi-variable control method[J]. Journal of Aerospace Power,2017,32(8): 2041-2048. (in Chinese) doi: 10.13224/j.cnki.jasp.2017.08.030
|
| [17] |
江天牧, 张晓博, 王占学. STOVL推进系统模式转换过程建模及分析[EB/OL]. [2023-01-09].https: //www.cnki.com.cn/Article/CJFDTotal-HKDI20220303003.htm.
JIANG Tianmu, ZHANG Xiaobo, WANG Zhanxue. Simulation and analysis of mode conversion performance for STOVL propulsion system [EB/OL]. [2023-01-09].https: //www.cnki.com.cn/Article/CJFDTotal-HKDI20220303003.htm. (in Chinese)
|
| [18] |
YE Yifan,WANG Zhanxue,ZHANG Xiaobo. Sequential ensemble optimization based on general surrogate model prediction variance and its application on engine acceleration schedule design[J]. Chinese Journal of Aeronautics,2021,34(8): 16-33. doi: 10.1016/j.cja.2021.03.010
|
| [19] |
ZHENG Qiangang,ZHANG Haibo. A global optimization control for turbo-fan engine acceleration schedule design[J]. Proceedings of the Institution of Mechanical Engineers: Part G Journal of Aerospace Engineering,2018,232(2): 308-316. doi: 10.1177/0954410016683412
|
| [20] |
郝旺,王占学,张晓博,等. 变循环发动机模态转换建模及控制规律设计方法研究[J]. 推进技术,2022,43(1): 78-87.
HAO Wang,WANG Zhanxue,ZHANG Xiaobo,et al. Mode transition modeling and control law design method of variable cycle engine[J]. Journal of Propulsion Technology,2022,43(1): 78-87. (in Chinese)
|
| [21] |
LI Jie,FAN Ding,SREERAM V. Optimization of aero engine acceleration control in combat state based on genetic algorithms[J]. International Journal of Turbo & Jet-Engines,2012,29(1): 29-36.
|
| [22] |
周红. 变循环发动机特性分析及其与飞机一体化设计研究[D]. 西安: 西北工业大学, 2016.
ZHOU Hong. Investigation on the variable cycle engine characteristics and integration design with aircraft[D]. Xi’an: Northwestern Polytechnical University, 2016. (in Chinese)
|
| [23] |
郝旺,王占学,张晓博,等. 变循环发动机地面起动建模及控制规律设计方法[J]. 航空动力学报,2022,37(1): 152-164.
HAO Wang,WANG Zhanxue,ZHANG Xiaobo,et al. Ground starting modeling and control law design method of variable cycle engine[J]. Journal of Aerospace Power,2022,37(1): 152-164. (in Chinese)
|
| [24] |
ZHANG Xiaobo,WANG Zhanxue,ZHOU Li,et al. Multidisciplinary design optimization on conceptual design of aero-engine[J]. International Journal of Turbo & Jet-Engines,2016,33(2): 195-208.
|
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