先进航空发动机核心关键技术
收稿日期: 2024-09-18
修回日期: 2024-10-15
录用日期: 2024-11-05
网络出版日期: 2024-11-25
基金资助
国家级项目
Core key technologies of advanced aircraft engine
Received date: 2024-09-18
Revised date: 2024-10-15
Accepted date: 2024-11-05
Online published: 2024-11-25
Supported by
National Level Project
程荣辉 , 张志舒 , 阮文博 , 王建锋 . 先进航空发动机核心关键技术[J]. 航空学报, 2025 , 46(12) : 31220 -031220 . DOI: 10.7527/S1000-6893.2024.31220
Aircraft engine is the core key to achieving comprehensive improvement in combat capabilities of advanced fighter jets. The increasing requirements for high performance, high reliability, long lifespan, and good maintainability of fighter jet engines have posed significant challenges to the development of aircraft engine technology and products. This article focuses on the core technical requirements of advanced fighter jets for aviation engines in seven aspects: comprehensive temperature control, rotor structure system robustness, full authority digital control, aircraft-engine thermal management, health management, thrust vectoring, and high stealth. The technical paths and main key technologies for meeting these requirements are analyzed, which can provide technical support for the development of advanced aviation engines.
| [1] | 程荣辉, 张志舒, 陈仲光. 第四代战斗机动力技术特征和实现途径[J]. 航空学报, 2019, 40(3): 022698. |
| CHENG R H, ZHANG Z S, CHEN Z G. Technical characteristics and implementation of the fourth-generation jet fighter engines[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(3): 022698 (in Chinese). | |
| [2] | 刘大响, 程荣辉. 世界航空动力技术的现状及发展动向[J]. 北京航空航天大学学报, 2002, 28(5): 490-496. |
| LIU D X, CHENG R H. Current status and development direction of aircraft power technology in the world[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(5): 490-496 (in Chinese). | |
| [3] | 杨伟. 关于未来战斗机发展的若干讨论[J]. 航空学报, 2020, 41(6): 524377. |
| YANG W. Development of future fighters[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(6): 524377 (in Chinese). | |
| [4] | 孙聪. 从空战制胜机理演变看未来战斗机发展趋势[J]. 航空学报, 2021, 42(8): 525826. |
| SUN C. Development trend of future fighter: A review of evolution of winning mechanism in air combat[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(8): 525826 (in Chinese). | |
| [5] | 孙志岩. 航空发动机控制系统发展概述[J]. 测控技术, 2019, 38(6): 1-4. |
| SUN Z Y. Overview of the development of aircraft engine control systems[J]. Measurement & Control Technology, 2019, 38(6): 1-4 (in Chinese). | |
| [6] | 王海峰. 战斗机推力矢量关键技术及应用展望[J]. 航空学报, 2020, 41(6): 524057. |
| WANG H F. Key technologies and future applications of thrust vectoring on fighter aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(6): 524057 (in Chinese). | |
| [7] | 陈仲光, 张志舒, 李德旺, 等. F119发动机总体性能特点分析与评估[J]. 航空科学技术, 2013, 24(3): 39-42. |
| CHEN Z G, ZHANG Z S, LI D W, et al. Analysis and evaluation of F119 engine overall performance[J]. Aeronautical Science & Technology, 2013, 24(3): 39-42 (in Chinese). | |
| [8] | LEFEBVRE A H. Gas turbine combustion?[M]. Lon-don: McGraw-Hill, 1983: 201-230. |
| [9] | 贾琳渊, 程荣辉, 张志舒, 等. 研发阶段涡扇发动机模型自适应方法[J]. 推进技术, 2020, 41(9): 1935-1945. |
| JIA L Y, CHENG R H, ZHANG Z S, et al. Adaptive modelling for turbofan engine in development stage?[J]. Journal of Propulsion Technology, 2020, 41(9): 1935-1945 (in Chinese). | |
| [10] | MARDANI A, ASADI B, BEIGE A A. Investigation of flame structure and precessing vortex core instability of a gas turbine model combustor with different swirler configurations[J]. Physics of Fluids, 2022, 34(8): 085129. |
| [11] | ZHANG Q, ZHANG P, SUN S L, et al. Large eddy simulation study of flow field characteristics of a combustor with two coaxial swirlers[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2020, 234(5): 625-642. |
| [12] | ESHATI S, ABDUL GHAFIR M F, LASKARIDIS P, et al. Impact of operating conditions and design parameters on gas turbine hot section creep life[C]?∥Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air. New York: ASME, 2010. |
| [13] | VERSTRAETE T, AMARAL S, VAN DEN BRAEMBUSSCHE R, et al. Design and optimization of the internal cooling channels of a HP turbine blade: Part Ⅱ: Optimization[C]∥Proceedings of ASME Turbo Expo 2008: Power for Land, Sea and Air. New York: ASME, 2008. |
| [14] | 程荣辉, 马艳红, 李超, 等. 航空燃气轮机结构系统动力学设计[M]. 北京: 北京航空航天大学出版社, 2023: 59-106. |
| CHENG R H, MA Y H, LI C, et al. Dynamic design of aero-engine structural system[M]. Beijing: Beijing University of Aeronautics & Astronautics Press, 2023: 59-106 (in Chinese). | |
| [15] | CHEN X Q, MA Y H, HONG J. Vibration suppression of additional unbalance caused by the non-continuous characteristics of a typical aero-engine rotor[C]?∥Proceedings of the 10th International Conference on Rotor Dynamics. Cham: Springer International Publishing, 2018: 34-48. |
| [16] | 王东, 韩卓荦, 杨哲夫, 等. 连接结构刚度非对称对高速转子动力特性影响[J]. 航空动力学报, 2024, 39(12): 133-143. |
| WANG D, HAN Z L, YANG Z F, et al. Influence of unsymmetrical stiffness of joints on high-speed rotor dynamic characteristics?[J]. Journal of Aerospace Power, 2024, 39(12): 133-143 (in Chinese). | |
| [17] | LIU S G, MA Y H, ZHANG D Y, et al. Studies on dynamic characteristics of the joint in the aero-engine rotor system?[J]. Mechanical Systems and Signal Processing, 2012, 29: 120-136. |
| [18] | HONG J, CHEN X Q, WANG Y F, et al. Optimization of dynamics of non-continuous rotor based on model of rotor stiffness?[J]. Mechanical Systems and Signal Processing, 2019, 131: 166-182. |
| [19] | 王东, 洪杰, 李其建, 等. 双转子航空发动机中介支点动载荷控制研究[J]. 航空动力学报, 2024, 40(2):20230252. |
| WANG D, HONG J, LI Q J, et al. Dynamic load control of intermediate fulcrum of dual rotor aero-engine[J]. Journal of Aerospace Power, 2024, 40(2):20230252 (in Chinese). | |
| [20] | PENG G, LI C, ZHENG H Q, et al. Quantitative analysis method of whole aero-engine structural design based on structural efficiency[C]?∥Proceedings of the 10th International Conference on Rotor Dynamics. Cham: Springer International Publishing, 2019: 3-17. |
| [21] | SCHWINGSHACKL C W, DI MAIO D, SEVER I, et al. Modeling and validation of the nonlinear dynamic behavior of bolted flange joints[J]. Journal of Engineering for Gas Turbines and Power, 2013, 135(12): 122504. |
| [22] | QIN Z Y, HAN Q K, CHU F L. Bolt loosening at rotating joint interface and its influence on rotor dynamics[J]. Engineering Failure Analysis, 2016, 59: 456-466. |
| [23] | LIU C, WANG D, WANG Y F, et al. Dynamic response and suppression method of high-speed rotors under the rotary inertial moment: GT2023-102818?[R]. New York: ASME, 2023. |
| [24] | HONG J, LI T R, ZHENG H Q, et al. Applications of structural efficiency assessment method on structural-mechanical characteristics integrated design in aero-engines?[J]. Chinese Journal of Aeronautics, 2020, 33(4): 1260-1271. |
| [25] | VOLPONI A, SIMON D L. Enhanced Self Tuning On-Board Real-Time Model (eSTORM) for aircraft engine performance health tracking: NASA/CR-2008-215272 [R]. Washington, D.C.: NASA, 2008. |
| [26] | MYERS L P. F-15 digital electronic engine control system description: PAPER-3[R]. Washington, D.C.: NASA, 1984. |
| [27] | 王建锋, 张天宏, 周永权, 等. 一种双通道热并行架构FADEC系统任务可靠性分析[J/OL]. 航空发动机, (2024-08-01)[2024-11-19]. . |
| WANG J F, ZHANG T H, ZHOU Y Q, et al. Research on mission reliability modeling and analysis for the dual-channel hot-parallelism architecture FADEC system?[J/OL]. Aeroengine, (2024-08-01)[2024-11-19]. (in Chinese). | |
| [28] | YAN W Z, GOEBEL K, LI J C. Classifier performance measures in multifault diagnosis for aircraft engines[C]∥Proceedings of SPIE, Component and Systems Diagnos-tics, Prognostics, and Health Management Ⅱ. Bellingham: SPIE, 2002. |
| [29] | KOBAYASHI T, SIMON D L. Application of a bank of Kalman filters for aircraft engine fault diagnostics[C]∥Proceedings of ASME Turbo Expo 2003, Power for Land, Sea, and Air. New York: ASME, 2003. |
| [30] | BROTHERTON T, VOLPONI A, LUPPOLD R, et al. eSTORM: Enhanced self tuning on-board real-time engine model[C]?∥2003 IEEE Aerospace Conference Proceedings. Piscataway: IEEE Press, 2003: 3075-3086. |
| [31] | VOLPONI A, BROTHERTON T, LUPPOLD R. Empirical tuning of an on-board gas turbine engine model for real-time module performance estimation[J]. Journal of Engineering for Gas Turbines and Power, 2008, 130(2): 021604. |
| [32] | ROBERTS R A, DECKER D D. Control architecture study focused on energy savings of an aircraft thermal management system?[C]?∥Proceedings of ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. New York: ASME, 2013. |
| [33] | FISCHER A. Future fuel heat sink thermal management system technologies: AIAA-2006-4026?[R]. Reston: AIAA, 2006. |
| [34] | JUSTICE K M, DALTON J S, HALLIWELL I, et al. Lube oil and bearing thermal management system?: GT2009-60048[R]. New York: ASME, 2009. |
| [35] | PANGBORN H C, HEY J E, DEPPEN T O, et al. Hardware-in-the-loop validation of advanced fuel thermal management control?[J]. Journal of Thermophysics and Heat Transfer, 2017, 31(4): 901-909. |
| [36] | WALTERS E, AMRHEIN M, O’CONNELL T, et al. INVENT modeling, simulation, analysis and optimization?[C]?∥48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2010. |
| [37] | HENDRICKS T J, MCENERNEY B, DRYMIOTIS F, et al. Design and testing of high-performance mini-channel graphite heat exchangers in thermoelectric energy recovery systems?[C]?∥ASME 2017 International Mechanical Engineering Congress and Exposition. New York: ASME, 2017. |
| [38] | DEMOTT L. TF41-A-2/A7E inflight engine condition monitoring ?system/IECMS: ?AIAA-1978-1472?[R]. Resotn: AIAA, 1978. |
| [39] | STAMATIS A G. Engine condition monitoring and diagnostics[M]∥BENINI E. Progress in Gas Turbine Performance. London: InTechOpen, 2013: 187-212. |
| [40] | AMIRKHANI S, TOOTCHI A, CHAIBAKHSH A. Fault detection and isolation of gas turbine using series-parallel NARX model?[J]. ISA Transactions, 2022, 120: 205-221. |
| [41] | RAHMOUNE M BEN, HAFAIFA A, KOUZOU A, et al. Gas turbine monitoring using neural network dynamic nonlinear autoregressive with external exogenous input modelling[J]. Mathematics and Computers in Simulation, 2021, 179: 23-47. |
| [42] | 冷子昊, 程荣辉, 苏壮, 等. 基于飞发一体化的滑油系统热性能仿真[J]. 航空发动机, 2024, 50(2): 121-126. |
| LENG Z H, CHENG R H, SU Z, et al. Thermal performance simulation of lubricating oil system based on aircraft-engine integration?[J]. Aeroengine, 2024, 50(2): 121-126 (in Chinese). | |
| [43] | EBERT F J. Fundamentals of design and technology of rolling element bearings[J]. Chinese Journal of Aeronautics, 2010, 23(1): 123-136. |
| [44] | DEMPSEY P, BOLANDER N, HAYNES C, et al. Investigation of bearing fatigue damage life prediction using oil debris monitoring: NASA/TM—2011-217117[R]. Washington, D.C.: NASA, 2010. |
| [45] | QIU H, EKLUND N, LUO H, et al. Fusion of vibration and on-line oil debris sensors for aircraft engine bearing prognosis: AIAA-2010-2858[R]. Reston: AIAA, 2010. |
| [46] | JIAO R H, PENG K X, DONG J, et al. Fault monitoring and remaining useful life prediction framework for multiple fault modes in prognostics[J]. Reliability Engineering & System Safety, 2020, 203: 107028. |
| [47] | SHI Z Y, CHEHADE A. A dual-LSTM framework combining change point detection and remaining useful life prediction?[J]. Reliability Engineering & System Safety, 2021, 205: 107257. |
| [48] | SHIN C S, KIM H D, SETOGUCHI T, et al. A computational study of thrust vectoring control using dual throat nozzle?[J]. Journal of Thermal Science, 2010, 19(6): 486-490. |
| [49] | CARSON G T, CAPONE F J .Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability:NASA-TM-4237[R]. Washington, D.C.: NASA, 1991. |
| [50] | 张志学, 王强, 邵万仁, 等. 航空发动机排气系统设计[M]. 北京: 科学出版社, 2022: 135. |
| ZHANG Z X, WANG Q, SHAO W R. Design of aircraft engine exhaust system[M]. Beijing: Science Press, 2022: 135 (in Chinese). | |
| [51] | 张少丽, 周吉利, 徐兴平, 等. 轴对称收扩喷管温度场数值仿真[J]. 航空发动机, 2023, 49(4): 122-127. |
| ZHANG S L, ZHOU J L, XU X P, et al. Numerical simulation on the temperature field of axisymmetric convergent divergent nozzle[J]. Aeroengine, 2023, 49(4): 122-127 (in Chinese). | |
| [52] | 桑建华, 张宗斌. 红外隐身技术发展趋势[J]. 红外与激光工程, 2013, 42(1): 14-19. |
| SANG J H, ZHANG Z B. Development trends of infrared stealth technology[J]. Infrared and Laser Engineering, 2013, 42(1): 14-19 (in Chinese). | |
| [53] | CHEN H Y, ZHANG H B, XI Z H, et al. Modeling of the turbofan with an ejector nozzle based on infrared prediction[J]. Applied Thermal Engineering, 2019, 159: 113910. |
| [54] | RAO G A, MAHULIKAR S P. Integrated review of stealth technology and its role in airpower[J]. The Aeronautical Journal, 2002, 106(1066): 629-642. |
| [55] | 王群, 邓洪伟, 杨胜男, 等. 一体化加力燃烧室支板雷达隐身修形仿真[J]. 航空发动机, 2022, 48(6): 1-6. |
| WANG Q, DENG H W, YANG S N, et al. Study on radar stealth shaping for struts of integrated rear frame and afterburner[J]. Aeroengine, 2022, 48(6): 1-6 (in Chinese). | |
| [56] | 邓洪伟, 尚守堂, 邵万仁, 等. 基于加力内锥冷却的红外隐身技术研究[J]. 航空发动机, 2011, 37(2): 12-15, 37. |
| DENG H W, SHANG S T, SHAO W R, et al. Investigation on infrared stealth technology based on afterburning cone cooling[J]. Aeroengine, 2011, 37(2): 12-15, 37 (in Chinese). | |
| [57] | WANG H, JI H H, LU H H. Experimental investigation on infrared radiation characteristics of two-dimensional convergent-divergent vectoring nozzle?[J]. Journal of Thermophysics and Heat Transfer, 2019, 33(3): 627-637. |
| [58] | WANG H, JI H H, LU H H. The influence of nozzle deflection on fluid dynamic and infrared characteristics of a two-dimensional convergent-divergent vectoring exhaust system[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(12): 4646-4662. |
| [59] | HAN T, LUO R Y, CUI G Y, et al. Effect of SiC nanowires on the high-temperature microwave absorption properties of SiCf/SiC composites[J]. Journal of the European Ceramic Society, 2019, 39(5): 1743-1756. |
| [60] | DUAN S C, ZHU D M, DONG J, et al. Enhanced mechanical and microwave absorption properties of SiCf/SiC composite using aluminum powder as active filler[J]. Journal of Alloys and Compounds, 2019, 790: 58-69. |
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