开式转子发动机变桨距机构研究进展

孙鹏; 陈永辉; 燕群; 霍施宇; 杨晓林

doi:10.7643/issn.1672-9242.2026.08.007

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装备环境工程 ›› 2026, Vol. 23 ›› Issue (8) : 52-57. DOI: 10.7643/issn.1672-9242.2026.08.007

专题——装备综合环境强度分析与试验技术

开式转子发动机变桨距机构研究进展

孙鹏, 陈永辉, 燕群, 霍施宇, 杨晓林

作者信息 +

Research Progress of Open Rotor Engine Pitch Change Mechanism

SUN Peng, CHEN Yonghui, YAN Qun, HUO Shiyu, YANG Xiaolin

Author information +

文章历史 +

摘要

主要分析了国内外变桨距机构的研制历程与技术进展,分别对液压变桨距机构和电动机械式变桨距机构特点进行了分析,对其研制所涉及的关键技术进行了讨论,总结了变桨距机构未来发展趋势和重点技术发展方向,以期为开式转子发动机变桨距机构的后续研制提供技术支持。

Abstract

The work mainly analyzes the historical and technological advancements of pitch change mechanisms both domestically and globally, explores the features of hydraulic and electromechanical pitch change mechanisms, talks about the major technologies involved in their development, and summarizes future trends and important technical development directions for pitch change mechanisms, so as to provide technical support for the subsequent development of pitch change mechanisms for open rotor engines.

导出引用

孙鹏, 陈永辉, 燕群, 霍施宇, 杨晓林. 开式转子发动机变桨距机构研究进展[J]. 装备环境工程. 2026, 23(8): 52-57 https://doi.org/10.7643/issn.1672-9242.2026.08.007

SUN Peng, CHEN Yonghui, YAN Qun, HUO Shiyu, YANG Xiaolin. Research Progress of Open Rotor Engine Pitch Change Mechanism[J]. Equipment Environmental Engineering. 2026, 23(8): 52-57 https://doi.org/10.7643/issn.1672-9242.2026.08.007

中图分类号： V231

参考文献

[1] PERULLO C A, TAI J C M, MAVRIS D N. Effects of Advanced Engine Technology on Open Rotor Cycle Selection and Performance[J]. Journal of Engineering for Gas Turbines and Power, 2013, 135(7): 259-269.
[2] VAN ZANTE D E, COLLIER F, ORTON A, et al. Progress in Open Rotor Propulsors: The FAA/GE/NASA Open Rotor Test Campaign[J]. The Aeronautical Journal, 2014, 118(1208): 1181-1213.
[3] VAN ZANTE D E. Progress in Open Rotor Research: A U.S. Perspective[C]//Volume 1: Aircraft Engine; Fans and Blowers, Marine. Montreal: American Society of Mechanical Engineers, 2015.
[4] 严成忠. 开式转子发动机[M]. 北京: 航空工业出版社, 2016.
YAN C Z.Open Rotor Engine[M]. Beijing: Aviation Industry Press, 2016.
[5] 郝羿飞, 胡士吉. 开式转子发动机的最新研究进展[J]. 国际航空, 2017(3): 58-59.
HAO Y F, HU S J.Progressing on Open-Rotor Technology[J]. International Aviation, 2017(3): 58-59.
[6] 周莉, 是介, 王占学. 开式转子发动机研究进展[J]. 推进技术, 2019, 40(9): 1921-1932.
ZHOU L, SHI J, WANG Z X.Research Progress in Open Rotor Engine[J]. Journal of Propulsion Technology, 2019, 40(9): 1921-1932.
[7] MASTROPIERRO F S, SEBASTIAMPILLAI J, JACOB F, et al.Modeling Geared Turbofan and Open Rotor Engine Performance for Year-2050 Long-Range and Short- Range Aircraft[J]. Journal of Engineering for Gas Turbines and Power, 2020, 142(4): 041016.
[8] DORSEY A, URANGA A.Design Space Exploration of Future Open Rotor Configurations[C]//AIAA Propulsion and Energy 2020 Forum. Virginia: AIAA, 2020.
[9] 何萍, 王翔宇. 赛峰和GE启动可持续发动机革新技术演示验证计划[J]. 航空动力, 2021(4): 40-43.
HE P, WANG X Y.Safran and GE Aviation Launch RISE Program[J]. Aerospace Power, 2021(4): 40-43.
[10] 周杰, 秦家禄. 开式转子发动机:航空动力减排增效的关键技术路径与发展趋势[J]. 航空动力, 2025(4): 40-43.
ZHOU J, QIN J L.Open Rotor Engine: Key Technological Pathway and Development Trends for Fuel-Efficient and Low-Emission Aero Engine[J]. Aerospace Power, 2025(4): 40-43.
[11] 张锦绣, ANTHONY J, 李泳凡. A320飞机换装开式转子发动机的匹配研究和直接使用成本计算[C]//中国航空学会第七届动力年会. 北京: 中国航空学会, 2010.
ZHANG J X, ANTHONY J, LI Y Y.Matching Research and Direct Cost Calculation of A320 Aircraft with Open Rotor Engine Replacement[C]//The 7th Annual Power Conference of the Chinese Aeronautical Society. Beijing: Chinese Aeronautical Society, 2010.
[12] STEINETZ B, LOEWENTHAL S, SARGISSON D, et al.An Advanced Pitch Change Mechanism Incorporating a Hybrid Traction Drive[C]//20th Joint Propulsion Conference. Virginia: AIAA, 1984.
[13] WILLIAMS T, HALL C, WILSON M.Variable Pitch Fan Aerodynamic Design for Reverse Thrust Operation[J]. Journal of the Global Power and Propulsion Society, 2023, 7: 127-139.
[14] VITLARIS D, RAJENDRAN D J, TUNSTALL R, et al.On Hysteresis in a Variable Pitch Fan Transitioning to Reverse Thrust Mode and back[J]. Journal of Engineering for Gas Turbines and Power, 2025, 147(7): 071007.
[15] SMITH D J.The Sustainable and Green Engine (SAGE) - Aircraft Engine of the Future[J]. The International Journal of Entrepreneurship and Innovation, 2016, 17(4): 256-262.
[16] GE Aviation Systems Limited. Final Report Summary- OREAT (Open Rotor Engines Advanced Technologies for Rotor Blade Pitch Change Mechanism): 255762[R]. United Kingdom: GE Aviation Systems Limited, 2010
[17] 徐德康. 欧洲“清洁天空”项目最新进展[J]. 国际航空, 2013(8): 55-57.
XU D K.European “Clean Sky” Project Updating[J]. International Aviation, 2013(8): 55-57.
[18] 陈培儒. 欧盟的雄心——“净洁天空计划2”启动[J]. 大飞机, 2014(5): 43-46.
CHEN P R.EU’s Ambition-“Clean Sky Plan 2” Launched[J]. Jetliner, 2014(5): 43-46.
[19] BROUCKAERT J F, MIRVILLE F, PHUAH K, et al.Clean Sky Research and Demonstration Programmes for Next-Generation Aircraft Engines[J]. The Aeronautical Journal, 2018, 122(1254): 1163-1175.
[20] CHRISTOPHE D.Technology Maturation in Clean Sky 2 for Next Generation SMR Engine[C]//Proceedings of 33^nd Congress of the International Council of the Aeronautical Sciences. Sweden:[s. n.], 2022.
[21] 田涛, 程文旺. 欧洲发布《“清洁天空2”十年成就报告》[J]. 国际航空, 2025(9): 54-58.
TIAN T, CHENG W W.Clean Sky 2 Achievement Report[J]. International Aviation, 2025(9): 54-58.
[22] 徐鹤鸣, 毕懿鑫, 陈实, 等. 带有变桨距系统的开式风扇发动机: CN202311280394.6[P].2025-03-28.
XU H M, BI Y X, CHEN S, et al. Open Fan Engine with Variable Pitch System: CN202311280394.6[P].2025-03-28.
[23] 杜辉, 孙凯, 石英, 等. 一种发动机桨距角调节装置及调节方法: CN202510031298.0[P].2025-05-27.
DU H, SUN K, SHI Y, et al. An Engine Pitch Angle Adjustment Device and Method: CN202510031298.0[P].2025-05-27.
[24] 孙凯, 杜辉, 侯乃先, 等. 用于风扇叶片的桨距角测量装置以及测量方法: CN202510735403.9[P].2025-07-08.
SUN K, DU H, HOU N X, et al. Pitch Angle Measuring Device and Method for Fan Blades: CN202510735403. 9[P].2025-07-08.
[25] 孙凯, 杜辉, 侯乃先, 等. 具有变桨距机构的涡轮发动机的风扇模块、涡轮发动机、桨距调节方法: CN2025 10797874.2[P].2025-09-02.
SUN K, DU H, HOU N X, et al. Fan Module, Turbine Engine,Pitch Adjustment Method for Turbine Engines with Variable Pitch Mechanism: CN 202510797874. 2[P].2025-09-02.
[26] 侯乃先, 潘毅飞, 方际澄, 等. 桨距角测量装置、开式转子发动机及其设计方法: CN202511770480.4[P].2025-12-26.
HOU N X, PAN Y F, FANG J C, et al. Pitch Angle Measuring Device, Open Rotor Engine and its Design Method, CN202511770480.4[P].2025-12-26.
[27] 侯乃先, 蔡培, 徐鹤鸣, 等. 叶片变桨距作动装置及航空发动机: CN202511737540.2[P].2025-12-23.
HOU N X, CAI P, XU H M, et al. Blade Pitch Control Actuator and Aircraft Engine: CN202511737540.2[P].2025-12-23.
[28] 陈实, 孙凯, 徐逸晗, 等. 磁控变桨距联调装置、开式转子发动机和涡轮螺旋桨发动机试验件: CN20231 1547894.1[P].2025-05-20.
CHEN S, SUN K, XU Y H, et al. Magnetic Controlled Pitch Control Device, Open Rotor Engine,Turboprop Engine Test Specimens: CN202311547894.1[P].2023-11- 17.
[29] 陈实, 徐逸晗, 孙凯. 一种用于发动机桨扇的配重装置及其参数设计方法: CN202410650296.5[P].2025-11-25.
CHEN S, XU Y H, SUN K. Blade Pitch Control Actuator and Aircraft Engine: CN202410650296.5[P].2024-05-23.
[30] 交通运输部. 螺旋桨适航规定[J]. 中华人民共和国国务院公报, 2026, 4: 26-33.
Ministry of Transport. Airworthiness Regulations for Propellers[J]. Bulletin of the State Council of the People's Republic of China, 2026, 4: 26-33.