
中国航空研究院,北京,100129
Published:2021
移动端阅览
吴希明, 牟晓伟. 直升机关键技术及未来发展与设想[J]. 空气动力学学报, 2021, 39(3): 1−10.
WU Ximing, MU Xiaowei. A perspective of the future development of key helicopter technologies[J]. 2021, 39(3): 1-10.
吴希明, 牟晓伟. 直升机关键技术及未来发展与设想[J]. 空气动力学学报, 2021, 39(3): 1−10. DOI: 10.7638/kqdlxxb-2021.0042
WU Ximing, MU Xiaowei. A perspective of the future development of key helicopter technologies[J]. 2021, 39(3): 1-10. DOI: 10.7638/kqdlxxb-2021.0042.
本文针对直升机特有的技术特点,尤其是其区别于固定翼飞机的飞行原理、复杂气动和结构动力学特性、极致重量设计等,对包括气动、振动、噪声、地面共振/空中共振、抗坠毁、安全性及重量控制等方面的直升机技术难点进行剖析,对问题产生的原因、机理进行深入浅出的分析,对当前技术发展情况及解决方法进行了阐述。随后对世界直升机技术发展方向进行了分析与探讨,提出未来直升机技术将以高速、绿色、智能化、无人及安全飞行等方向为重点,并结合我国直升机技术发展现状和未来发展趋势,提出了我国直升机技术未来发展的三个重要方向—先进直升机旋翼桨叶翼型设计技术、智能旋翼技术和高速直升机技术,提出了各发展方向的关键技术的科学内涵和解决途径,为我国直升机未来发展提供思路。
This paper focuses on the special technical characteristics of helicopters
especially on the flight principle that differs from fixed-wing aircrafts
complex aerodynamics and structural dynamics
and demanding weight design
etc. Technical difficulties in aerodynamics
vibration and noise
ground/air resonance
crashworthy
safety
and weight control
as well as the underlying physical mechanisms and solutions are also expounded. Based on the analyses and study about development directions of helicopter technology in the world
it is proposed that future helicopter technology will focuses on high-speed
green
intelligent
unmanned
and safe flight. Combining the present situation and future trend of the helicopter technology development in China
three important directions for the future development of helicopter technology in China are put forward. These directions are advanced rotor blade and airfoil design
smart rotor
and high-speed helicopter. The scientific connotation and possible solutions of key technologies for the above directions are further proposed
which can hopefully provide a good idea for the future development of Chinese helicopter technology.
WANG Y M. Research and analysis on global civil helicopter market[J]. Jiangsu Science Technology Information, 2020, 37(17): 34-37. (in Chinese)
YANG J, ZHAN Y M, HONG B. Development status and plans of world military helicopter industry[J]. Helicopter Technique, 2020(3): 68-72. (in Chinese)
LUO X M. Prospect analysis of domestic civil helicopter development[J]. Aeronautical Manufacturing Technology, 2015, 58(3): 12-15. (in Chinese)DOI: 10.16080/j.issn1671-833x.2015.03.012.
XIAO Z Y, GUO Y H, ZHANG L, et al. State-of-the-art and trend analyses in CFD based simulation of rotorcraft[J]. Acta Aerodynamica Sinica, 2021, 39(5): 1-9.
WANG S C, XU G H. Progress of helicopter rotor aerodynamics[J]. Journal of Nanjing University of Aeronautics Astronautics, 2001, 33(3): 203-211. (in Chinese)
HU S H, WEI B B. Multi objective aerodynamic design and analysis of airfoil based on genetic algorithm[J]. Electronic Design Engineering, 2019, 27(13): 49-52, 57. (in Chinese)DOI: 10.14022/j.cnki.dzsjgc.2019.13.011.
ZHANG W L. Vibration fault analysis of helicopter based on vibration prediction technology[J]. Modern Machinery, 2019(5): 26-30. (in Chinese)DOI: 10.13667/j.cnki.52-1046/th.2019.05.007.
CHEN P J, ZHONG W G, DUAN G Z. Progress in aero-acoustic technology of helicopter[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(3): 18-24. (in Chinese)
TIAN X, SHEN Y J, MA X Y. Rotor active control technology research[J]. China Science and Technology Information, 2019(Z1): 37-44. (in Chinese)
DAI Z X, QIAN F, FENG Z Z. Development and trend of helicopter main reduction fluidlastic vibration isolation technology[J]. Aeronautical Science Technology, 2020, 31(6): 19-26. (in Chinese)DOI: 10.19452/j.issn1007-5453.2020.06.004.
林长亮, 王金亮, 张亚军, 等. 直升机振动主动控制技术研究现状[C]//探索 创新 交流——第六届中国航空学会青年科技论坛论文集. 沈阳, 2014: 557-562.
MA X Y, CHEN H. Design optimization of ground resonance influence parametersfor a helicopter[J]. Helicopter Technique, 2020(2): 10-14. (in Chinese)
YANG K T. Research on the development of helicopter active control technology[J]. Aeronautical Science and Technology, 2006, 17(5): 21-25. (in Chinese)
ZHAO Z L, XU F. Dynamic analysis of “ship resonance” for shipboard helicopter[J]. Science Technology and Engineering, 2020, 20(16): 6650-6657. (in Chinese)
CHENG Y B, MEI Z Y, YUN Q W. Research and design of database system about crashworthy helicopter[J]. Mechanical Engineering Automation, 2017(1): 85-87. (in Chinese)
LUO Z P, XIANG J W. Crashworthiness performance evaluation to helicopter landing gear by finite element simulation[J]. Acta Aeronautica et Astronautica Sinica, 2003, 24(3): 216-219. (in Chinese)
REN X W, MA Z Y. Crashworthiness design of helicopter fuel system components[J]. Helicopter Technique, 2020(4): 69-72. (in Chinese)
ZHANG H L. The technology of helicopter lightning protection[J]. Helicopter Technique, 2014(4): 35-38. (in Chinese)
SONG W S, YANG C S. Design and analysis of loss-of-lubrication capacity of helicopter reducer[J]. Journal of Mechanical Transmission, 2020, 44(1): 156-162. (in Chinese)DOI: 10.16578/j.issn.1004.2539.2020.01.026.
LIU H L. The development of helicopter power supply system[J]. Practical Electronics, 2018(11): 82-83. (in Chinese)DOI: 10.16589/j.cnki.cn11-3571/tn.2018.11.033.
WANG H, LI X Y, WANG T, et al. Research on helicopter autorotation experiment and safety characteristics[J]. Engineering Test, 2015, 55(1): 34-37. (in Chinese)
LIN C L, WANG Y F, WANG H W, et al. Computation of dynamic response of helicopter blade under bird impact[J]. Journal of Vibration and Shock, 2013, 32(10): 62-68. (in Chinese)DOI: 10.13465/j.cnki.jvs.2013.10.017.
ZHAO Q H. Analysis of civil helicopter L/HIRF under RMSG-3[J]. Modern Information Technology, 2020, 4(6): 34-36. (in Chinese)DOI: 10.19850/j.cnki.2096-4706.2020.06.012.
ZHANG H T. Helicopter cost estimating based on the empty weight[J]. Aeronautical Science Technology, 2013, 24(2): 18-21. (in Chinese)
XU W J. Artificial intelligence technology in helicopter[J]. Electronic Technology Software Engineering, 2020(2): 153-154. (in Chinese)
OSBORNE T, YUAN Z Y, CHEN Y. Big data simplifying HUMS for helicopters[J]. Aviation Maintenance Engineering, 2019(1): 27-28. (in Chinese)DOI: 10.19302/j.cnki.1672-0989.2019.01.006.
王锦盛. 基于机器学习的直升机飞行状态识别技术研究[D]. 南昌: 南昌航空大学, 2017.
WANG F, ZHANG J Y. Development and key technology of electric helicopter[J]. Modern Manufacturing Technology and Equipment, 2020(1): 144-145. (in Chinese)DOI: 10.16107/j.cnki.mmte.2020.0060.
SUN X S, CHENG W Y, MU Z D, et al. White paper on the development of electric aircraft[J]. Aeronautical Science Technology, 2019, 30(11): 1-7. (in Chinese)DOI: 10.19452/j.issn1007-5453.2019.11.001.
LI K S. Summary of research on core technology of electric aircraft[J]. Aeronautical Science Technology, 2019, 30(11): 8-17. (in Chinese)DOI: 10.19452/j.issn1007-5453.2019.11.002.
LI K S. Research on the development of electric aircraft technology[J]. Aeronautical Science Technology, 2019, 30(1): 1-7. (in Chinese)DOI: 10.19452/j.issn1007-5453.2019.30.001.
YIN X F, ZHANG D B, ZHANG J Y, et al. Development status and key technologies of micro unmanned helicopter[J]. Aerodynamic Missile Journal, 2018(5): 33-37. (in Chinese)DOI: 10.16338/j.issn.1009-1319.20170324.
HAN Z G. Developing progress and enlightenment of US cooperative technique for manned helicopters and unmanned aerial vehicles[J]. Telecommunication Engineering, 2018, 58(1): 113-118. (in Chinese)
LU F G, CHEN S C. Demand analysis of helicopter borne air to ground missile precision strike intelligence development[J]. Aerodynamic Missile Journal, 2019,(3): 45-49. (in Chinese)DOI: 10.16338/j.issn.1009-1319.20180322.
ZHAO Z P, LU R M, WANG J C, et al. Development and prediction on intelligent unmanned aerial vehicle technology[J]. Tactical Missile Technology, 2017(3): 1-7. (in Chinese)DOI: 10.16358/j.issn.1009-1300.2017.03.01.
LYU S J, YANG Y, HAN Z F. Research on the development of military helicopter intelligent and autonomous control technology[J]. Aeronautical Science Technology, 2020, 31(10): 36-40. (in Chinese)DOI: 10.19452/j.issn1007-5453.2020.10.006.
WU X M. Current status, development trend and countermeasure for high-speed rotorcraft[J]. Journal of Nanjing University of Aeronautics Astronautics, 2015, 47(2): 173-179. (in Chinese)DOI: 10.16356/j.1005-2615.2015.02.001.
ZHOU J L, DONG L H, YANG W D, et al. Closed-loop vibration control simulation of a helicopter active rotor with trailing-edge flaps based on the weighted-least-squares-error identification method[J]. Journal of Vibration and Shock, 2019, 38(4): 237-244. (in Chinese)DOI: 10.13465/j.cnki.jvs.2019.04.035.
LI P, ZHUANG K L, LI J. Review of Foreign Research on Helicopter Rotor Airfoil[J]. Helicopter Technique, 2007(3): 103-109. (in Chinese)
WU Y P, XI J. Control and load research of coaxial rigid rotor compound high speed helicopter[J]. Journal of Nanjing University of Aeronautics Astronautics, 2019, 51(2): 166-170. (in Chinese)DOI: 10.16356/j.1005-2615.2019.02.005.
XUE M, SUN Q. Tiltrotor military requirement and critical technology analysis[J]. Helicopter Technique, 2020(1): 47-49, 27. (in Chinese)
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