Volume 36 Issue 6
Jun.  2021
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HUANG Mingqi, XU Dongxia, HE Long, ZHU Qinghua, WANG Liangquan. Development overview and key technologies of high speed hybrid helicopter with single main rotor[J]. Journal of Aerospace Power, 2021, 36(6): 1156-1168. doi: 10.13224/j.cnki.jasp.2021.06.004
Citation: HUANG Mingqi, XU Dongxia, HE Long, ZHU Qinghua, WANG Liangquan. Development overview and key technologies of high speed hybrid helicopter with single main rotor[J]. Journal of Aerospace Power, 2021, 36(6): 1156-1168. doi: 10.13224/j.cnki.jasp.2021.06.004
shu

Development overview and key technologies of high speed hybrid helicopter with single main rotor

doi: 10.13224/j.cnki.jasp.2021.06.004
  • 1.

    Rotor Aerodynamics Key Laboratory,Low Speed Aerodynamics Institute,China Aerodynamics Research and Development Center,Mianyang Sichuan 621000,China

  • 2.

    National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics,College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China

  • Received Date: 2020-09-29
  • Publish Date: 2021-06-28
    Abstract
  • The development and key technologies of high speed hybrid helicopter with single main rotor were reviewed. Firstly, the general concept about the layout type and control mode of high speed hybrid helicopter with single main rotor was briefly introduced. Then, the high speed hybrid helicopters with single main rotor were divided into three configurations based on their own forward flight power structure features. At the same time, the layout of different configurations and their development situations were described respectively. And on this basis, according to the present problems faced by high speed hybrid helicopter with single main rotor, the key technologies such as the overall layout design and optimization, transition mode control and distribution design were summarized and sorted out. Lastly, combined with the development trend of high speed helicopter at home and abroad and the characteristics of helicopter with this configuration, the development prospect of high speed hybrid helicopter with single main rotor was analyzed and some preliminary suggestions on its development in our country were put forward.

     

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  • [1]
    王适存.直升机空气动力学［M］.南京:航空专业教材编审组,1985:127-129.
    [2]
    黄明其.直升机风洞试验［M］.北京:国防工业出版社,2014:1-3.
    [3]
    王焕瑾,高正.高速直升机方案研究［J］.飞行力学,2005,23(1):38-42. WANG Huanjin,GAO Zheng.Research on the scheme of a high speed helicopter［J］.Fight Dynamics,2005,23(1):38-42.(in Chinese)
    [4]
    吴希明.高速直升机发展现状、趋势与对策［J］.南京航空航天大学学报,2015,47(2):173-179. WU Ximing.Current status,development trend and countermeasure for high-speed rotorcraft［J］.Journal of Nanjing University of Aeronautics and Astronautics,2015,47(2):173-179.(in Chinese)
    [5]
    李建波.复合式直升机技术发展分析［J］.南京航空航天大学学报,2016,48(2):149-158. LI Jianbo.Progress of compound helicopter technology［J］.Journal of Nanjing University of Aeronautics and Astronautics,2016,48(2):149-158.(in Chinese)
    [6]
    ORCHARD M N,NEWMAN S J.The compound helicopter:why we have not succeeded before?［J］.Aeronautical Journal,1999,103(1028):489-495.
    [7]
    ORCHARD M,NEWMAN S.The fundamental configuration and design of the compound helicopter［J］.Journal of Aerospace Engineering,2003,217(6):297-315.
    [8]
    TANABE Y,AOYAMA T,KOBIKI N,et al.A conceptual study of high speed rotorcraft［R］.Southampton,UK:The European Rotorcraft Forum International Committee,2014.
    [9]
    TANABE Y,SUGIURA M,KOBIKI N,et al.A new concept of compound helicopter and flight tests［C］∥The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology.Tokyo,Japan:Japan Aerospace Exploration Agency,2018:1343-1352.
    [10]
    RUSSELL C,JOHNSON W.Exploration of configuration options for a large civil compound helicopter［R］.Phoenix,USA:The American Helicopter Society International Incorporation,2013.
    [11]
    吴希明.直升机技术现状、趋势和发展思路［J］.航空科学技术,2012(4):13-16. WU Ximing.Status,trend and strategy of helicopter technology［J］.Aeronautical Science and Technology,2012(4):13-16.(in Chinese)
    [12]
    朱.俄罗斯资助新型高速直升机研发［J］.直升机技术,2011(2):19.
    [13]
    吕春雷,朱璟,黄利.突破直升机速度极限［J］.航空制造技术,2014(19):34-37. Lv Chunlei,ZHU Jing,HUANG Li.Break limit of helicopter speed［J］.Aeronautical Manufacturing Technology,2014(19):34-37.(in Chinese)
    [14]
    COLUCCI F.Paying for speed:faster vertical lift comes at a price,but high-speed rotorcraft have to pay off with greater productivity［J］.Vertiflite,2014,60(3):44-48.
    [15]
    EDI P,YUSOFF N,YAZID A A.New design approach of compound helicopter［J］.Wseas Transactions on Applied and Theoretical Mechanics,2008,3(9):799-808.
    [16]
    HIRSCHBERGM.The battle of the compound is joined［J］.Vertiflite,2010,56(4):16-22.
    [17]
    FOURNIER D.Airbus helicopter X3 flight tests:overview of X3 flight test phase and perspectives for the RACER airbus demonstrator［R］.Mailand,Italian:The European Rotorcraft Forum International Committee,2017.
    [18]
    莫雳.高速直升机技术日趋成熟——专访欧洲直升机X-3项目经理让·范肯［J］.环球飞行,2012(8):48-49.
    [19]
    招启军,倪同兵,李鹏,等.倾转旋翼机流动机理及气动干扰特性试验［J］.航空动力学报,2018,33(12):2900-2912. ZHAO Qijun,NI Tongbing,LI Peng,et al.Experiment on flow mechanism and aerodynamic interaction characteristics of tilt-rotoraircraft［J］.Journal of Aerospace Power,2018,33(12):2900-2912.(in Chinese)
    [20]
    袁明川,刘平安,樊枫,等.共轴刚性旋翼气动干扰特性风洞试验研究［J］.南京航空航天大学学报,2019,51(2):257-262. YUAN Mingchuan,LIU Ping’an,FAN Feng,et al.Wind tunnel test investigation of coaxial rigid rotor aerodynamic interaction［J］.Journal of Nanjing University of Aeronautics and Astronautics,2019,51(2):257-262.(in Chinese)
    [21]
    王畅,黄明其,彭先敏,等.分离式共轴刚性旋翼风洞试验技术研究［J］.南京航空航天大学学报,2019,51(2):194-200. WANG Chang,HUANG Mingqi,PENG Xianming,et al.Separating test technology of coaxial rigid rotor wind tunnel［J］.Journal of Nanjing University of Aeronautics and Astronautics,2019,51(2):194-200.(in Chinese)
    [22]
    吴希明.共轴刚性旋翼空气动力学问题与研究进展［J］.南京航空航天大学学报,2019,51(2):137-146. WU Ximing.Aerodynamic problems and research progresses of rigid coaxial rotor［J］.Journal of Nanjing University of Aeronautics and Astronautics,2019,51(2):137-146.(in Chinese)
    [23]
    张啸迟,万志强,章异嬴,等.旋翼固定翼复合式垂直起降飞行器概念设计研究［J］.航空学报,2016,37(1):179-192. ZHANG Xiaochi,WAN Zhiqiang,ZHANG Yiying,et al.Conceptual design of rotary wing and fixed wing compound VTOL aircraft［J］.Acta Aeronautica et Astronautica Sinica,2016,37(1):179-192.(in Chinese)
    [24]
    赵寅宇,黎鑫,史勇杰,等.双拉力螺旋桨构型复合式高速直升机旋翼/螺旋桨干扰流场分析［J］.南京航空航天大学学报,2017,49(2):154-164. ZHAO Yinyu,LI Xin,SHI Yongjie,et al.Analysis on rotor-propellers interaction flowfield for compound double-thust-propeller high-speed helicopters［J］.Nanjing University of Aeronautics and Astronautics,2017,49(2):154-164.(in Chinese)
    [25]
    蒋鸿翔,徐锦法,高正,等.新型复合式无人直升机悬停/着陆控制［J］.航空学报,2008,29(增刊1):46-54. JIANG Hongxiang,XU Jinfa,GAO Zheng,et al.Hover/landing control for the novel compound unmanned aerial helicopter［J］.Acta Aeronautica et Astronautica Sinica,2008,29(suppl.1):46-54.(in Chinese)
    [26]
    王俊超.ZX-1型旋翼机高速型总体方案设计研究［D］.南京:南京航空航天大学,2010. WANG Junchao.Research onpreliminary design of ZX-1 type autogiro high-speed scheme［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2010.(in Chinese)
    [27]
    NEWMAN S.The compound helicopter and the helicopter speed trap［J］.Aircraft Engineering and Aerospace Technology,1997,69(5):407-413.
    [28]
    ORCHARD M,NEWMAN S.Some design issues for the optimisation of the compound helicopter configuration［R］.Beach,USA:The American Helicopter Society International Incorporation,2000.
    [29]
    ROBBR L.Hybrid helicopters:compounding the quest for speed［J］.Vertiflite,2006,52(2):30-54.
    [30]
    陈石卿.高速混合型直升机［J］.航空科学技术,2011(2):15. CHEN Shiqin.High-speed hybrid helicopter［J］.China Aeronautical Science and Technology,2011(2):15.(in Chinese)
    [31]
    DUBOIS T.Eurocopter X3 demonstrator targets 220 knots［J］.Rotor and Wing Magazine,2010(11):14-15.
    [32]
    HIRSCHBERG M.X3 completes U.S.demo tour［J］.Vertiflite,2012,58(5):12-14.
    [33]
    PERRY T D.X3 retires with record-breaking flight［J］.Flight International,2013(6):12.
    [34]
    FERRIER J.Hybrid helicopter that is fast and has long range:US 2010/0065677 A1［P］.2010-03-18.
    [35]
    BLACHA M,FINK A,EGLIN P,et al.“CLEAN SKY 2”:exploring new rotorcraft high speed configurations［R］.Mailand,Italian:The European Rotorcraft Forum International Committee,2017.
    [36]
    BUTTERWORTH-HAYES P.Europe prepares for clean sky 2 research［J］.Aerospace America,2014,52(7):6.
    [37]
    FINKA.Compound helicopter:EP 2690011 B1［P］.2014-01-29.
    [38]
    ROESCH P.Fast hybrid helicopter with long range:US 8113460 B2［P］.2008-12-04.
    [39]
    FRADENBURGH E A,CHUGA G M.Flight program of the NH-3A research helicopter［J］.Journal of the American Helicopter Society,1968,13(1):44-62.
    [40]
    Piasecki Aircraft.16H-1 Pathfinder［EB/OL］.［2020-09-20］.http:∥piasecki.com/wp-content/uploads/2018/12/16H-1-Pathfinder.pdf.
    [41]
    Piasecki Aircraft.16H-1A Pathfinder Ⅱ［EB/OL］.［2020-09-20］.http:∥piasecki.com/wp-content/uploads/2018/12/16H-1A-Pathfinder Ⅱ.pdf.
    [42]
    COLUCCI F.Speed Hawk-Phase I［J］.Vertiflite,2007,53(4):18-22.
    [43]
    倪先平.俄罗斯直升机工业再展宏图［J］.国际航空,2008(9):70-73. NI Xianping.Russian helicopter industry in reforming［J］.International Aviation,2008(9):70-73.(in Chinese)
    [44]
    RAND O,KHROMOV V.Compound helicopter:insight and optimization［J］.Journal of the American Helicopter Society,2015,60(1):1-12.
    [45]
    YEO H,JOHNSON W.Aeromechanics analysis of a compound helicopter［R］.Phoenix,USA:The American Helicopter Society International Incorporation,2006.
    [46]
    YEO H,JOHNSON W.Optimum design of a compound helicopter［J］.Journal of Aircraft,2006,46(4):1210-1229.
    [47]
    LIENARD C,DIN I S E,RENAUD T,et al.RACER high-speed demonstrator:tail unit vertical fin aerodynamic design［R］.Phoenix,USA:The American Helicopter Society International Incorporation,2018.
    [48]
    孔卫红.复合式高速直升机若干关键技术研究［D］.南京:南京航空航天大学,2011. KONG Weihong.Research on some key technical issues of compound high speed helicopter［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2011.(in Chinese)
    [49]
    FERGUSON K,THOMSON D.Manoeuvrability assessment of a hybrid compound helicopter configuration［R］.Southampton,UK:The European Rotorcraft Forum International Committee,2014.
    [50]
    曹飞,陈铭,田力,等.复合式直升机过渡飞行功率特性［J］.航空动力学报,2016,31(2):413-420. CAO Fei,CHEN Ming,TIAN Li,et al.Power characteristics of the compound helicopter in transition flight mode［J］.Journal of Aerospace Power,2016,31(2):413-420.(in Chinese)
    [51]
    何晓萍,韩东,杨克龙,等.基于双螺旋桨推进的复合式直升机飞行性能［J］.航空动力学报,2020,35(4):815-822. HE Xiaoping,HAN Dong,YANG Kelong,et al.Flight performance of compound helicopter with twin propeller［J］.Journal of Aerospace Power,2020,35(4):815-822.(in Chinese)
    [52]
    STOKKERMANS T,VOSKUIJL M,VELDHUIS L,et al.Aerodynamic installation effects of lateral rotors on a novel compound helicopter configuration［R］.Phoenix,USA:The American Helicopter Society International Incorporation,2018.
    [53]
    LIENARD C,DIN I S E,RENAUD T,et al.RACER high-speed demonstrator:rotor and rotor-head wake interactions with tail unit［R］.Phoenix,USA:The American Helicopter Society International Incorporation,2018.
    [54]
    WENTRUP M,YIN J,KUNZE P,et al.An overview of DLR compound rotorcraft aerodynamics and aeroacoustics activities within the CleanSky2 NACOR project［R］.Phoenix,USA:The American Helicopter Society International Incorporation,2018.
    [55]
    万佳,陈铭.机翼位置对复合式直升机旋翼-机翼干扰的影响［J］.北京航空航天大学学报,2009,35(5):519-522. WAN Jia,CHEN Ming.Influence of wing location on rotor-wing interaction of compound helicopter［J］.Journal of Beijing University of Aeronautics and Astronautics,2009,35(5):519-522.(in Chinese)
    [56]
    申遂愿,朱清华,朱振华,等.高速直升机旋翼/螺旋桨/机身干扰特性分析［J］.航空工程进展,2020,11(1):46-55.
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