Review of high-lift devices design for amphibious aircraft

ZHANG Qingyun; WANG Zhenghua; WEI Meng; LIN Wenjie

doi:10.7638/kqdlxxb-2017.0110

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Review of high-lift devices design for amphibious aircraft

更新时间：2026-05-28

- Review of high-lift devices design for amphibious aircraft
- Vol. 37, Issue 1, Pages: 19-32(2019)
- 作者机构：
  
  中国航空工业集团公司中航通飞研究院有限公司第一研究室,广东,珠海,519040
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2017.0110
  CLC： V221.3
- Published：2019
- 稿件说明：
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张庆云, 王峥华, 魏猛, 林文杰. 大型水陆两栖飞机增升装置特殊设计综述[J]. 空气动力学学报, 2019, 37(1): 19-32.

ZHANG Qingyun, WANG Zhenghua, WEI Meng, et al. Review of high-lift devices design for amphibious aircraft[J]. 2019, 37(1): 19-32.
张庆云, 王峥华, 魏猛, 林文杰. 大型水陆两栖飞机增升装置特殊设计综述[J]. 空气动力学学报, 2019, 37(1): 19-32. DOI： 10.7638/kqdlxxb-2017.0110.

ZHANG Qingyun, WANG Zhenghua, WEI Meng, et al. Review of high-lift devices design for amphibious aircraft[J]. 2019, 37(1): 19-32. DOI： 10.7638/kqdlxxb-2017.0110.

摘要

为掌握大型水陆两栖飞机增升装置工程设计的基本原理和主要技术，设计出满足较高气动力与水动力性能要求的高效增升装置，围绕两栖飞机增升装置的特殊设计方法开展了系统研究。通过对比分析两栖飞机与常规陆基飞机增升装置的技术特征与设计差异，在综合分析国内外典型两栖飞机增升装置的类型及设计特点的基础上，针对两栖飞机的快速性、喷溅性和抗浪性指标，对增升装置在使用和设计环节中相关影响要素进行了详细阐述。依据两栖飞机的使用环境以及使用要求，探讨了气动力与水动力耦合设计对两栖飞机增升装置的重要性，分析了水面喷溅、近水面效应、机构偏转限制等对增升装置的影响机理和影响规律，剖析了增升装置设计与抗浪指标的内在联系，对增升装置下偏量的选取方法给出建议。结合大量水动力、气动力试验和数值模拟数据，总结提炼出了与工程实际紧密结合的两栖飞机增升装置特殊设计原则。依据本文总结的设计方法完成的增升装置方案，已成功应用于我国正在研制的某大型水陆两栖飞机。通过风洞及水动力试验验证，结果表明该飞机越过阻力峰后未发生主喷溅冲击增升装置的现象，耐波性预报表明该飞机的抗浪能力满足预定的技术要求，从而进一步验证了本文提出的增升装置设计思路和设计方法的可行性，且具有较强的工程应用价值，可为两栖飞机增升装置的设计提供可靠的设计参考。

Abstract

Amphibious aircraft studies are inadequate in domestic. Systematic technical guidance is insufficient regarding the high-lift devices of amphibious airplane. In order to grasp the basic principle and design technology for the high-lift devices of amphibious aircraft

which satisfy the aerodynamic and hydrodynamic design requirement

special design methods have been systematically investigated in this paper. Technical characteristics and design features are compared between amphibious aircraft and land-based aircraft based on domestic and international high-lift device types and design features. On the basis of the special operating environment

operating mode

and hydrodynamic characteristics of amphibious aircraft

various factors affecting the designing of high-lift devices of amphibious aircraft are discussed for the first time. These factors include splash

wave-resistance

and so forth. The high-lift device designs for amphibious aircraft should meet the general design principles of land-based aircraft

and satisfy the special technical requirement of aquatic environment and operating mode. The aerodynamic configuration of amphibious aircraft is closely related to hydrodynamic configuration. The design of high-lift devices for amphibious aircraft is significant different from that for land-based aircrafts. The main sensitive parameters in the design progress of high lift system are pointed out

and the correlation is discussed between trailing-edge high-lift devices design and anti-waves capability. Finally

some suggestions are given for the design principles of the high-lift devices of amphibious aircraft.Based on a lot of water/wind tunnel tests and CFD results of hydrodynamic/aerodynamic characteristics one high performance flap scheme of a civil large amphibian aircraft has been developed according to the present design principle.A water tunnel test shows that

there is no splash on the high-lift devices

and the airplane has the ability in resisting given height wave. This design is completed by solving the contradiction between aerodynamic configuration and hydrodynamic configuration.The design principle of high-lift devices for amphibious aircraft summarized in this paper is feasible

and has a high application worth. Moreover

it can be used as a reference material of the amphibious aircraft high-lift devices design.

关键词

Keywords

references

孙湘平.中国沿岸海洋水文气象概况[M].北京:科学出版社, 1981.

张磊, 王辉, 蔡东明, 等.中国近海海浪分布特征的初步分析[C]//中国航海学会, 海洋船舶驾驶专业委员会, 海浪与船舶航行安全及防抗台风经验研讨会论文集. 1998.

邵利民.海浪的形成和海浪等级[C]//防止船舶行事故新经验新技术学术研讨会论文集(下册). 2004.

陈登俊.航海气象学与海洋学[M].北京:人民交通出版社版, 2009.

方钟圣.西北太平洋波浪统计集[M].北京:国防工业出版社, 1996.

海军航空兵司令部翻译室翻译.水上飞机的流体力学[M].北京:航空工业出版社, 2010.

SUN J J, MA D L. Resistance evaluation for flying boats sliding at medium and high speed in calm water[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5):925-929. (in Chinese)

ZHU Y G, FAN G L, YI J Q. Modeling longitudinal aerodynamic and hydrodynamic effects of a flying boat in calm water[C]//Proceedings of the IEEE International Conference on Mechatronics and Automation. 2011.

李云波.船舶阻力[M].哈尔滨:哈尔滨工程大学出版社, 2006.

QIU L J. Integrated aerodynamic and hydrodynamic optimization of amphibious aircraft[D]. Shanghai: Shanghai Jiaotong University, 2013. (in Chinese)

《飞机设计手册》总编委会.飞机设计手册[M].第5册民用飞机总体设计.北京: 航空工业出版社, 2005.

《飞机设计手册》总编委会.飞机设计手册[M].第6册气动设计.北京: 航空工业出版社, 2002.

EGBERT Torenbeek. Analysis and optimization of subsonic civil airplanes[M]. Beijing: Aviation Industry Press, 2016.

方宝瑞, 李天, 余松涛.飞机气动布局设计[M].北京:航空工业出版社, 1997.

余雄庆, 徐惠民, 昂海松.飞机总体设计[M].北京:航空工业出版社, 2000.

李洪畴.水轰5型反潜巡逻水上飞机的设计特点[J].飞机设计, 1989, 3:6-14.

《飞机设计手册》总编委会.飞机设计手册[M].第4册军用飞机总体设计.北京: 航空工业出版社, 2005.

美国军用标准手册题录[J].世界标准信息. 1995, 4: 29-35.

美国海军规范MIL-T-7791.水机、飞船、水陆两栖飞机的拖曳和系留装置设计和安装[S].美国国家标准协会. 1954.

美国海军规范MIL-T-81259, 拴系接头——结构设计要求[S].美国国家标准协会. 2016.

美国海军规范MIL-T-8677(1), 海军飞机火控系统及其有关设备的安装[S].美国国家标准协会. 1978.

美国海军规范MIL-H-8661, 船身、辅助浮筒和上下水装置的设计和制造[S].美国国家标准协会. 1971.

美国海军规范MIL-STD-805, 固定翼飞机乘员位置的控制和显示装置[S].美国国家标准协会. 1987.

QU D C. Russia's Be-200 multi-pulfi-purpose amphibious seaplane[J]. Aeronautical Science and Technology. 2005, 1:28-30.

凌志勤.多用途水陆两用飞机别-200[J].国际航空, 1993(10):13-14.

Jane's all the world aircraft[M]. 1992.

王武红, 兰芝芳.加拿大CL-215型水陆两用灭火机[J].民用飞机, 1988, 2:14-33.

TAYLOR, JOHN W R. Jane's all the world's aircraft[M]. Jane's Yearbooks, 1976.

SURHONE L M, TENNOE M T, HENSSONOW S F. Bombardier 415[M]. Betascript Publishing. 2010.

EVANS, DAVID C, PEATTIE, et al. Strategy, tactics and technology in the imperial Japanese navy[M]. Annapolis, Maryland:Naval Institute Press, 1997.

ANDERSON S B. An examintaion of handling qualities criteria for V/STOL aircraft[R]. NASA TND-331, 1960.

Buweps Confidential Letter RAAD-3/63[J]. GLD serial 04223 of 2 Oct 1963.

Shin Meiwa Ss-2A stol amphibious aircraft[R]. Shin Meiwa Industry CO., LTD. 1972.

HOLZHAUSER C A, DECKERT W H, QUIGLEY H C, et al. Design and operating considerations of commercial STOL transports[J]. AIAA J, 1965, 2(2):87-93.

山本宣夫. STOL飞行艇の自动推力制御装置による着水アプローチ[J].日本航空宇宙学会志, 1983, 31(349):103-109.

Naval Air Test Center Technical report, Final Report Flight Test Evalutation of'the Uf-Xs Japanese Stol Seaplane (U)[R]. LCDR Nicholasj. Vagianos, USN MrEu eneC. Rooney, FT2121-031R-64, 1968.

中国人民解放军第六O五研究所情况组.外国水上飞机汇编[G]. 1970.

Shin Meiwa PS-1/US-1. Japan's BigBoat by David Donald[J]. World Airpower Journal, 1993, 15:126-133.

王专孝、李七云.日本PS-1/US-1的研制、生产与使用[M].航空工业出版社.水上飞机文集, 2011.

日本海上自卫队US-1A改进型水上飞机[J].现代兵器, 2003, 8:22-23.

第三机械工业部第六O五研究所技术图书馆. PS-1水上飞机飞行手册[R]. 1978.

第三机械工业部第六O五研究所技术图书馆.水上救护机US-1(PS-1改型)型号说明书[R]. 1975.

T Ishizaki. The livery design for prototype US-2 search and rescue amphibian[J]. Annual Design Review of Japanese Society, 2005, 10:16-19

SOBIECZKY H. Parametric airfoils and wings[J]. Noteon Numerical Fluid Mechanics, 1998, 68(1):71-88.

CHU L T. Seaplane hydrodynamic design[M]. Beijing: Aviation Industry Press, 2014.(in Chinese)

邱大洪.波浪理论及其在工程上的应用[M].北京, 高等教育出版社, 1985.

吴秀恒.船舶操纵性与耐波性[M].北京, 人民交通出版社, 1999.

李麟, 李效东.气象仪器与观测方法指南[M].气象出版社, 1992.

LING H J. Research of spray characteristics and real time numerical prediction of the motion response of high speed planing craft[D]. Jiangsu University of Science and Technology, 2013. (in Chinese)

LU G X, ZHOU D J. Investigation in aerohydro dynamic characters of WIG[J]. Experiments and Measurements in Fluid Mechanics, 1997, 4:18-22. (in Chinese)

盛振邦, 刘应中.船舶原理[M].上海交通大学出版社, 2005.

BENEDICT K, KORNEV N, MEYER M, et al. Complex mathematical model of the WIG motion including the take-off mode[J]. Ocean Engineering, 2002, 29:315-357.

REMINGTON W. The canadair CL-215 amphibious aircraft-development and applications[R]. AIAA-89-1544CP.

顾诵芬, 崔尔杰.填补运输效率的黄金空白——地面效应原理与地效飞行器[J].现代军事, 2005, 3:10-11.

SUN R M. Experimental investigation on aerodynamics characteristics and tip vortices of a wing in ground effect[D]. Shanghai University, 2011.

GRATZER L B, MAHAL A S. Ground effects in STOL operation[J]. Journal of Aircraft, 1971, 19(3):236-242.

STEINBACH D, JACOB K. Some aerodynamic aspects of wings near ground[J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 1991, 34(104):56-70.

SMITH A M O. High lift aerodynamics[J]. Journal of Aircraft, 1975, 12(6):501-530.

PARKINSON, JOHN B, OLSON, et al. Aerodynamic and hydrodynamic tests of a family of models of flying boat hulls derived from a streamline body-NACA, Model 84 Series[R]. NACA REPORT 766, 1943

GJB 67. 5A-2008.军用飞机结构强度规范[S].第5部分: 水上飞机的水载荷. 2008.

中国航空百科词典[M].航空工业出版社, 2000.

ANDERSON J D. Fundamentals of aerodynamics[J]. AIAA Journal, 2007, 48:2983-2983.

(俄)比施根斯, (俄)Г. С. Бюшгенс, 姜育义.干线飞机空气动力学和飞行力学[M].航空工业出版社, 1996.

INGO D, MANRICO L. Hydrodynamic characteristics of seaplanes affected by hull shape parameters[R]. AIAA 1989-1540.

WEI C, ZHANG T J, LIU T Z. Multi-objective optimization of fowler flap on general aircraft[J]. Acta Aerodynamica Sinica, 2017, 35(4):572-578.(in Chinese)

ZHU G L, WANG K C, JIN G, et al. The calculation of aerodynamic characteristics for high lift devices of airplane[J]. Acta Aerodynamica Sinica, 2001, 19(2):148-155.(in Chinese)

LOCKE F W S, HELEN L. A method for making quantitative studies of the main spray characteristics of flying boat hull models[J]. NACA-ARR-3K11, 1943, (3):253-256.

HAMILTON J, ALLEN J E. Seaplane research-the MAEE contributions[J]. The Aeronautical Journal, 2003, 107(1069):125-148.

TANG B B, WU B, WANG M Z, et al. Comparative test study for the effect of groove type spray suppressor widths on amphibious aircraft spray performance[J]. Aeronautical Science Technology, 2015, 1:73-79. (in Chinese)

张宝吉, 船舶静力学[M].上海:上海交通大学出版社, 2016.

蔡岭梅, 王兴权.船舶静力学[M].北京:人民交通出版社, 1995.

HOLZHAUSER C A, INNIS R C, VOMASKE R F. A flight and simulator study of the handling qualities of a deflected slipstrea STOL seaplane having four propellers and boundary-layer contril[R]. NASA TN D-2966, 1965.

JIAO Y Q, CHEN Y Q, JIN C X. Wind tunnel experimental research on lift enhancing mechanism of jet on wing of aircraft[J]. Journal of Experiments in Fluid Mechanics, 2008, 22(2):20-24. (in Chinese)

WANG J J, LI Y C, CHOI K S. Gurney lap-lift enhancement, mechanisms and applications[J]. Progress in Aerospace Sciences, 2008, 44(1):22-47.

KORBACHER G K. Aerodynamics of powered high-lift system[J]. Annual Review of Fluid Mechanics, 2003, 6(6):319-358.

GRIFFIN H A, GONNZALEZ L F, SHRINIVAS K. Computational fluid dynamics analysis of externally blown flap configuration for transport aircraft[J]. Journal of Aircraft, 2008, 45(1):172-184.

ONES G S, VIKEN S A. An active flow circulation controlled flap concept for general aviation aircraft applications[R]. AIAA 2002-3157.

ALEJANDRA Uranga. Boundary layer ingestion benefit of the D8 transport aircraft[J]. AIAA J, 2017, 55(11):3693-3708.

ANDERSON S B. An examination of handling qualities criteria for V/STOL aircraft[R]. NASA TN D-331, 1960.

WEN J. Exterior blowing augmentor wing in NASA Langley research center (part seven)[J]. International Aviation, 2007, 7:64-68. (in Chinese)

SLOTNICK J P. Navier-Stokes analysis of a high wing transport high-lift configuration with externally blown flaps[R]. AIAA 2000-4219.

MARCOS J. Computational and experimental comparison of a powered lift upper surface blowing configuration[J]. AIAA Journal, 2010, 502:1-19.

SLOTNICK J P. Navier-Stokes analysis of a high wing transport high-lift configuration with externally blown flaps[R]. AIAA-2000-4219.

Amphibious aerial fire fighting and maritime search and rescue aircraft[G]. Operations and Design Consideration Training Course China Aviation Industry General Aviation Co. Ltd. 2011, 9.

KUHN R E. Semi-empirical procedure forestimating lift and drag characteristics of propeller-wing-flap configurations for vertical and short take off and landing airplanes[R]. NASA Memo-1-16-59L, 1959.

PARLETT L P. Wind-tunnel investigation of a large jet transport model equipped with an external-flow jetflap[R]. NASA-1968-4928.

PARLETT L P, Shivers J P. Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap[R]. NASA-1969-5364.

PARLETT L P, FREEMAN D C. Wind-tunnel investigation of a jet transport airplane configuration with high thrust-weight ratio and an external-flow jet flap[R]. NASA-1970-6058.

AOYAGI K, FALARSKI M D, KOENIG D G. Wind tunnel investigation of a large scale 25 deg swept-wing jet transport model with an external blowing tripple slotted flap[R]. NASA-1973-62197.

BARBERIE F J, WICK A T, HOOKER J R. Low speed powered lift testing of atransonic cruise efficient STOL military transport[R]. AIAA 2013-1099.

WILIAMS J, BUTLER S F J. Wood M N. The aerodynamic of jet flaps: R MNo 3304[R]. London: Her Majesty's Stationery Offices, 1963.

航空工业部605所.日本短距起落水上飞机吹气附面层控制系统的设计[J].水上飞机设计研究, 1975, 8(2):12-16.

DAI S Z, DONG J H. A study of externally blowing powered lift technique for application to large transport[J]. Aeronautical Science Technology, 2006, 2:33-37. (in Chinese)

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