Advanced Search
Volume 42 Issue 2
Feb.  2016
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2016  >  42(2): 383-390.
LI Mengxiao, XIANG Jinwu, REN Yiru, et al. Evaluation and analysis method of aviation seat crashworthiness[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(2): 383-390. doi: 10.13700/j.bh.1001-5965.2015.0086(in Chinese)
Citation: LI Mengxiao, XIANG Jinwu, REN Yiru, et al. Evaluation and analysis method of aviation seat crashworthiness[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(2): 383-390. doi: 10.13700/j.bh.1001-5965.2015.0086(in Chinese)
shu

Evaluation and analysis method of aviation seat crashworthiness

doi: 10.13700/j.bh.1001-5965.2015.0086
  • 1.

    School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • 2. College of Mechanical and Vehicle Engineering, Hunan University, Changsha 410082, China

  • Received Date: 06 Feb 2015
  • Publish Date: 20 Feb 2016
    Abstract
  • In order to research the structural response characteristics of an aviation seat under crash scenarios, an evaluation and analytical method of aviation seat crashworthiness was proposed for a seat/occupant system. A finite element model of the seat was established based on actual seat geometry and reasonable simplifying assumptions, then the seat model was coupled with a 50th Hybrid Ⅲ multi-rigid-body dummy model. A crashworthiness simulation of this seat/occupant system was carried out according to airworthiness regulations which define dynamic impact test methods and qualification requirements for crew seats in general aviation aircraft in consideration of the cabin floor deformation. Seat deformations and energy-absorption, as well as occupant injury indicators under typical loading conditions were obtained. The results show that the seat/occupant system suffers more serious damage under forward and lateral loading, and the plastic deformation of the front seat beams increases when the backrest adjustment mechanism is too rigid. Cabin floor deformation aggravates seat structure damage. Compared with pitch deformation, roll deformation of the cabin floor causes greater damage. Modifications for the seat structure are proposed to improve its crashworthiness.

     

    • FullText(HTML)
  • loading
    • References(21)
  • [1]
    任毅如,向锦武,罗漳平,等.飞行器机身结构耐撞性分析与设计[J].工程力学,2013,30(10):296-304. REN Y R,XIANG J W,LUO Z P,et al.Crashworthiness analysis and design of aircraft fuselage structure[J].Engineering Mechanics,2013,30(10):296-304(in Chinese).
    [2]
    任毅如,向锦武,罗漳平,等.客舱地板斜撑杆对民机典型机身段耐撞性能的影响[J].航空学报,2010,31(2):271-276. REN Y R,XIANG J W,LUO Z P,et al.Effect of cabin-floor oblique strut on crashworthiness of typical civil aircraft fuselage section[J].Acta Aeronautica et Astronautica Sinica,2010,31(2):271-276(in Chinese).
    [3]
    郑建强,向锦武,罗漳平,等.民机机身下部结构耐撞性优化设计[J].航空学报,2011,32(4):640-649. ZHENG J Q,XIANG J W,LUO Z P,et al.Crashworthiness optimization of civil aircraft subfloor strcture[J].Acta Aeronautica et Astronautica Sinica,2011,32(4):640-649(in Chinese).
    [4]
    郑建强,向锦武,罗漳平,等.民机机身耐撞性设计的波纹板布局[J].航空学报,2010,31(7):1396-1402. ZHENG J Q,XIANG J W,LUO Z P,et al.Crashworthiness layout of civil aircraft using waved-plate for energy absorption[J].Acta Aeronautica et Astronautica Sinica,2010,31(7):1396-1402(in Chinese).
    [5]
    罗漳平,向锦武.直升机起落架抗坠毁性能的有限元仿真评估[J].航空学报,2003,24(3):216-219. 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).
    [6]
    何欢,陈国平,张家滨.带油箱结构的机身框段坠撞仿真分析[J].航空学报,2008,29(3):627-633. HE H,CHEN G P,ZHANG J B.Crash simulation of fuselage section with fuel tank[J].Acta Aeronautica et Astronautica Sinica,2008,29(3):627-633(in Chinese).
    [7]
    刘小川,郭军,孙侠生,等.民机机身段和舱内设施坠撞试验及结构适坠性评估[J].航空学报,2013,34(9):2130-2140. LIU X C,GUO J,SUN X S,et al.Drop test and structure crashworthiness evaluation of civil airplane fuselage section with cabin interiors[J].Acta Aeronautica et Astronautica Sinica,2013,34(9):2130-2140(in Chinese).
    [8]
    Federal Aviation Administration.Airworthiness standards:General aviation aircrafts:Title 14 code of federal regulations:14 CFR part 23[S].Washington,D.C.:Government Printing Office,1989:279-283.
    [9]
    中国民用航空局.中国民用航空技术标准规定:旋翼航空器、运输类飞机、正常类和实用类飞机座椅系统:CTSO-C127b[S].北京:中国民用航空局,2003:86-91. Civil Aviation Administration of China.Civil aviation technical standard orders of China:Seats in civil rotorcraft,transport aircraft,and general aviation aircraft:CTSO-C127b[S].Beijing:Civil Aviation Administration of China,2003:86-91(in Chinese).
    [10]
    Society of Automotive Engineers.Performance standard for seats in civil rotorcraft,transport aircraft,and general aviation aircraft:SAE AS 8049B-2005[S].Washington,D.C.:Society of Automotive Engineers,2005:23-27.
    [11]
    GALEA E R.Proposed methodology for the use of computer simulation to enhance aircraft evacuation certification[J].Journal of Aircraft,2006,43(5):1405-1413.
    [12]
    VEMULAKONDA G,TANG B R,JAYACHANDRAN R,et al.Approaches to modeling the dynamic interaction for an automotive seat and occupant system:SAE technical paper 2007-01-0988[R].Washington,D.C.:Society of Automotive Engineers,2007:3-5.
    [13]
    BHONGE P.A methodology for aircraft seat certification by dynamic finite element analysis[D].Wichita,Kansas:Wichita State University,2008:3-10.
    [14]
    DHOLE N E.Development and validation of a finite element model of a transport aircraft seat under part 25.562 dynamic test conditions[D].Wichita,Kansas:Wichita State University,2010:2-6.
    [15]
    ASTORI P,IMPARI F.Crash response optimisation of helicopter seat and subfloor[J].International Journal of Crashworthiness,2013,18(6):570-578.
    [16]
    邹建胜.民机坠撞环境下乘员座椅/约束系统仿真分析及优化[D].南京:南京航空航天大学,2011:1-8. ZOU J S.Dynamic simulation and detail optimization on occupant seat and restraint system of civil aeroplane[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2011:1-8(in Chinese).
    [17]
    HU D Y,ZHANG X.Full-scale crash test and FEM simulation of a crashworthy helicopter seat[J].Journal of Aerospace Power,2012,27(2):395-400.
    [18]
    HALLQUIST J O.LS-DYNA theory manual[Z/OL].California:Livermore Software Technology Corporation,2006(2014-06-25)[2015-01-20].http://ftp.lstc.com/anonymous/outgoing/jday/manuals/DRAFT_Theory.pdf.
    [19]
    TNO Automotive China.MADYMO theory manual[M/OL].Delft:Crash Safety Research Centre,2007-03-07(2013-06-01)[2015-01-20].http://www.doc88.com/p-7116111422634.html.
    [20]
    王宏雁,张丹.汽车座椅有限元建模与计算[J].同济大学学报(自然科学版),2004,32(7):947-951. WANG H Y,ZHANG D.Modeling and simulation with finite element method in vehicle seats[J].Journal of Tongji University(Natural Science),2004,32(7):947-951(in Chinese).
    [21]
    MARTIN B,BERNHARD S.Coupled simulation of multibody and finite element systems:An efficient and robust semi-implicit coupling approach[J].Archive of Applied Mechanics,2012,82(6):723-741.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(1093) PDF downloads(628) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return