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飞机机身结构非正常着陆耐撞性仿真分析

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飞机机身结构非正常着陆耐撞性仿真分析 飞 机 机 身 结 构 非 正 常 着 陆 耐 撞 性 仿 真 分 析 Ξ NUMERICAL SIMULATION OF CRASHWORTHINESS OF AN AIRCRAFT STRUCTURE ???1ΞΞ  ???1   ???2 (1 . ?????? ???? , ?? 710072) (2. ????????? , ?? 710089) YIN ZhiPing1  LI YuLong1  TAN ShenGang2 (1 . College of Aeronautics , Nort...

飞机机身结构非正常着陆耐撞性仿真分析
飞 机 机 身 结 构 非 正 常 着 陆 耐 撞 性 仿 真 分 析 Ξ NUMERICAL SIMULATION OF CRASHWORTHINESS OF AN AIRCRAFT STRUCTURE ???1ΞΞ  ???1   ???2 (1 . ?????? ???? , ?? 710072) (2. ????????? , ?? 710089) YIN ZhiPing1  LI YuLong1  TAN ShenGang2 (1 . College of Aeronautics , Northwestern Polytechnical University , Xi′an 710072 , China) (2 . The First Aircraft Institute , Xi′an 710089 , China) ??  ????????????? ,???????????? ,???????? CCAR223??????。? ?????????????????? ,???????????????? ,???????????????? ??、?????????????????????? ,????????????????????。???? , ????????????????? ,????????????? 。?????? ,????????????? ???????? ,??????????。 ???  ???  ???  ?????  ???? ?????  V223  TP391. 9  V215. 2 Abstr act  Under the abnormal landing , the aircraft structure must guarantee the safety of passengers according to China Civil Avi2 ation Regulations223(CCAR223) . For the first time , the crashworthiness model of some civil2aircraft fuselage structure is carried out. The influence of crash velocity has been taken into account. Under different crash velocity , the acceleration of floor , impact force , and energy absorption capability have been analyzed. Numerical results show that horizontal velocity influences the impact force , energy ab2 sorption , and acceleration of the floor. And some horizontal velocity is beneficial for crashworthiness of the aircraft structure . And these provide a reference for reliability design and evaluation of this aircraft. Key words Cra shwor thiness ; Dynamics ; Acceler ation of floor ; Impact for ce Corresponding author : YIN ZhiPing , E2mail : yzp @nwpu. edu . cn , Tel : Π Fax : +86229288492045 Manuscript received 20080521 , in revised form 20080705. 1  ?? ??????????? ,????????? ??????????? ,??????????? ?????。??????????23 ????、? ??、??????????? ( CCAR223) ???? ???????“????”??????? ,??? ?????????????????????? ? ,???????????????? ,????? ?????[ 1]。?? ,???????? ,???? ???????? ,?????????????? , ????????????????。 ???????????????????? ? ,??[ 2]????????????? ,???? ???????????????????? ,?? ?????????? ,???? ;???????? ??? ,?????????????。?? [ 3 ] [4 ]1132124??????????????????? ????? ,????????????????? ????? ,????????????????? ????????????????????? ,? ???[ 4]1462155???????????????? ????????。?????????????? ?????????????? ,???????? ?????????????? ,???????? ??????????????????。 ??????? ,????????????? ??????? ,??????????????? ????。?? ,??[ 526 ]??????????? ??????????? ;?? [ ]???????? Journa l of Mechanical Strength 2010 , 32(2) 1962201 Ξ ΞΞ ??? , ? , ? ?? , ??????? , ??。?? , ???? , ?????????????、????????????。 5 ???? , 5?????。 7 1977 12 20080 21 2008070 ??????????????????????? ??????? ;?? [8]???????????? ??????? ;?? [ 9 ]??????????? ? ,????????????????。?? [10 ] ???????????? ,?????????? ??????????。???????? ,??? ?????????????????? ,???? ?????????? ,???????????? ????????????????????。 ?????????? ,?????????? ???????????? ,?????????? ??????? ,??????????????? ?? ,???????????????????? ?????????? ,???????????? ??????? ,??????????????? ?????? ;???????????????? ??? ;??????????? ,???????? ?????????????????????? ?。 2  ?????????????? ???????????????????? ?[11 ]  [ M ] ?d + [ C] �d + [ K] d = F (1) ?? ,[ M ] ??????? ,[ C] ????? , [ K] ? ???? , ?d ???? ?? , �d ? ???? , d ????? , F ?????。 ????????????????????? ? ,?????????。???????????? ???? ,?? 1??。 ? 1 ????? Fig. 1  Master2slave contact surface ?????? ,?????????????? ?? ,??????( slave surface) ???????? ?? (master surface) ???? ;????????? ? ,??????????? ,??? ?????? ???? ,???????? ,????????? ? ,????????????????????? ?? ,??? (????) ???????。 ????????? ,??????????? ????????。???????????? ,?? ??????????????????????? ? ,?? 2 ?????????????。????? ??????? (master surface) ??????? ,? ?????“Both”??? ,?????? ,????? “Bottom”???????。 ? 2 ????????? Fig. 2  Hooking of slave surface ??? MSCΠDytran ??? ,????????? ??????????????。??? MSCΠDytran ????????????  t = α?0. 5 ?t1 + α?0. 5 ?t2 + G (2) ?? , t ????? ,α?“shell”???????? , t1 ????“shell”???? , t2 ????“shell”??? ? , G????????????。?????? 3 ? ?。 ? 3 ???????????? Fig. 3  Contact thickness between shell el ements ??4 ?? ,??????????????? ??????????? ,??????????? ??。???????? ,???????????? ????? ,????????????????? ????。 ? 4 ???????????? Fig. 4 Use of a contact thickness p revent s hooking 3  ??????????? ???????????????????? 5 ?? ,??????? Q ???? ,?????  ? 32 ?? 2? ???? : ?????????????????? 197   uad4 ?、????????????? ,???????? ?? 17 000 ??? ,14 000 ???。???????? ??? ?????????、????? ???? ???????、?? ??????????? ,? ???????????? ,?????????? ???????????。??????????? ?????? ,????? CCAR23???? 0. 5。 ? 5 ?????????????? Fig. 5 Finit e element model of aircraft fuselage ????????? ,??????????? ???2024??? ,???????????? ?? ? ,????????????????? ,???? ????? 1 ??。 ?1  2024??????? Tab . 1  Material pr opert ies of Alumin um 2024 ?? Material ???? Elasti c modulusΠPa ??? Poisson’s ratio ???? Yield stress ΠPa ?? Densi ty kg?m- 3 ?????? Maximum plasti c st rain Al2024 68. 95 ?109 0. 33 344. 74 ?106 2 770 0 . 15   ??????????????MSC.Dyt ran ? ????????????????。?????? ? PC ???? ,????? ,CPU Pentium2. 93 GHz , ?? 1Gb , ?? 120 Gb ,7 200 ?。???????? 1. 0 ?10- 7s ,????? 25 ms ,????????? 3 h。 ????????????????????? ?? ,???????? 2??。 ? 2 ???????????? Tab . 2  Cra sh velocit ies of a ircraft fu sela ge ??? Case ???? Verti cal velocity VV Π(mΠs) ???? Horizontal velocity VH Π(mΠs) ??? Total velocity V Π(m Πs) 10 10. 7 13. 4 17 . 1 20 10. 7 8. 0 13. 36 30 10. 7 4. 0 11. 42 40 10. 7 0. 0 10 . 7 3 5 6 6 3 6 3 3 3 3 3 55 4  ????????????? ????????????????????? ????? 6 ??。 ? 6 ????????????? Fig. 6  Imp act deformation of subfloor ? 7 ???????????? Fig. 7  Impact deformation of frame ?  ?????????????? F   f f f ????????????????????? ????? ,? 7 ??????????????? ????? ,??????????????? 310 mm ,????????????????????? ?????? ,???????????????? ????????。 ? 8 ????????????、?????? ??。?????????????? ,????? ????? ,?????????? ;??????? ?? ,???????????????????? ??? ,???????? ,??????????? ????。?????????????????? , ???????????????。 ????????????? ,???????  198 ?   ?   ?   ? 2010?   11 8. 0 1 . 4 1 . 1 12 . 0 1 . 4 14. 8 1 4. 0 1 . 4 1 . 98 14 2. 0 1 . 4 1 . 8 i g. 8 Post impact de orma tion o use lage ski n ??????????????????????? ?? ,?????????????????? ,?? ???????? ,?????????????? ?????????? ,??????????“?? ??”????????? ,? Y?。 ? 9 ?????????????? ,???? ???????????。??????“10”、“11”? ??????? 1 ????? ,Y?? Y???? ,? ?? 102Y???? 10? Y ?????? ,???? ??。 ? 9  ?????????????????? Fig. 9  Imp act force of different vertical velocities ? 10 ???????????????? Fig. 10  Maximum impact force for vertical veloci ties ????????????????????? ?? 10 ??。????????????????? ??????????????? ,??????? ????? ,??? 8 m Πs??????????? , ??? 8 m Πs?????????????。 ???????? ,???????10. 7 mΠs ,? ??????????????????????? ??? ,??? 10. 7 m Πs???????????? ?? ,????????????。 ? 11??????????????? ,??? ??????????????。 ?11????????? ,???????0? , ????????。?? 12 ?????? ,???? ????? ,??????? ;????? 0 ? ,?? ???????。??????????? ,???? ????????????????? ,??? ? ??????????? ,??????????? ???? ,??????????????????。 ? 11 ?????????????????? Fig. 11 Impact force of different horizontal velociti es ? 12 ???????????????? Fig. 12 Maximum imp act force for horizontal velociti es ????????????????????? ???? ,?????? 64 m Πs ? ,??????? ??????? 1 544 kN ,? 13. 4 m Πs ?????? ?。????????????? ,???????? ????。???????? , ??????? 13. 4 m Πs? ,?????? ,???????? ,?? ??????????????????????? ? ,??????????????? ,?????? ?????????? ,???????????? ????。 ????????????????? ,??? ??? 13、? 14、? 15、? 16 ??。 ? 13 ??????????????? Fig. 13  Subfloor acceleration curves for vert ical velocity ????????????????? ,??? ???????? ,?????????????致 , ????????????????????? ,? ? 3、? ?? ;???????????? ,??? ? 5、? 6 ??。??? Π ????????  ? 32?? 2 ? ???? : ?????????????????? 199   7 1 14 1 1 10. 7 m s ? 14 ????????????????? Fig. 14 Maximum subfloor acceleration curve for vert ical velocity ? 15 ??????????????? Fig. 15  Subfloor acceleration curves for horizontal velocity ? 16 ????????????????? Fig. 16  Maximum subfloor acceleration curve for horizontal velocity ???????1 300 mΠs2 ;??[ 12213] ? ,???? ???????????????? 2 600 m Πs2 ,? ?????????? 5 ,??????????? ??????? 520 m Πs2 。??????????? ? 2 ? ,????? 7 ??????? ,?????? ??????????????????????? ???? ,?????????????????? ?? ,???????????????????? ??????? ,????????????? ,?? ??????????????????????。 ? ?????????????????? ???????????????? ,?????? ? ,?? ???????????????? ,? ? 17 ?????????????????? Fig. 17  Structure energy absorption percent ? 14?????????。???????? ,?? ??????????? 25 ms ? , ?????? 90 %?? ,?????????????????。 ???? 17??????????? ,?????? ????? 25 ms? ,?? 20、?? 30、?? 40??? ??????????? ,?? 90 % ; ?? 10、?? 11、??12、??13、??14??????????? ????? ,????????????????? ??? ,???????????。???????? ??? , ????????? , ???????? 13. 4 mΠs? ,??????????????? ,?? ????? 25 ms。 5  ?? ??????????????? ,????? ???????????????????。??? ??????????????????? ,??? ??? ,???????? : 1) ???????????? ,??????? ????????????? ,????????? ??????????? ,???????? ,??? ???13. 4 mΠs? ,????????13. 4 mΠs?? ??。 2) ????????????????? ,?? ????????????? ,????????? ??????????????????????? ? ,????????????????????? ??。 3) ??????????????????? ????? ,????????????????? ???????????? ,?????????? ???????????? ,?????????? ????????? 13. 4 m Πs????、????。 ???? ( R f ) [ ] ?????? ????????? 3? ???、???、?   200 ?   ?   ?   ? 2010 ?   17 40 e er ences 1 . 2 : ?????????? : ? 23 . 561 ? : ? 23. 562 ? [S] . ?? : ?????? , 2003 : 51254. Civil Aviation Admini stration China. China civil aviation regulation223 (CCAR223) : No. 23. 561 : No . 562 [S]. Beijing : Civil Aviation Admin2 istration China , 2003 : 51254( In Chinese) . [ 2 ]  Hughes K. Application of the finite element method to predict the crash2 worthy response of a metallic helicopter under floor structure onto water [J ]. International Journal of Impact Engineering , 2007 , 12(1) : 1216. [ 3]   Edwin L. Best practices for crash modeling and simulation : NASAΠTM2 20022211944 [ R] . Vi rginia , U. S. : U. S. Army Research Laboratory Vehicle Technology Directorate Langley Research Center , 2002 : 48263. [ 4 ]  Alan Byar. A crashworthiness study of a Boeing 737 fuselage section[D ]. Philadelphia , U. S. : Drexel University , 2004 : 1132124 ; 2004 : 1462 155. [ 5 ]  ??? , ??? , ??? . ???????????????? ???[J ]. ?????? : ????? , 2005 , 33 (3) : 3662371 . LIU RuiTong , LIU J ianPing , TIAN HaoBin. Analysis method of compos2 ite materi al structure’s crashworthiness based on structural elements [J ] . Journal of Tongji University : Natural Science Edition , 2005 , 33 (3 ) : 3662371 ( In Chinese) . [ 6 ]  ??? , ??? , ??? , ?. ?????????????? ???????[J ]. ?????? , 2003 , 20(4) : 51257. NI XianPing , WANG YongLiang , J IA ShuPing , et al . Analysi s of crash impact behaviour of typical composite components of helicopter of bottom structure[J ] . Acta Materi al Composite Sinica , 2003 , 20 (4) : 51257 ( In Chinese) . [ 7]  ??? , ??? . ???????????????? [J ] . ? ??? , 2005 , 26 (5) : 2982302 . GONGJunJie , WANGXinWei . Numerical simulation of energy absorp2 tion capability of composite waved beams[J ]. Cata Aeronautica et Ast ro2 nautica Sinica , 2005 , 26 (5) : 2982302 ( In Chinese) . [ 8]  ??? , ??? . ??????????????????? [J ]. ???? , 2003 , 24 (3) : 2162219. LUO ZhangPing , XIANGJinWu. Crashworthiness performance evaluation to helicopter landing gear by finite element simulation[J ] . Cata Aeronau2 ti ca et Astronautica Sinica , 2003 , 24 (3) : 2162219 (In Chinese) . [ 9 ] ??? , ??? , ?  ? , ?. ?????????????? ?????????? ( Ⅰ) ????????? [J ]. ???? , 2002 , 23(1) : 23227. YANGJ iaLing , WU WeiHua , ZHAO Yan , et al . Energy absorbing ca2 pability of kneeling landing gear for new type armed heli copters during crash process( Ⅰ) : numerical simulation[J ] . Cata Aeronautica et Astro2 nautica Sinica , 2002 , 23 (1) : 23227 ( In Chinese) . [ 10 ]  ?  ? , ?  ? , ?  ? . ??????????????? [J ]. ???? , 2007 , 29 (5) : 7132716. LIU Fang , ZHAOMei , MENG Guang. Dynamic analysis of printed cir2 cuit board assembly subjected to drop impact [J ]. Journal of Mechanical Strength , 2007 , 29(5) : 7132716 (In Chinese) . [ 11 ]  MSCΠDytran. DYTRAN user’s manual [M ]. Los Angeles , California : The MacNeal Schwendler Corporation , 2000 : 1862205. [ 12 ]  Karen E. Impact testing and simulation of a crashworthy composit e fuse2 l age[ C]ΠΠAmerican Helicopter Society 56thAnnual Forum. Virginia : US Army Research Laboratory , 2000 : 2542267. [ 13]  Karen E. Crashworthy evaluation of a 1Π52scale model composite fuselage concept : NASAΠTM219992209132 [ R] . Virginia , U. S. : U. S. Army Research Laboratory Vehicle Technology Directorate Langley Research Center , 1999 : 1242142 .  ? 32 ?? 2? ???? : ?????????????????? 201  
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