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)
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????? 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.
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Tab . 2 Cra sh velocit ies of a ircraft fu sela ge
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Case
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Verti cal velocity
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Horizontal velocity
VH Π(mΠs)
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Total velocity
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i g. 8 Post impact de orma tion o use lage ski n
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Fig. 9 Imp act force of different vertical velocities
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Fig. 11 Impact force of different horizontal velociti es
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Fig. 12 Maximum imp act force for horizontal velociti es
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Fig. 13 Subfloor acceleration curves for vert ical velocity
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Fig. 14 Maximum subfloor acceleration curve
for vert ical velocity
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Fig. 15 Subfloor acceleration curves for
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Fig. 16 Maximum subfloor acceleration curve for
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Fig. 17 Structure energy absorption percent
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17
40
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? 32 ?? 2? ???? : ?????????????????? 201
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