ๆญฏ์กธ์—…๋…ผ๋ฌธ_์œ ์„ฑ์šฉ.PDF



Similar documents
์ •๋ด‰์ˆ˜.PDF

ๆญฏ95_dbtech.PDF

ๆญฏ320.PDF

์†ก๋™์šฐ.PDF

Microsoft Word - KSR2013A320

๋ณด๊ด€๋ณธ.PDF

์ตœ์ข…์šฑ.PDF

ๆญฏ PDF

( )๋ฐ•์šฉ์ฃผ97.PDF

ๆญฏPLSQL10.PDF

๊ฒ‰ํ‘œ์ง€.PDF

ๆญฏ๋…ผ๋ฌธ์†๊ทœ๋งŒ.PDF

๋…ผ๋ฌธ์ˆ˜์ •๋ณธ.PDF

12(4) 10.fm

No Title

๊ณต์ฒญํšŒ์ž๋ฃŒ(์ตœ์ข…).PDF

์ˆ˜ํƒ์—ฐ๊ตฌ01-09(์ˆ˜์š”์ž ์ค‘์‹ฌ1).hwp

PDF

(3) () () LOSS LOSS LOSS LOSS (4) = 100 = 100 = 100 = 100 = 100 = 100 = 100 = 100 = 100 = 100 = 100 = 100

THE JOURNAL OF KOREAN INSTITUTE OF ELECTROMAGNETIC ENGINEERING AND SCIENCE Jun.; 27(6),

<353920C0B1B1E2BFEB2DB0E6B0F1C0DCB1B320BBF3BACEB1B8C1B6C0C720C8DA2E687770>

๊ธฐ๋Šฅ.PDF

์ด์ˆ˜์ง„.PDF

Alloy Group Material Al 1000,,, Cu Mg 2000 ( 2219 ) Rivet, Mn 3000 Al,,, Si 4000 Mg 5000 Mg Si 6000, Zn 7000, Mg Table 2 Al (%

PDF

08.hwp

์ €์ž‘์žํ‘œ์‹œ - ๋น„์˜๋ฆฌ - ๋ณ€๊ฒฝ๊ธˆ์ง€ 2.0 ๋Œ€ํ•œ๋ฏผ๊ตญ ์ด์šฉ์ž๋Š”์•„๋ž˜์˜์กฐ๊ฑด์„๋”ฐ๋ฅด๋Š”๊ฒฝ์šฐ์—ํ•œํ•˜์—ฌ์ž์œ ๋กญ๊ฒŒ ์ด์ €์ž‘๋ฌผ์„๋ณต์ œ, ๋ฐฐํฌ, ์ „์†ก, ์ „์‹œ, ๊ณต์—ฐ๋ฐ๋ฐฉ์†กํ• ์ˆ˜์žˆ์Šต๋‹ˆ๋‹ค. ๋‹ค์Œ๊ณผ๊ฐ™์€์กฐ๊ฑด์„๋”ฐ๋ผ์•ผํ•ฉ๋‹ˆ๋‹ค : ์ €์ž‘์žํ‘œ์‹œ. ๊ท€ํ•˜๋Š”์›์ €์ž‘์ž๋ฅผํ‘œ์‹œํ•˜์—ฌ์•ผํ•ฉ๋‹ˆ๋‹ค. ๋น„์˜๋ฆฌ. ๊ท€ํ•˜๋Š”์ด์ €์ž‘๋ฌผ์„์˜๋ฆฌ๋ชฉ์ ์œผ๋กœ์ด์šฉํ• 

Kinematic analysis of success strategy of YANG Hak Seon technique Joo-Ho Song 1, Jong-Hoon Park 2, & Jin-Sun Kim 3 * 1 Korea Institute of Sport Scienc

ๆญฏ PDF

hwp

*์„ธ์ง€6๋ฌธ์ œ(306~316)OK

ํšจ์„ฑํŽŒํ”„ํŽธ๋žŒ

Lumbar spine


06ร†ยฏรรฝ

10(3)-10.fm

ๆญฏ์ „์šฉ]

a16.PDF

๋ฉด์ง€

ๆญฏ PDF

example code are examined in this stage The low pressure pressurizer reactor trip module of the Plant Protection System was programmed as subject for

๋‚˜์‚ฌ์‹๋ณผ๋ฐธ๋ธŒ.indd

334 ้€€ ๆบช ๅญธ ๊ณผ ๅ„’ ๆ•Ž ๆ–‡ ๅŒ– ็ฌฌ 55 ่™Ÿ ่ง’ ่ชช ์—์„œ๋Š” ๋ฟ”์ด ๋‚œ ๋ง๊ณผ ๊ณ ์–‘์ด๋ผ๋Š” ๊ธฐํ˜•์˜ ๋™๋ฌผ์„ ์†Œ์žฌ๋กœ ํ•˜์—ฌ ๋‹น๋Œ€ ์ •์น˜ ์ƒ ํ™ฉ์„ ๋น„ํŒํ•˜์˜€๊ณ , ็™ฝ ้ป‘ ้›ฃ ์—์„œ๋Š” ์„ ๊ณผ ์•…์„ ์ƒ์ง•ํ•˜๋Š” ์ƒ‰๊น”์ธ ็™ฝ ๊ณผ ้ป‘ ์ด ์„œ๋กœ ๋ฒŒ์ด ๋Š” ๋ฌธ๋‹ต์„ ํ†ตํ•˜์—ฌ ์˜ณ๊ณ  ๊ทธ๋ฆ„์˜ ๊ฐ€์น˜๊ด€์ด ์ „๋„๋œ ํ˜„์‹ค์„ธ

WOMA Pumps - Z Line

๋Œ€ํ‘œ์ด์‚ฌํ™•์ธ( ) I. ํšŒ์‚ฌ์˜ ๊ฐœ์š” 1. ํšŒ์‚ฌ์˜ ๊ฐœ์š” 1. ์—ฐ๊ฒฐ๋Œ€์ƒ ์ข…์†ํšŒ์‚ฌ ๊ฐœํ™ฉ(์—ฐ๊ฒฐ์žฌ๋ฌด์ œํ‘œ๋ฅผ ์ž‘์„ฑํ•˜๋Š” ์ฃผ๊ถŒ์ƒ์žฅ๋ฒ•์ธ์ด ์‚ฌ์—…๋ณด๊ณ ์„œ, ๋ถ„๊ธฐใ† ๋ฐ˜๊ธฐ๋ณด๊ณ ์„œ๋ฅผ ์ œ์ถœํ•˜๋Š” ๊ฒฝ์šฐ์— ํ•œํ•จ) (๋‹จ์œ„ : ๋ฐฑ๋งŒ์›) ์ƒํ˜ธ ์„ค๋ฆฝ์ผ ์ฃผ์†Œ ์ฃผ์š”์‚ฌ์—… ์ง์ „์‚ฌ์—…์—ฐ๋„๋ง ์ž์‚ฐ์ด์•ก ์ง€๋ฐฐ๊ด€๊ณ„ ๊ทผ

AD AD 8-0 / A A-2 / A A A-5 / A A T-T / Q

์ค‘ ๊ตญ 6 ๋Œ€ ํŒจ ์…˜ ์‹œ ์žฅ ์กฐ ์‚ฌ ๋ณด ๊ณ  ์„œ < 2004 ๋…„ ์ƒ ํ•ด 10 ๋Œ€ ๋งค ์žฅ 10๋Œ€ ํŒจ ์…˜ ์ œ ํ’ˆ ์˜ ๋ธŒ ๋žœ ๋“œ ์‹œ ์žฅ ์  ์œ  ๋ฎฌ > ์ œ ํ’ˆ ๋ธŒ ๋žœ ๋“œ ์‹œ ์žฅ ์  ์œ  ์œจ ์ œ ํ’ˆ ๋ธŒ ๋žœ ๋“œ ์‹œ ์žฅ ์ ์œ  ์œจ C O N C H P LA Y B O Y

Microsoft Word - KSR2012A038.doc

143.fm

ๆญฏ์—ฐ์กฐ98-4.PDF

๊ณตํ•™๋ฐ•์‚ฌํ•™์œ„ ๋…ผ๋ฌธ ์šด์˜ ์ค‘ ํ„ฐ๋„ํ™•๋Œ€ ๊ตด์ฐฉ์‹œ ์ง€๋ฐ˜๊ฑฐ๋™ ํŠน์„ฑ๋ถ„์„ ๋ฐ ํ”„๋กœํ…ํ„ฐ ์„ค๊ณ„ Ground Behavior Analysis and Protector Design during the Enlargement of a Tunnel in Operation 2011๋…„ 2์›” ์ธํ•˜๋Œ€

ๆญฏ174๊ตฌ๊ฒฝํšŒ.PDF

์žฅ์˜์ค€.PDF

PJTROHMPCJPS.hwp

-์‹œ๋ฐฉ์„œ ๋ชฉ์ฐจ- 1. ๊ณต ์‚ฌ ๊ฐœ ์š” 1 2. ์ด ์น™ 2 ์ œ 1 ์žฅ. ๊ฐ€ ์„ค ๊ณต ์‚ฌ 8 ์ œ 2 ์žฅ. ๋ชฉ ๊ณต ์‚ฌ 9 ์ œ 3 ์žฅ. ์ˆ˜ ์žฅ ๊ณต ์‚ฌ 10 ์ œ 4 ์žฅ. ์ฐฝ ํ˜ธ ๊ณต ์‚ฌ 21 ์ œ 5 ์žฅ. ์œ  ๋ฆฌ ๊ณต ์‚ฌ 27 ์ œ 6 ์žฅ. ๋„ ์žฅ ๊ณต ์‚ฌ 34 ์ œ 7 ์žฅ. ์ฒ  ๊ฑฐ ๊ณต ์‚ฌ

Berechenbar mehr Leistung fur thermoplastische Kunststoffverschraubungen

์ œ6์กฐ(์ „์ €ํ•ญ ์‚ฐ์ •) ๋ถ€์œ ์‹ ํ•ด์ƒ๊ตฌ์กฐ๋ฌผ์˜ ์ „์ €ํ•ญ(R)์€ ๋‹ค์Œ ์‹์— ์˜ํ•˜์—ฌ ์‚ฐ์ •ํ•œ๋‹ค. R = (kg) ์ด ์‹์—์„œ Ra๋Š” ๋‹ค์Œ ์‚ฐ์‹์— ์˜ํ•œ ๊ฐ’ Ra = Ka Aa Va (kg) ์ด ์‹์—์„œ Ka: (ํšก๋ฐฉํ–ฅ ํ’์••๊ณ„์ˆ˜) (kg sec /m ) Aa : ํ˜์ˆ˜์„  ์ƒ๋ถ€

ๆญฏ์‹ ์šฉ์นด๋“œ์‹œ์žฅํ˜„์ƒ.PDF

๊ธฐ์ˆ  ๋ฐ์ดํ„ฐ ์ž๋ฃŒ (์ฃผ)ํ™”์‹  ๊ตญ์ œ ์ธ์ฆ๊ทœ๊ฒฉ ์ธ์ฆํ’ˆ ์†Œ๊ฐœ ๋ฐ•์Šค ๋ณดํ˜ธ๋“ฑ๊ธ‰(IP) / UL / NEMA / RoHS ๋ฐฉํญ ๋“ฑ๊ธ‰ / ์šฐ๋ ˆํƒ„ ๊ฐ€์Šค์ผ“ ํฌ๋ฐ 4P~5P 6P~7P 8P~9P ํ”Œ๋ผ์Šคํ‹ฑ ๋ฐ•์Šค & ์•Œ๋ฃจ๋ฏธ๋Š„ ์ œํ’ˆ ํ”Œ๋ผ์Šคํ‹ฑ ์ œํ’ˆ์˜ ํŠน์ง• ๋ฐ ์ „ ์ œํ’ˆ ์†Œ๊ฐœ 10P~11P ๋‹จ์žํ•จ

KAERI/TR-2128/2002 : SMART ์ œ์–ด๋ด‰๊ตฌ๋™์žฅ์น˜ ๊ธฐ๋ณธ์„ค๊ณ„ ๋ณด๊ณ ์„œ

ๆญฏ๋ณธ๋ฌธ.PDF

ๆญฏD13236_F1.PDF

PDF

ํ•œ๊ตญ์ „์ง€ํ•™ํšŒ ์ถ˜๊ณ„ํ•™์ˆ ๋Œ€ํšŒ Contents ๊ธฐ์กฐ๊ฐ•์—ฐ LI GU 06 ์ดˆ๊ฐ•์—ฐ ๊น€๋™์šฑ 09 ์•ˆ์žฌํ‰ 10 ์ •์ฐฝํ›ˆ 11 ์ด๊ทœํƒœ 12 ๋ฌธ์ค€์˜ 13 ํ•œ๋ณ‘์ฐฌ 14 ์ตœ์›์ฐฝ 15 ๋ฐ•์ฒ ํ˜ธ 16 ์•ˆ๋™์ค€ 17 ์ตœ๋‚จ์ˆœ 18 ๊น€์ผํƒœ 19 ํฌ์Šคํ„ฐ ๊ฐ•์ค€์„ญ 23 ์œค์˜์ค€ 24 ๋„์ˆ˜์ • 25 ๊ฐ•์ค€ํฌ 26

A 001~A 036

ๆญฏRCM

DBPIA-NURIMEDIA

09๊ถŒ์˜ค์„ค_ok.hwp

ๆญฏ PDF

์œ ํ•œ์ฐจ๋ถ„๋ฒ•์„ ์ด์šฉํ•œ ๋‹ค์ค‘ ๊ธฐ์ดˆ์ž์‚ฐ ์ฃผ๊ฐ€์—ฐ๊ณ„์ฆ๊ถŒ ๊ฐ€๊ฒฉ๊ฒฐ์ •

, Yard Bottom Slamming, Slamming,, 10-8 Probability Level Bottom Slamming., Bottom Slamming,, Evaluation, Allowable Criteria, Ballast Reduction, Botto

ํšจ์„ฑํŽŒํ”„ํŽธ๋žŒ

<BFACC3D15F F31375FB5B5B7CEBBE7BEF7C0C7B1B3C5EBBCF6BFE4C3DFC1A4BFC0C2F7B9DFBBFDBFF8C0CEB9D7BFB5C7E2BAD0BCAE5FC1A4BCBABAC0C0E5BCF6C0BA2E687770>

THE JOURNAL OF KOREAN INSTITUTE OF ELECTROMAGNETIC ENGINEERING AND SCIENCE Aug.; 30(8),

๋™์•„๋‚ด์ง€1์ˆ˜(A~E)-์ˆ˜์ •2

์™„์„ฑ09E02๋ฐ•์€์ˆ™.PDF

ร†รทร€รฅ82ลก

I 154

ๆญฏIC-706.PDF

DV690-N_KOR_ indd

THE JOURNAL OF KOREAN INSTITUTE OF ELECTROMAGNETIC ENGINEERING AND SCIENCE Sep.; 30(9),

02 _ The 11th korea Test Conference The 11th korea Test Conference _

02 Reihe bis 750 bar GB-9.03

(KPU-300 \(TDS, \307\321\261\333\).hwp)

์‚ฐ์„ ์ƒ์˜ ์ง‘์ž…๋‹ˆ๋‹ค. ํ™˜์˜ํ•ด์š”

A 0 D5-a (XQD Card Type) D5-b (CF Card Type)

๋Œ€๊ฒฝํ…Œํฌ์ข…ํ•ฉ์นดํƒˆ๋กœ๊ทธ

untitled

์‘์šฉA ์ˆ˜์ •.hwp

๊ฐœ์ตœ์š”๊ฐ•


Manufacturing6

DBPIA-NURIMEDIA

ๆญฏ7๊ถŒ2ํ˜ธ.PDF

Parts List

7. ์˜์ƒ์ •๋ณด์ฒ˜๋ฆฌ ์‹œ์Šคํ…œ ์—ฐ๊ตฌ.hwp

ยณยปรรถ

ยตยตโ‰ˆโ€ขโˆโ€กโˆ†ร†1

Vertical Probe Card Technology Pin Technology 1) Probe Pin Testable Pitch:03 (Matrix) Minimum Pin Length:2.67 High Speed Test Application:Test Socket

๋‚จ๋ถํ•œ๊ต๊ณผ์„œ์—์„œ๋‚˜ํƒ€๋‚œ ๋ฏผ์กฑ์ •์ฒด์„ฑ

Transcription:

2 0 0 2 2

D ev elopm ent of A n aly s is T echnique for improv em ent in s treng th and s afety of A ut om otiv e s e at s tructure

. 2 0 0 1 1 2

. 1 1. 1 2. 2. 5 1. 5 2. 11. 14 1. 15 1) 15 2) T rack 20 3) 22 2. 31 1) 31 2) Luggage 35. 47 48 Ab str act 49

Li s t of F ig ure s F ig. 1 Clas sification of aut om otiv e seat F ig. 2 Dev elopm ent proces s of seat sy stem F ig. 3 F.E.M odel of Back F ram e F ig. 4 F.E.M odel of Recliner F ig. 5 F.E.M odel of Slidin g Lat ch F ig. 6 F.E.M odel of Rail P art F ig. 7 F.E.M odel of Body Block F ig. 8 Specim en of S eat F ram e F ig. 9 Configuration of F MVS S 202 H ead Restraint F ig. 10 F.E.M odel of Head Rest Sim ulation F ig. 11 B oundary Condition of Head Rest Sim ulation F ig. 12 Deform ed Shape F ig. 13 Stress Concentration F ig. 14 Boun dary Condition of T rack P art F ig. 15 Deform ed Shape of T rack P art F ig. 16 configuration of F MVS S 210 S eat Belt An chorages T est F ig. 17 Ph ot ograhp of F MVS S 210 S eat Belt Anchorag es T est F ig. 18 Load History Curv e & Load Con dition F ig. 19 F.E.M odel of F MV S S 210 F ig. 20 Ph ot ograph of S eat Belt Anchorag es T est F ig. 21 Stress Distribution F ig. 22 Deform ed Shapes F ig. 23 F MVS S 210 W ith Cent er Rail F ig. 24 Stress Distribution F ig. 25 Deform ed Shapes w ith Cent er Rail F ig. 26 Configuration of F MVS S 201 H ead Im pact T est F ig. 27 F.E.M odel of Head Rest & Im pact or F ig. 28 Initial Configuration of F MV S S 201 H ead Rest Im pact T est F ig. 29 Deform ed Shapes of S eat under Head Rest Im pact Simulation F ig. 30 M ax imum A cceleration of H ead Rest F ig. 31 Configuration of Lu gg age Block Im pact T est

F ig. 32 Im itial Configuration for Lug gage T est Sim ulation F ig. 33 Im posed Initial Velocity for Lu gg age T est Sim ulation F ig. 34 Deform ed Shape & M ax. Displacem ent F ig. 35 Deform ed Shape on T op View F ig. 36 Ph ot ograph of Lu gg age T est F ig. 37 V arialble Design of Hing e Bracket F ig. 38 Comparison of M ax. Displacem ent Graph F ig. 39 M ax. Displacem ent of each T ype F ig. 40 Ph ot ograph of Lu gg age T est (D T ype) Li s t of t able s T able 1 M at erial of S eat F ram e T able 2 M at erial Dat a T able 3 P aram atic study of Lug gag e Block Im pact Sim ulation

. 1.1 (Seat ) (Chair )... FMVSS (Federal Motor Vehicle Safety Stadard) ECE.,,,...,,,. - 1 -

1.2 Fig.1,, 1,,,,...,,. (Foam ),, (Floor ),, (Seat Belt Anchorage)..,...,. (head rest ).,. (padding ). (back rest ). T Ek., - 2 -

,.. F ig. 1 Classification of Aut om otiv e S eat - 3 -

Fig. 2 Development Process of Seat Sy stem - 4 -

. 2.1 1) (back frame) (recliner ).,.,,,. (spring ) (wire). - 5 -

CAD Mode l F.E. Mode l (2), (shell). /., 10 mm. - 6 -

(3),.,,. CAD Mode l - 7 -

F.E.Mode l (4),,.. Fig. 7,. - 8 -

F.E. Mode l of ra il pa rt (4),,.. - 9 -

(a) F.E. Mode ling of uppe r body block (b) F.E. Mode ling of uppe r body block Fig. 7 F.E.Model of Body Block - 10 -

2.2.. T able 1. T able 1 Material of Seat Frame SP CC (S CP 1) - seat fram e - bracket SPH C (SHP 1) - seat fram e - bracket SAPH440 (SA PH45) - seat m echanism - box leg ST KM - cu shion - back m ain frm - 11 -

1) -. (a) Spes ime n of Plate (b) Spes ime n of Pipe Fig. 8 Specime n of Seat Frame - 12 -

T able 2 Material Data M at erial Yeild Stress [kg/ m m 2 ] Ultim ate Stress [kg/ mm 2 ] Youn g ' s M odulu s [kg/ m m 2 ] P oission ratio T hickn ess [m m ] SP CC 20.89 30.63 21.0 0.3 2.6 SPH C 29.5 37.25 21.0 0.3 2.3 SAPH440 35.44 50.35 21.0 0.3 2.6 ST KM 36.79 40.84 21.0 0.3 1.5-13 -

III.,,, (T rack ),,..,,. (Explicit Dynamic Code) PAM - CRASH. - 14 -

3.1 3.1.1 1) (FMVSS 202) 38 kgf m., 102 mm. 890N. Fig. 9 Configur ation of FMVSS 202 Head Restraint - 15 -

2) Fig. 10,,. Fig. 10 F.E.Model of Head Rest Simulation - 16 -

,. (hinge bracket ).. - : Rotation Free/ Direction Fixed - : All Fixed Fig. 13 (node). - (quasi- static) 140 msec Ramping Up. Fig. 11 Boundary Condition of DS2 Head Rest Simulation - 17 -

3) FMVSS 202,. Fig. 12 Deformed Shape - 18 -

,. Fig. 13 Fig. 13 Stress Concentration - 19 -

3.1.2 (T rack) Fig. 14 1,449 1292., 1,300 kgf Fig. 14 Boundary Condition of T r ack Part - 20 -

2) Fig. 15 250, 500, 1000, 1300kgf. 1,300kgf.. Fig. 15 Deformed Shape of T rack Part - 21 -

3.1.3 1) (FMVSS 210) (NHT SA ; National Highway T raffic Safety Administration ) FMVSS 210. (lap belt system ) (body block) 22.24kN (static load), (lap and shoulder belt system ) 13.35kN. 5 15 o. 20... 16 210.. 17. (load cell)., (zig ). - 22 -

Fig. 16 Configuration of FMVSS 210 Seat Belt Anchor ages T est Fig. 17 photograph of FMVSS 210 Seat Belt Anchorages T est - 23 -

2) (Finite Elment Model) / HYPERMESH T M.,,. FMVSS 210.(Fig. 8) (Contact ) (shell element ), (bar element ).,, (rigid body ). Fig. 18. (Inertia effect ). Fig. 19.. Fig. 18 C 20. A 3000 lb +10 o B 5000 lb +10 o C 29000 lb 0 o Fig. 18 Load History & Load Condition - 24 -

Fig. 19 F.E.Model of FMVSS 210 Fig. 20 Photograph of Seat Belt Anchor ages T est - 25 -

3) (1) Fig. 22 (center rail). RR _d RR. (floor ) (leg ) RR. Fig. 21. RR. Fig. 21 Stress Distribution - 26 -

(a) Side & T op view at 0ms (b ) Side & T op view at 80ms (c) Side & T op view at 120ms Fig. 22 Deformed Shapes - 27 -

(2). RR. Fig. 23. Fig. 23 FMVSS 210 With Center Rail - 28 -

Fig. 25. Fig. 24 RR.,. Fig. 24 Stress Distribution - 29 -

(a) Side & T op view at 0ms (b ) Side & T op view at 80ms (c) Side & T op view at 120ms Fig. 25 Deformed Shapes w ith Center Rail - 30 -

3.2 3.2.1 1) (FMVSS 210) FMVSS. (interior ) FMVSS 201. A,B (pillar ). 172 mm, 6.8kg (head foam ) 15mph 3m s 80g. F ig. 26 Configuration of F MV S S 201 Head Im pact T est - 31 -

2). FMVSS 201 Fig. 27 (impactor ). 172 mm. 7,468. Fig. 27 Finite Element Model of Head Rest & Impactor Fig. 28 Initial Configuration of FMVSS 201 Head Rest Impact T est - 32 -

3) Fig. 29.,.. Fig. 29 Deformed Shapes of Seat under Head Rest Impact Simulation - 33 -

3ms Fig. 30 22.346 g. Fig. 30 Maximum Acceler ation of Head Rest - 34 -

3.2.2 Luggage 1) (ECE No. 17-7) RV,,.. ECE No.17., 50 ± 2 kph (luggage) 100 mm, 150 mm.,. Fig. 31 Configur ation of Lugage Block Impact T est - 35 -

2)... Fig. 41 (SRP ; Seating Reference Point ). 50 mm 5. 300 mm 20 mm 18 kg. 50 km/ h 100 mm. - 36 -

Fig. 32 Initial Configuration for Luggage T est Simulation Fig. 33 Imposed Initial Velocity for Luggage T est Simulation - 37 -

3) Fig. 34. 219 mmqus 100 mm 119 mm.. Fig. 36. - 38 -

(a ) T op Veiw (b) Side View Fig. 34 Deformed Shape & Max. Displacement - 39 -

(a) 0 msec (b) 30 m sec (c) 60 msec Fig. 35 Deformed Shape on T op View - 40 -

(a ) Rear View (b) Side View Fig. 36 Photogr aph of Luggage T est - 41 -

3.2.3 Luggage. Fig. 37 A,B,C,D 4. Fig. 37.. A, B. C B 2.6 mm 3.2 mm D B Fig. 37.. - 42 -

Fig. 37 Param atic Study of Hinge Br acket T able 3 Paramatic Study of Luggage Block Impact Simulation Hing e T ype Recliner Brack et Original T ype Hin ge Bracket None A T ype Recliner SP CC 2.3t B T ype Recliner SA PH 2.6t C T ype Recliner SA PH 3.2t D T ype Recliner SA PH 2.6t & Rear Pipe - 43 -

1) 2, (Double Recliner ). SPCC 2.3t SAPH 2.6t, SAPH. SAPH 3.2t (D T ype), SAPH 2.6t (C T ype),. SAPH 2.6t (1.5t ) (D T ype). Fig. 38 D. Displacement Regulation Original A T ype B T ype C T ype D T ype 100 mm 219 mm 249 mm 74.8 mm 80.4 mm 50.5 mm Fig. 38 Comparison of Max. Displacement Graph - 44 -

(a ) A T ype (b ) B T ype (c) C T ype (d) D T ype Fig. 39 Max. Displacement of Each T ype - 45 -

D.. Fig. 40 Photograph of Luggage T est (D T ype) - 46 -

.,.. 1) - 2) 3) -. 4). 5) - 200% -, 4 50% D- T ype. - 47 -

[1] "Optimum Design and Impact Characteristics for Automobile Seat". Heon Young Kim, Sang Keun Lee, Jung Jae Kim, Pacific Conference on Automotive Engineering, 1997. [2] CRASH AMD- Vol. 169/BED- Vol 25, Cr ashw orthines s and Occupant Pr otection in T r an sportation Sy stem s ASME 1993. [3] Seating sy stem T est, FMVSS NO 208 NHT SA USA. [4] Seating Belt A ssembly Anchor ages T est, FMVSS NO 210 NHT SA USA. [5] "Injury Mitigating Benefits of an Inflatable Shoulder Belt for Seat Integr ated Application", Advacnes in Safety T echnology 1999(1999-01- 0085). [6] "Studies with Belt Integr ated Vehicular Seat s", Anthony Sances, Kenneth J. Saczalski, Envir onm ent Research and Safety T echnologies, Inc., Newport Beach, California. [7] "Autom otiv e Belt s to Seat", Philip W. Leistr a III, Autom otiv e Body Interior & Safety Sy stem s, IBEC ' 96. [8] "Belt Integr ated Vehicular Seat Rear Impact Studies", Kenneth J. Saczalski, Joseph L. Burtion, Paul R, Lw eis, T odd K. Saczalski, Peter E, Bar ay, Seoul 2000 FISIT A World Automotive Congress [9] "A dvanced Restr aint Sy stem s for Rear Seat Occupant s", Dr. Harald Zellm er, Bag & Belt ' 98, 5th International Akzo Nobel Symposium on aut om otiv e Occupant Restraint Sy st em s. [10] "CAE Simulation of FMVSS 207/ 210 T est For Seat Belt Anchor ages", Grish Bapu, Shekar Erasala, Saleem Humayun, Autom otiv e Body Interior & Safety Sy stem s, IBEC ' 95 [11] "Preent Status of Impact Analy sis in Japan", K. Andoh, H. Niizeki, HANPM '95-48 -

D e v e lopm e nt of A n aly s is T e c h n iqu e f or im prov e m e nt in s tre n g th an d s afety of A u t om otiv e s e at s tru c tu re Yoo Sung Yong D ep artm ent of M echanical E ng ineering Graduate S chool, K ang won N ational Univ ers ity U sing FEM (Finite Element Method) can provide u seful inform ation s to design a new car seat and can r educe the overall design cost and time. T his paper deal w ith the safety capability of the seat sy stem while occupant s are sitting on the seat in case of v ariou s impact condition s : fr ontal, rearw ar d, and ruggage impact. T he structur al analy sis of car seat sy stem by the finite element method. T he load- deformation characteristics of seat fram e are simulated accor ding to the test r equirem ent s by FMVSS. T hr ee dimen sion modeling technique is applied to the component s of the seat frame. Comparison w ith test r esult s show s the validity of this analy sis technique. T he design of a car seat sy st em r equir es the structur al optimization for the w eight, strength, and performance. - 49 -