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Lightweight Electric/Hybrid Vehicle Design

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(a)<br />

Creepstrain dE/dt<br />

(b)<br />

3.0<br />

2.0<br />

1.0<br />

0.05<br />

0.03<br />

0.01<br />

0<br />

Hinge mount<br />

0 1000 3000 5000<br />

Loading period t(h)<br />

p /2<br />

p /2<br />

1O<br />

/3<br />

1O<br />

/3<br />

1O<br />

/3<br />

1O 10 200 N<br />

11 110 N 11 110 N<br />

Test appliance<br />

100 N/mm 2<br />

<strong>Lightweight</strong> construction materials and techniques 185<br />

Seat belt anchorage<br />

20 N/mm 2<br />

Striker pin, driver’s door<br />

Mount point for belt retractor<br />

T=0.6 kp/cm 2<br />

Creep modulas of elasticity Ec (kN/mm 2 )<br />

40<br />

30<br />

20<br />

15<br />

10<br />

9<br />

8<br />

7<br />

6<br />

5<br />

10 -1<br />

0<br />

0 1000 3000<br />

Loading period t(h)<br />

5000<br />

(c)<br />

(d)<br />

normal resin<br />

10 0<br />

T=0.4 kp<br />

T=0.2 kp<br />

IV<br />

I<br />

VII<br />

1 d 1 w 1 month<br />

10 1<br />

10 2<br />

10 3<br />

Loading period t(h)<br />

II<br />

320 N<br />

900 N<br />

V<br />

10 4<br />

Test appliance<br />

23°C<br />

23°C<br />

40°C<br />

60°C<br />

23°C<br />

40°C<br />

60°C<br />

10 5<br />

GF 82 -UP<br />

GF 68 -EPweb<br />

GF 30 -UP<br />

resinmat<br />

Fig. 7.7 Composites in passenger cars: (a) test forces on front door frame; (b) creep strain of GRP showing exponential<br />

and linear regions; (c) creep of rigid PUR foam under constant shear; (d) time/temperature dependency of GRP;<br />

(e) composite GRP floor design.<br />

III<br />

(e)

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