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Design Guide - Solvay Plastics

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<strong>Design</strong>ing for Stiffness<br />

When a design engineer considers replacing a metal<br />

component with plastic, one consideration is the rigidity<br />

or stiffness of the component. If the application requires<br />

that the maximum deflection under load remain at the<br />

current value, then the plastic component must have<br />

stiffness equivalent to the metal component.<br />

Table 38 provides the deflection equations for a variety<br />

of beams. Selecting the beam with both ends fixed and<br />

a uniformly distributed load, the deflection (Y) is given by<br />

Y =<br />

FL 3<br />

384EI<br />

To arrive at a part design with equivalent stiffness, start<br />

by equating the deflection equations for the plastic and<br />

metal parts as follows:<br />

FL 3<br />

384EI<br />

metal<br />

=<br />

FL 3<br />

384EI<br />

plastic<br />

Assuming a constant load and length, and removing<br />

the factors common to both sides of the equation, the<br />

governing equation becomes:<br />

Equation 1<br />

[EI] metal = [EI] plastic<br />

Knowing that the modulus of elasticity (E) of these<br />

materials are substantially different, it becomes apparent<br />

that the dimensions of the parts will need to be changed<br />

to adjust the moment of inertia (I).<br />

For example, if the metal part is produced from<br />

magnesium with a modulus of 6.5 psi x 10 6 psi<br />

(44.9 GPa) and the replacement plastic material is Udel<br />

GF-130 with a modulus of 1.07 psi x 10 6 psi (7.38 GPa),<br />

then the required increase in the moment of inertia can<br />

be calculated from Equation 2.<br />

Equation 2<br />

(6.5 psi x 10 6 psi)(I magnesium )=(1.07 psi x 10 6 psi)(I Udel )<br />

or (44.9 GPa)(I magnesium )=(7.38 GPa)(I Udel )<br />

I Udel =6.07 I magnesium<br />

Increasing Section Thickness<br />

One way to increase the moment of inertia is to increase<br />

the section thickness.<br />

From Table 39, the formula for the moment of inertia of a<br />

rectangular section is:<br />

Substituting into Equation 2 and eliminating<br />

common factors:<br />

If the section thickness in magnesium was 0.100 inch<br />

(2.54 mm), then<br />

3<br />

d<br />

Udel<br />

= 6.07(.001)<br />

or<br />

d<br />

3<br />

6.07d 3<br />

Udel<br />

d<br />

Udel<br />

=<br />

magnesium<br />

3<br />

d<br />

Udel<br />

= 6.07(16.38)<br />

d<br />

Udel<br />

To achieve equivalent stiffness by simply increasing<br />

section thickness requires an 82% increase.<br />

Adding Ribs to Maintain Stiffness<br />

Another method of achieving stiffness is to increase the<br />

moment of inertia by adding ribs. The use of ribs can<br />

reduce wall thickness and weight, and still provide the<br />

required stiffness.<br />

Because the material is the same as in the previous<br />

example, the moment of inertia of the rib design is equal<br />

to the moment of inertia of the 0.182 inch (4.63 mm)-thick<br />

plate. The moment of inertia of the plate is given by:<br />

I plate<br />

=<br />

=<br />

0.182 inch<br />

4.63 mm<br />

bd 3<br />

12<br />

If we assign 1 inch (25.4 mm) to the width, then I = 5.02<br />

x 10 -4 in 4 (209 mm 4 ).<br />

Calculating the rib and wall thickness that will give<br />

the same moment of inertia is done using the following<br />

equations for the distance from the neutral axis to the<br />

extreme fiber (c), the moment of inertia (I), and the<br />

area (A).<br />

d 2 t + s 2 (b − t)<br />

c = d −<br />

2(bs + ht)<br />

I =<br />

=<br />

tc 3 + b(d − c) 3 − (b − t)(d − c − s) 3<br />

3<br />

I =<br />

bd 3<br />

12<br />

A = bs + ht<br />

where b is the width and d is the thickness of the section.<br />

<strong>Design</strong> Information<br />

Udel ® Polysulfone <strong>Design</strong> <strong>Guide</strong><br />

45

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