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Consolidated Tech Man - Holo-Krome

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FASTENER JOINT DESIGN<br />

In applications which experience high cyclic loading analysis of<br />

the fastener loading is critical. Based on the relative stiffness of the<br />

assembly and the screw, and the external load applied, the fastener size<br />

and proper preload can be determined.<br />

Preload is normally achieved by tightening the screw. The<br />

torque required to achieve the specific preload depends on the surface<br />

lubricity at the threads and at the head, the surface finish, thread pitch,<br />

head bearing configuration, and torque wrench accuracy.<br />

PRELOAD AND EXTERNAL LOAD CONSIDERATIONS<br />

When a fastener is tightened, the load on the assembly and<br />

fastener increase. In the ideal case, the screw stretches, and the joint<br />

compresses, within the elastic limit, according to Hooke's Law.<br />

Suppose a joint has been tightened to a preload P i and additional<br />

load, P e , tending to separate the members is applied. In general in rigid<br />

assemblies, as long as the external load is less then P t it primarily<br />

decompresses the joint and has little effect on the tension in the screw.<br />

Thus even if such a load is repeatedly applied, the fastener will not fail in<br />

fatigue. However, if a repeated external load greater than P i must be<br />

applied, it should be kept to a minimum, since it produces cyclic tensioning<br />

in the screw and may lead to fatigue failure.<br />

This principle has important practical applications. Often when<br />

fasteners fail, the solution used is to switch to the next larger size. This<br />

involves changing the tooling for hole preparation and tightening, and<br />

possibly changing assembly fixtures. Most likely, merely tightening the<br />

fastener above the external load would solve the problem. For instance,<br />

a 180,000 psi tensile strength socket screw has an average endurance limit<br />

of only 15,000 psi. This means that the fastener is capable of withstanding<br />

a maximum one-time applied stress of 180,000 psi, but that a stress<br />

change felt by the fastener of more than 15,000 psi could result in a fatigue<br />

failure within a given number of cycles.<br />

A conservative formula giving the tension on a fastener which<br />

has an external load, P e is:<br />

[ ] Ks P = P + K + K P t i s c e<br />

Nomenclature<br />

Pt = Total Bolt load, lb.<br />

Pi = Preload, lb.<br />

Pe = External load, lb.<br />

Ks = Screw spring constant, lb./inch.<br />

Kc = Assembly spring constant, lb./inch.<br />

The spring constant, K, for a member is given by:<br />

52<br />

(area, sq. in.) (modulus of elasticity, psi)<br />

(length, in.)<br />

Since these calculations ignore factors such as bending, heat,<br />

and impact loading, they are useful as a guide only.<br />

Torque to achieve preload<br />

When screws are torqued to achieve preload, the torsional<br />

stresses on them reduces the total tensile force they can withstand<br />

before yielding. The following formula can be used to determine the<br />

effect of this torsional component:<br />

P ( S = ±<br />

t<br />

A<br />

√ 2 J A<br />

P)<br />

+( ) t x r 2<br />

2<br />

The desired tightening torque can be estimated using the<br />

empirical formula:<br />

T = KDP<br />

Nomenclature<br />

S t = Total tensile stress felt by bolt, psi<br />

P = Preload exerted by bolt, lb.<br />

A = Thread stress area, sq. inches<br />

T = Tightening torque, in.-lb.<br />

t = Torsion felt by screw (approximately 40% of applied<br />

torque, depending on lubricity), in.-lb.<br />

r = √A/π<br />

J = πr4 (polar moment of inertia), in. 4<br />

2<br />

K = Constant from 0.05 to 0.35, dimensionless<br />

D = Nominal screw diameter, inches<br />

The constant, K, is normally from 0.19 to 0.25 for a black screw.<br />

For a lubricated fastener or one with cadmium plating, K is from 0.13 to<br />

0.17. Zinc plated screws, not lubricated, may have a K value as high as<br />

0.30 to 0.35.<br />

For rigid parts of steel, the conservative practice is to tighten the<br />

fasteners to 75% of yield. Lower torques should be considered for<br />

flexible joints, joints with gaskets, or assemblies subject to high<br />

temperatures.<br />

Joint Design Steps<br />

1. Calculate the assembly service load.<br />

2. Determine relative loading on each fastener.<br />

3. Determine the style fastener desired (hex, socket, etc.).<br />

4. Using the highest loaded fastener in assembly, apply an appropriate<br />

safety factory based on the estimated reliability of the service load<br />

value, the quality level of the type fastener used, estimate of<br />

assembly techniques consistency, and danger of an assembly<br />

failure. Normally a safety factory could range from 1.5 to 6.<br />

5. Determine fastener size, tightening torque, and cycle life, where<br />

applicable.<br />

6. Specify tightening torques on drawing.<br />

Fastener Assembly Tips:<br />

1. Preload properly.<br />

2. Do not use split type lock washers on socket head screws or Grade<br />

8 hex screws.<br />

3. Use long screws when possible.<br />

4. Avoid transverse or shear loading against the threads.<br />

5. Keep the members clean during assembly.<br />

6. Use wrenches that fit properly and are correctly heat treated.

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