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6<br />
Effective Weight<br />
Effective weight is an important factor in selecting shock<br />
absorbers . A shock absorber “sees” the impact of an<br />
object in terms of weight and velocity only; it does not<br />
”see” any propelling force . The effective weight can<br />
be thought of as the weight that the shock absorber<br />
“sees” on impact . Effective weight includes the effect<br />
of the propelling force on the performance of the shock<br />
absorber .<br />
Failing to consider the effective weight may result in<br />
improper selection and poor performance of the shock<br />
absorber . Under extreme conditions, an effective weight<br />
that is too low may result in high forces at the start of<br />
stroke (high on-set force) . However, an effective weight<br />
that is too high for the shock absorber may cause high<br />
forces at the end of stroke (high set-down force) .<br />
Consider the following examples:<br />
1 .) A 5 lb (2 .27 kg) weight travelling at 25 ft/sec (7 .62<br />
m/s) has 625 lbs (71 Nm) of kinetic energy (figure A) .<br />
On this basis alone, a MA 3325 would be selected .<br />
However, because there is no propelling force, the<br />
calculated effective weight is five pounds – which is<br />
below the effective weight range of the standard MA<br />
3325 . This is a high on-set force at the start of the<br />
stroke (Figure B) . The solution is to use a speciallyorificed<br />
shock absorber to handle the load .<br />
2 .) A weight of 50 lbs (22 .68 kg) has an impact velocity<br />
of 0 .5 ft/sec (0 .15 m/s) with a propelling force of<br />
800 lbs (111N) (Figure C) . The total impact energy<br />
is 802 .5 inch-pounds . Again, a MA 3325 would be<br />
selected based just on the energy . The effective<br />
weight is calculated to be 16,050 pounds (7,280<br />
kg) . This is well above the range of the standard MA<br />
3325 . If this shock absorber is used, high-set-down<br />
forces will result (Figure D) . In this case, the solution<br />
is to use a ML 3325, which is designed to work in<br />
low-velocity, high-effective weight applications .<br />
Computer-Aided Simulation<br />
By combining application data with a shock absorbers<br />
design parameters, ACE engineers can create a picture<br />
of how the shock will perform when impacted by the<br />
application load . Peak reaction force, peak deceleration<br />
(G’s), time through stroke, and velocity decay are<br />
identified with extreme accuracy . The user benefits by<br />
having the guesswork taken out of sizing decisions and<br />
by knowing before installation how his shock problem<br />
will be solved .<br />
Simulation is also used to maximize the performance<br />
of ACE adjustable models by predicting the ideal<br />
adjustment setting for a particular group of conditions .<br />
By using simulation software during product<br />
development stages, ACE has maximized the<br />
performance of its entire line of deceleration devices for<br />
over two decades .<br />
Figure A<br />
Figure B<br />
ACE Controls <strong>Inc</strong>. · 800-521-3320 · (248) 476-0213 · Fax (248) 476-2470 · www.acecontrols.com · email: shocks@acecontrols.com<br />
Force<br />
Figure C<br />
800 lbs<br />
(111 N)<br />
Figure D<br />
Force<br />
Low Effective Weight<br />
25 ft/sec (7.62 m/s)<br />
5 lbs<br />
(2. 27 kg)<br />
Low Effective Weight<br />
Stroke<br />
High Effective Weight<br />
Example 2: Orifice Area Is<br />
Too Large (High Set-Down)<br />
Linear<br />
Deceleration<br />
Example 1: Orifice Area Is<br />
Too Small (High On-Set)<br />
High Effective Weight<br />
0.5 f/s (0.15 m/s)<br />
50 lbs<br />
(22.68 kg)<br />
<strong>Air</strong>-<strong>Oil</strong> <strong>Systems</strong>, <strong>Inc</strong>. www.airoil.com<br />
Stroke<br />
Linear<br />
Deceleration