Aircraft Floor Panel Insert Press By
Motion Control Systems
This
2 ton press forms collars into the mounting holes on
aircraft floor panels to within .002" of the surface top.
The challenge with this application was that the floor
panels have a thickness variation of up to .005", therefore
the motion control required was much more then a simple
preset index. A spring loaded sensor ring with and
internal LVDT was part of the bottom press anvil. As
the top anvil down stroke impacts the collar, the sensor
ring is deflected, sending an analog signal relative to the
level of the surface back to the controller. The
signal is used to determine the end position of the stroke
travel. The key to achieving production rates
comparable to non-intelligent "bang-bang" presses was to
essentially throw the actuator servo into reverse for a
number of milliseconds in order to stop the down stroke
within tolerance.