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Define a block slightly wider, with a trailing end margin (around 2.5 cm).
This is used as an entry point into the foam and allows the wire to reach
thermal equilibrium prior to effectively begin the real airfoil section
cut.
In order to avoid distortion at the beginning of the cut:
These margins are located at both block ends (left and right), but also
at leading and trailing edges. When cutting the trailing edge, if the cutting
speeds are different at root and tip, the wire temperature and the glow
are also different, so the trailing edge is misaligned. This remains true
even with an instantaneous adjustment of the wire temperature.
In fact, to have a perfect match and smooth section evolution over
the wing, you need to have the wire cut beginning at the same instant for
the trailing edge, from root to tip. Of course, you should also end the
cut simultaneously at the leading edge (For those beginning the cut with
the LA, same thing with reverse order). Imagine a trapezoidal wing, with
200mm and 150mm chords, and 10 mm margins added at both leading and trailing
edges. Then as your margins are not proportionnal to the chords, as the
wire moves at constant speed (as Gilles asserts us), and displacement at
both wing ends are calculated to penetrate and get out of the foam at the
same time, the wire will actually reach the root trailing edge whilst still
in the margin at tip. At the leading edge the wire will reach the margin
at root prior to end the airfoil cut at the tip.
The simplest workaround is to add at leading and trailing edges margins
which are proportionnal to the choords.
So:
Cut your block - and your wing - wider than necessary (2 cm margin
at both root and tip)
After this first shaping, remove the distorted margins with a knife
With everything setup and adjusted correctly, the end precision of
a wing pannel is really good.
A method to evaluate and adjust the wire kerf compensation:
Evaluation, Why ? :
To allow the Cnc software to compensate for the wire kerf when cutting
a wing (straight or trapezoidal), and get foam cores of the desired thickness.
How to evaluate :
A test cut requires to cut horizontal slices in a foam block of known
thickness. The wire kerf is equal to the thickness difference before and
after cuts, divided by the number of slices made in the block. This test
should be done with the best wire temperature for a given speed V, and
with the same temperature at half speed V/2 (This mimicks the case of a
wing with a tip chord dimension half of the root chord).
Practising:
For all tests, prepare two foam blocks, identical to those used for
wire temperature adjustment. As foam blocks are not plane, they have to
be shaped on one side with the 'Test cut' menu. You can proceed with all
blocks in a single operation if you want to save time. Then measure the
thickness of the blocks. With one block, at V speed and ideal wire temperature,
cut as many slices as possible, with a minimal thickness for a slice around
10 mm (If slices are too thin, this will corrupt the result). Working conditions
are the same than for wire temperature determination, same displacements
at both ends, so the wire should begin and end cut simultaneously over
the whole span. Then measure the resulting thickness of the remaining block
(slices in fact). Preferably in the middle and without too much pressure.
Then calculate the ray value for the nominal speed. Then repeat the process
with the second block, with the same wire temperature adjustment but a
a speed devide by two. This will give you the ray value at V/2.
The values can then be entered in the "Wire Temperature" menu
and will be stored then into the foam.bd file.
For best compensation by the CNC software, this evaluation should be
done over the whole speed range you can use for foam cuts. For instance
from 0.5 mm/s up to 3.5 mm/s with 0.5 mm/s steps. All the values are to
be entered in the "Wire Temperature", or directly into the foam.bd
file.
Findings:
If you proceed with this test over the whole usable speed range of your
foam cutting table, you are going to realize that for a given foam type,
at the ideal wire temperature adjustment, the wire kerf values does not
change. For instance, with expanded polystyren KNAUF 400 EM and a 0.35mm
wire, ray at V = 0.8mm and ray at V/2 = 1.5mm.
Another finding is the fact that the ideal temperature adjustment is
nearly proportional to speed. The evaluation and adjustment of wire temperature
is so simplified. Rather than performing ideal temperature adjustments
over the whole speed range, it may be determined at lowest and highest
speeds and then interpolated between those two measure points.

As ray values at V and V/2 are identical for all speed values, the wire
kerf determination may be performed at both maximal and minimal speed and
then averaged at V and V/2. These averaged values will be set for all intermediate
speeds in the wire temperature menu (without further tests).
Future : (NB already implemented in recent software versions)
With an electronic control board which supports the wire temperature
control and allows the software to read back the values (BB20XX) you will
not have to adjust the wire temperature any longer as this will be performed
by the CNC software.