PARAMETERS DEFINITION FIXED (during initial setup).
     
  • Used Motors (58 or 100 steps/turn).
  • Leading screws characteristics.
  • Overall excursion on both axis ( stops should not be reached during a cut operation).
VARIABLE (for each cut).
     
  • Distance between both trolleys. If the trolleys are fixed on the table then the parameter is actually fixed.
  • Foam block dimensions.
  • Foam block location (positionning).
  • Wire diameter
  • Cutting speed.
The values of the last variable set used are displayed on the screen.
 
DESCRIPTION DE L'OBJET A DECOUPER Wing of wing segment, stabilizer
     
  • Root airfoil section choice.
  • Modification of the relative thickness.
  • Tip airfoil section choice.
  • Modification of the relative thickness.
  • Segment length.
  • Root chord.
  • Tip Chord.
  • Leading edge sweep back.
  • Twist.
  • Diehedral (optional).
  • Leading edge thickness.
  • Trailing edge width.
  • Skin thickness.
  • Position of spar(s).
  • Dimentions of spar(s).
  • Choice between left or right wing.
Fin.
     
  • Root section choice.
  • Modification of the relative thickness.
  • Tip airfoil section choice.
  • Modification of the relative thickness.
  • Segment length.
  • Root chord.
  • Tip Chord.
  • Leading edge sweep back.
  • Leading edge thickness.
  • Trailing edge width.
  • Skin thickness.
  • Position of spar(s).
  • Dimentions of spar(s).
Fuselage back.
     
  • Segment length.
  • 1st end width.
  • 2nd end width.
  • input for intermediate points
  • skin thickness.
  • Foam thickness (if hollowed).
Cutting a block.
     
  • Direct cut with index display on screen .
  • Parametrable cut angle.
  • Cut length input.