Objective Braze carbide rotary file assemblies with uniform concentricity in an aerospace application
  Material • Carbide blank
  • High speed steel shank
  • Temperature indicating paint
  • Braze shim and black flux
  Temperature 1400°F (760°C)
  Frequency 252 kHz
  Equipment Power of 6KW induction heating system, equipped with a remote heat station containing two 0.33 μF capacitors (total 0.66 μF)
  An induction heating coil designed and developed specifically for this application.
  Process A multi-turn helical coil is used. The part is heated to determine the time required to reach the desired temperature and required heat pattern. It takes approximately 30 – 45 seconds to reach 1400°F (760°C) depending on the various part sizes.
  Flux is applied to the entire part. A braze shim is sandwiched between the steel shank and carbide. Induction heating power is applied until the braze flows. With proper fixturing, concentricity of the part can be achieved.
  Results/Benefits • Repeatable, consistent precise heat.  
   
  brazing-carbide-file  








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