CH34055

Champion Aerospace Turbine Engine Igniter
   ➢ Silver-plated shell for protection against corrosion and seizing at mechanical interfaces
   ➢ Advanced glass and mechanical sealing feature design outside the combustor case for protection against gas leakage under high temperature conditions.
   ➢ Internal configuration design that optimizes heat flow away from terminations to protect sensitive ignition lead components
   ➢ Internal termination protective coating to prevent lead component seizing
   ➢ Use of external wear and thermal barrier coatings to protect the life limiting features from wear and thermal distress