Igniter Electrode Life Control.
Abstract
The prevention of electrode material erosion by undercutting in the outer electrode shell of igniter electrodes of jet engine ignition systems is prevented by the application of an electrical insulation coating. The coating is applied to the surface of the outer electrode shell which faces the ceramic insulation around the center electrode where erosion patterns are known to occur. the insulation material is selected from electrical insulation substances such as oxides of aluminum, tungsten, magnesium, beryllium or zirconium by choosing a non-porous electrical insulating substance with thermal expansion characteristics approximately equalling those of the outer electrode shell. Since a typical outer electrode shell is composed of 446 stainless steel, an optimum choice for the electrical insulation coating is AL203 deposited with a coating thickness of between 5 and 10 mils. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 07, 1985
- Accession Number
- ADD012007
Entities
People
- John C. Scott
Organizations
- United States Department of the Air Force