Igniter cable connector
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United States of America Patent
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-
Dec 18, 1990
Grant Date -
N/A
app pub date -
Mar 17, 1989
filing date -
Mar 17, 1989
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
An improved high voltage igniter connector for aircraft applications. An insulator projecting from the cable connector extends into a tubular insulator in the igniter. An electrical contact at the free end of the connector insulator is urged into contact with a center electrode terminal in the igniter. A resilient annular first seal is formed between the connector and an end of the igniter insulator. A resilient annular second seal is located between the connector insulator and the interior wall of the igniter insulator near the free end of the connector insulator to increase resistance to flashover at the connector.
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