Aircraft power connector with differential engagement and...

Electrical connectors – Coupling part with actuating means urging contact to move... – Expandable contact or spreadable contacts

Reexamination Certificate

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Reexamination Certificate

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07871282

ABSTRACT:
A new and improved aircraft power connector, for electrical connection to an aircraft electrical connector, has incorporated thereon a dual-position mechanism which can effectively alter the engagement force level defined between the electrical connector contact pins of the aircraft power connector and the aircraft electrical connector. When the mechanism is disposed at a first position, the force level is relatively low so as to easily permit connection and disconnection, whereas when the mechanism is disposed at a second position, the force level is relatively high so as to ensure the connection of the aircraft power connector to the aircraft electrical connector and thereby prevent the inadvertent disconnection of the aircraft power connector from the aircraft electrical connector.

REFERENCES:
patent: 1119864 (1914-12-01), Ovington
patent: 3643202 (1972-02-01), Coon

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