Aircraft grounding receptacle

Geometrical instruments

Patent

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Details

361215, H01R 466

Patent

active

045416842

ABSTRACT:
An aircraft grounding receptacle comprising a connector portion and a tubular portion. The connector portion includes an external thread and a hexagonal portion. The tubular portion includes a reduced diameter portion and a hexagonal flange. Four slots separate the tubular portion into four segments and intersect the flange at locations spaced apart from four of the six points comprising the hexagonal shape of the flange. A bore extends through the body for receiving an aircraft grounding plug and includes reduced diameter portions for mating engagement with the terminal groove of the plug.

REFERENCES:
patent: 1564855 (1925-12-01), Jurs
patent: 1564925 (1925-12-01), Anthony
patent: 1749179 (1930-03-01), Davis, Jr.
patent: 1785729 (1930-12-01), Davis, Jr.
patent: 2434534 (1948-01-01), Alford
patent: 2958843 (1960-11-01), Long
patent: 3038972 (1962-06-01), Lagier
patent: 3145329 (1964-08-01), Deakin et al.
patent: 3258734 (1966-06-01), Greasley

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