Patent ID: 6709274
Filing Date: 2004-03-23
Classification: H01R

Abstract:
An aircraft high performance external power connector and its assembly for use at ground electrical supplies, said power connectors and its assembly comprising:an aircraft fixed receptacle connector having a multiplicity of 120 KVA hermaphrodite power contacts and relay socket contacts, said power contacts independently surrounded by boss like creepage barrier tubes; a ground supply free plug connector having (i) a body portion and a connection portion, said body portion holding and retaining said multiplicity of 120 KVA hermaphrodite power contacts and conventional relay pin contacts, and said connection portion having an environmentally sealing cable clamp or backshell threadedly connected onto said body portion; (ii) a reinforced boss which houses a latch pin with a circumferentially machined groove located at its front end; and (iii) a full metal housing around a dielectric body portion, said full metal housing comprising of a set of doors attached to a set of hinge springs which are connected to a slide link, (iv) a spring-loaded actuator pin which is centrally located at the seams on said doors that controls the forward and rearward movement slide link of a metal housing.