Patent ID: 6322398
Filing Date: 2001-11-27
Classification: H01R

Abstract:
A plug connector (10, 106) of an aircraft power supply device for the on-board power supply of aircraft, comprising a housing (12), divided so that it can be separated into at least a first section (14, 104) and a second section (16, 106) in a longitudinal direction, said first section, constituting a front housing element (14, 104), having cylindrical first contact elements (24) releasably connectable with cylindrical second contact elements (32), extending from the second section (16, 106) of the housing, said second section forming a rear element, wherein the second contact elements are connected with strands of a cable and encapsulated after having been connected, wherein the front housing element (104) comprises an outer shell body (118) and an insert (120) releasably arranged therein, said insert further comprising a plurality of hollow-cylindrical receivers (122, 124, 126) for said first contact elements (24) substantially separated from each other and said housing by at least one air gap.