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A hinge for an aircraft power distribution system unit is provided. The unit has a housing comprising a first housing part and a second housing part. The hinge comprises a first hinge member for connection to the first housing part of the unit; and a second hinge member for connection to the second housing part of the unit, wherein the first and the second hinge members comprise an electrically conductive material and wherein the first and the second hinge members are connectable to one another to establish an electrical connection between the first and the second hinge members and to allow relative rotation between the first and the second hinge members.
A hinge for an aircraft power distribution system unit is provided. The unit has a housing comprising a first housing part and a second housing part. The hinge comprises a first hinge member for connection to the first housing part of the unit; and a second hinge member for connection to the second housing part of the unit, wherein the first and the second hinge members comprise an electrically conductive material and wherein the first and the second hinge members are connectable to one another to establish an electrical connection between the first and the second hinge members and to allow relative rotation between the first and the second hinge members.
ELECTRICAL HINGE CONNECTOR
ELEKTRISCHER GELENKVERBINDER
CONNECTEUR ÉLECTRIQUE DE CHARNIÈRE
WORLEY ANDREW (author)
2016-03-23
Patent
Electronic Resource
English
IPC:
H01R
Elektrisch leitende Verbindungen
,
ELECTRICALLY-CONDUCTIVE CONNECTIONS
/
E05D
Scharniere oder andere Aufhängevorrichtungen für Türen, Fenster oder Flügel
,
HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS, OR WINGS
/
H02G
INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
,
Verlegen oder Installieren elektrischer Kabel oder Leitungen, Verlegen oder Installieren kombinierter optischer und elektrischer Kabel oder Leitungen