DE3517301

In an aircraft power supply system with heavy-duty conductors, it is proposed to couple these via plug-in connection members in the area of a control section in order to reduce failure times. A cable head is preferably used which is detachably attached to the control section and automatically produc...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	ROESSLER, RALF, 6000 FRANKFURT, DE, SCHULZ, HANS EGMUND., 6085 NAUHEIM, DE
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	In an aircraft power supply system with heavy-duty conductors, it is proposed to couple these via plug-in connection members in the area of a control section in order to reduce failure times. A cable head is preferably used which is detachably attached to the control section and automatically produces the electrical plug-in connection with corresponding members in the control section. At the same time, the cable head can have a lateral receiving member on which a hook of a multiple socket part connected to the cable head via cable can be hooked in. As a result, the clear height below a passenger bridge can be reduced when the power supply device is not being used.