CURRENT SUPPLY SYSTEM FOR AIRCRAFT

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
1. Verfasser: SCHULZ, HANS EGMUND
Format: Patent
Sprache:eng ; ger
Schlagworte:
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