Aircraft comprising a landing gear with controlled detachment in the event of an accident

On an aircraft, particularly of the commercial type, a landing gear (16) placed in front of a fuel tank (18) comprises a rod system (32) capable of coming into contact with a sliding rail (52) formed on a reinforced structural part (48) of the aircraft, in the event of accidental tilting of the gear...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: DAZET FRANCIS, MAURIN ANDRé
Format: Patent
Sprache:eng
Schlagworte:
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