Engine suspension device to an aircraft structure

Engine suspension device to an aircraft structure

The system has a connection unit connected between a span wise beam (1010) and a fitting (1003) and including an eccentric body (1013) housed in a bore of the span wise beam. The eccentric body is fixed rotatively around a primary axis with a trunnion fixed to the fitting. An axis is eccentric with...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: TESNIERE, MARC PATRICK, NOIRCLERC, GABRIEL, CHEVALIER, LYDIE MARIE HELENE
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The system has a connection unit connected between a span wise beam (1010) and a fitting (1003) and including an eccentric body (1013) housed in a bore of the span wise beam. The eccentric body is fixed rotatively around a primary axis with a trunnion fixed to the fitting. An axis is eccentric with respect to the primary axis of rotation. The trunnion is mounted on the eccentric body using a bearing.