TOOL FOR HANDLING AN AIRCRAFT ENGINE NACELLE
The present disclosure provides a tooling for handling a nacelle of an aircraft turbojet engine. The tooling includes a gantry having at least one upper support bar which is hinged about at least a first upper axis of rotation (A) by a first upper hinge. The upper support bar is hinged between at le...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Patent |
Sprache: | eng ; fre ; ger |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Schreiben Sie den ersten Kommentar!