Device for suspending a turbine engine from an airplane

A device for suspending a turbojet casing, the device including a shouldered pin extending through aligned orifices of two lugs of a clevis secured to the casing. A protection piece for providing protection against wear is mounted on each lug of the clevis and has the shouldered pin passing therethr...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MARTIN ARNAUD, EVAIN GAËL, LEUTARD FLORENCE IRÈNE NOËLLE, DURAND DIDIER NOËL
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A device for suspending a turbojet casing, the device including a shouldered pin extending through aligned orifices of two lugs of a clevis secured to the casing. A protection piece for providing protection against wear is mounted on each lug of the clevis and has the shouldered pin passing therethrough, the protection piece being prevented from moving in rotation on the lug by co-operating shapes.