An aircraft engine attachment connecting an attachment body and a primary structure of an aircraft pylon, the engine attachment comprising a shear pin immobilized in translation by a first immobilization system that comprises a shoulder and a removable stop that are integral with the primary structure, between which a flange of the shear pin is immobilized, and a second immobilization system that comprises, first, a groove positioned in an extension of the shear pin and, second, a fork connected to the primary structure via at least one removable link and interacting during operation with the groove in such a manner as to immobilize the shear pin in translation.
ATTACHE-MOTEUR D'AÉRONEF COMPRENANT AU MOINS UN SYSTÈME D'IMMOBILISATION EN TRANSLATION DE TYPE FOURCHETTE D'UN PION DE CISAILLEMENT, PROCÉDÉ DE MONTAGE DE LADITE ATTACHE-MOTEUR ET AÉRONEF COMPRENANT LADITE ATTACHE-MOTEUR
ENGINE MOUNTING STRUCTURE COMPRISING AT LEAST A YOKE-TYPE TRANSLATION FIXING SYSTEM FOR A SHEAR PIN, MOUNTING METHOD OF SUCH A STRUCTURE AND AIRCRAFT COMPRISING SUCH A STRUCTURE
ANTRIEBSAUFHÄNGUNG BEINHALTEND ZUMINDEST EIN JOCH-BEFESTIGUNGSSYSTEM FÜR EINEN SCHERSTIFT, MONTAGEVERFAHREN FÜR EINER SOLCHEN AUFHÄNGUNG UND FLUGZEUG BEINHALTEND EINE SOLCHE AUFHÄNGUNG
2021-02-24
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2018
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