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 a stop plate, connected by at least one removable link to the primary structure, which closes the first hole, at least in part.
ATTACHE-MOTEUR D'AÉRONEF COMPRENANT AU MOINS UN SYSTÈME D'IMMOBILISATION EN TRANSLATION D'UN PION DE CISAILLEMENT COMPORTANT UNE PLAQUE D'OBTURATION, PROCÉDÉ DE MONTAGE DE LADITE ATTACHE-MOTEUR ET AÉRONEF COMPRENANT LADITE ATTACHE-MOTEUR
ENGINE MOUNTING STRUCTURE COMPRISING AT LEAST A TRANSLATION FIXING SYSTEM OF A SHEAR PIN COMPRISING A BLANKING PLATE, MOUNTING METHOD OF SUCH A STRUCTURE AND AIRCRAFT COMPRISING SUCH A STRUCUTRE
ANTRIEBSAUFHÄNGUNG BEINHALTEND ZUMINDEST EIN BLINDPLATTEFIXIERUNGSSYSTEM FÜR EINEN SCHERSTIFT, MONTAGEVERFAHREN EINER SOLCHEN AUFHÄNGUNG UND FLUGZEUG BEINHALTEND EINE SOLCHE AUFHÄNGUNG
2021-04-14
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2020
|European Patent Office | 2018
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