An assembly for an aircraft engine mounting comprising an articulation axis supported by two plain bearings and a blocking device blocking the translation of the articulation axis in a direction which comprises a blocking screw that is screwed, in operation, into a first, tapped internal portion of a tubular extension secured to one of the two plain bearings, a first blocking system comprising an internal elastic stop ring housed in a groove formed in the tubular extension, and a second blocking system comprising a blocking screw which passes through first orifices passing through the second section of the blocking screw and second orifices passing through the tubular extension.
ASSEMBLAGE POUR UNE ATTACHE-MOTEUR D'AERONEF COMPRENANT UN AXE D'ARTICULATION SUPPORTE PAR UNE CHAPE ET IMMOBILE EN TRANSLATION
ASSEMBLY FOR AN AIRCRAFT ENGINE ATTACHMENT COMPRISING A HINGE PIN SUPPORTED BY A YOKE AND IMMOBILE IN TRANSLATION
ANORDNUNG FÜR EINE FLUGZEUG-MOTORBEFESTIGUNG, DIE EINE GELENKACHSE UMFASST, DIE VON EINER GABEL GEHALTEN WIRD UND NICHT VERSCHIEBBAR IST
2020-04-15
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / F16C SHAFTS , Wellen |
European Patent Office | 2020
|European Patent Office | 2015
|European Patent Office | 2015
|European Patent Office | 2021
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