An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house a threaded shank of one of the connecting elements. The engine mount comprises a transverse nut which comprises at least two bodies joined together each having a tapped hole configured to engage with one of the threaded shanks.
ATTACHE MOTEUR D'AERONEF COMPRENANT AU MOINS UN ECROU TRANSVERSAL ET AERONEF COMPRENANT LADITE ATTACHE MOTEUR
AIRCRAFT ENGINE MOUNT COMPRISING AT LEAST ONE TRANSVERSE NUT AND AIRCRAFT COMPRISING SAID ENGINE MOUNT
MOTORBEFESTIGUNG FÜR LUFTFAHRZEUG, DIE MINDESTENS EINE QUER VERLAUFENDE MUTTER UMFASST, UND LUFTFAHRZEUG, DAS DIESE MOTORBEFESTIGUNG UMFASST
2020-03-04
Patent
Elektronische Ressource
Französisch
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 |
Europäisches Patentamt | 2018
|