An aircraft pylon comprising an aircraft pylon fairing extending along a longitudinal axis, a primary structure having a peg that is inserted in a through opening of an inner rib of the fairing and four yokes as well as four removable fixing elements that can be inserted from the outside of the fairing. The fixing elements are inserted in a direction perpendicular to said longitudinal axis of the fairing in order to hold in place a fitting of the primary structure that has an oblong through opening and is inserted into one of said yokes of the fairing. Also a method of assembling an aircraft pylon and an aircraft with such a pylon.
CARÉNAGE AMELIORÉ DE MÂT D'AÉRONEF, ENSEMBLE DE CARÉNAGE, MÂT D'AÉRONEF ET AÉRONEF
IMPROVED FAIRING FOR AN AIRCRAFT MAST, FAIRING ASSEMBLY, AIRCRAFT MAST AND AIRCRAFT
VERBESSERTE VERKLEIDUNG FÜR EINEN FLUGZEUGPYLON, VERKLEIDUNGSANORDNUNG, FLUGZEUGPYLON UND FLUGZEUG
2025-06-18
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
CARENAGE AMELIORE DE MÂT D’AERONEF, ENSEMBLE DE CARENAGE, MÂT D’AERONEF ET AERONEF.
European Patent Office | 2024
|European Patent Office | 2019
|European Patent Office | 2020
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