The present invention refers to a pylon assembly (7) for attaching engines (2) to an aircraft fuselage (8), the pylon assembly (7) comprising first and second elongated boxes (7a,7b), aligned longitudinally with respect to an axis (X) and assembled to each other, wherein the first box (7a) has an outer section (7ao) and an inner section (7ai), the inner section (7ai) having a tubular configuration, wherein the second box (7b) has an outer section (7bo) and an inner section (7bi), wherein the inner section is inserted inside the inner section of the first box. First and second boxes (7a,7b) are configured such as the inner section of the second box is tightly fitted inside the inner section of the first box, thereby in the mechanical coupling between the two boxes is achieved simply by the tight contact between the two boxes, without the need of fastenings for load transfer.
AIRCRAFT PYLON ASSEMBLY
FLUGZEUGPYLONANORDNUNG
ENSEMBLE DE MÂT D'AÉRONEF
2017-06-21
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Improved aircraft pylon fairing, fairing assembly, aircraft pylon and aircraft
Europäisches Patentamt | 2024
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