An aircraft pylon comprising a primary structure and a pipe segment having an internal duct positioned inside at least one structural tube primary structure. This solution makes it possible to reduce the crowding outside the structural tubes of the primary structure, makes it easier to integrate other equipment inside the pylon, and may help to improve the aerodynamic performance of the pylon by reducing its cross section.
MÂT D'AÉRONEF COMPRENANT UNE STRUCTURE PRIMAIRE TUBULAIRE INTÉGRANT AU MOINS UNE CANALISATION À DOUBLE PEAU ET AÉRONEF COMPORTANT AU MOINS UN TEL MÂT
AIRCRAFT MAST COMPRISING A TUBULAR PRIMARY STRUCTURE INCLUDING AT LEAST ONE PIPE WITH DOUBLE SKIN AND AIRCRAFT CONTAINING AT LEAST ONE SUCH MAST
FLUGZEUGMAST MIT EINER ROHRFÖRMIGEN PRIMÄRSTRUKTUR, DIE MINDESTENS EINE DOPPELWANDIGE ROHRLEITUNG UMFASST, UND FLUGZEUG MIT MINDESTENS EINEM SOLCHEN MAST
2023-05-03
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2022
|MATELAS D'ISOLATION D'AERONEF INTEGRANT AU MOINS UNE CANALISATION DE CONDITIONNEMENT D'AIR
European Patent Office | 2024
|CANALISATION D'AERONEF A DOUBLE PEAU EQUIPEE D'AU MOINS UN DISPOSITIF DE REVELATION DE FUITE
European Patent Office | 2021
|