The invention is related to an aircraft with a fuselage that comprises at least one hollow beam element 20, wherein the at least one hollow beam element 20 accommodates at least one hollow duct element 21 that comprises a tubular duct element wall 21a, and wherein at least one protective spacer 22a, 22b, 22c is arranged between the tubular duct element wall 21a and the at least one hollow beam element 20 such that free space 22j is available between the tubular duct element wall 21a and the at least one hollow beam element 20.
AN AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT
FLUGZEUG MIT RUMPFSCHALE MIT MINDESTENS EINEM HOHLEN TRÄGERELEMENT
AÉRONEF COMPRENANT UN FUSELAGE COMPORTANT AU MOINS UN ÉLÉMENT DE POUTRE CREUSE
28.04.2021
Patent
Elektronische Ressource
Englisch
IPC: | 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 / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Aircraft with a fuselage that comprises at least one hollow beam element
Europäisches Patentamt | 2022
|AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT
Europäisches Patentamt | 2018
|AN AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT
Europäisches Patentamt | 2018
|AN AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT
Europäisches Patentamt | 2020
ROTARY WING AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE STRUCTURAL STIFFENED PANEL
Europäisches Patentamt | 2018
|