An aircraft subassembly (100) comprises a fuselage structure (102), comprising a first side (108) and a second side (114). The aircraft subassembly (100) further comprises a main-landing-gear system (104), having a single pair of wheels (107). The main-landing-gear system (104) additionally comprises a sponson (130), connected to and extending outward from the fuselage structure (102). The sponson (130) comprises a central portion (131) and a first main-landing-gear door (140) that is moveable relative to the central portion (131) between, inclusively, a closed position and an open position. The sponson (130) further comprises a second main-landing-gear door (142) that is moveable relative to the central portion (131) between, inclusively, a closed position and an open position. The main-landing-gear system (104) further comprises a first main-landing-gear assembly (106), connected to the first wheel (110) and a second main-landing-gear assembly (112), connected to the second wheel (116).


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    Titel :

    AIRCRAFT SUBASSEMBLY, HAVING MAIN-LANDING-GEAR ASSEMBLY AND SPONSON, HOUSING MAIN-LANDING-GEAR ASSEMBLY


    Weitere Titelangaben:

    FLUGZEUGBAUGRUPPE, MIT HAUPTFAHRWERKSANORDNUNG UND SPONSON, WELCHER DIE HAUPTFAHRWERKANORDNUNG AUFNIMMT
    SOUS-ENSEMBLE D'AÉRONEF COMPORTANT UN TRAIN D'ATTERRISSAGE PRINCIPAL ET UN CAISSON LATÉRAL ABRITANT L'ENSEMBLE DE TRAIN D'ATTERRISSAGE PRINCIPAL


    Beteiligte:

    Erscheinungsdatum :

    28.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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