A rotorcraft comprising a fuselage forming at least one lower lateral fuselage compartment with at least a first fitting, a second fitting, and a third fitting; and at least one non-retractable wheel-type landing gear that comprises: at least one wheel; a shock absorber with a shock absorber tube having an open end and an axially opposed closed end, and a shock absorber rod telescopically mounted to the shock absorber tube via the open end; a first fixation provided close to the open end on the shock absorber tube and connected to the first fitting; a second fixation provided close to the closed end on the shock absorber tube and connected to the second fitting; and a third fixation provided close to the closed end on the shock absorber tube and connected to the third fitting.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR


    Beteiligte:
    FINK AXEL (Autor:in) / OIOLI-NETO REYNALDO (Autor:in)

    Erscheinungsdatum :

    05.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotorcraft with a non-retractable wheel-type landing gear

    FINK AXEL / OIOLI-NETO REYNALDO | Europäisches Patentamt | 2025

    Freier Zugriff

    Rotorcraft with a non-retractable wheel-type landing gear

    FINK AXEL / ACHARD AURELIEN / BERTIN DIDIER | Europäisches Patentamt | 2025

    Freier Zugriff

    ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR

    FINK AXEL / ACHARD AURELIEN / BERTIN DIDIER | Europäisches Patentamt | 2024

    Freier Zugriff

    ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR

    FINK AXEL / ACHARD AURELIEN / BERTIN DIDIER | Europäisches Patentamt | 2024

    Freier Zugriff

    NON-RETRACTABLE WHEEL-TYPE LANDING GEAR FOR A ROTORCRAFT

    FINK AXEL / OIOLI-NETO REYNALDO / BERTIN DIDIER | Europäisches Patentamt | 2024

    Freier Zugriff