The present invention provides a hatch locking device (100) for an aircraft or spacecraft hatch (10), comprising: a drivable spindle drive (101) which extends in a longitudinal axis (X) and is fixed in relation to a hatch frame (11) of the aircraft or spacecraft hatch (10) along the longitudinal axis (X); at least one locking bolt (102) which is driven by the drivable spindle drive (101) and is guided along the longitudinal axis (X); and at least one adjustment bush assembly (110) being mounted on a fuselage frame (1) and comprising a first eccentric bush (111) having a bolt receptacle (112) which is oriented centrally along the longitudinal axis (X) for receiving the at least one locking bolt (102) such that the hatch locking device (100) is positive-locking connectable in two axles (Y, Z) both being perpendicular to the longitudinal axis (X). Further the present invention provides an aircraft or spacecraft hatch (10) comprising such hatch locking device (100) as well as an aircraft (A) comprising such aircraft or spacecraft hatch (10).


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    Titel :

    HATCH LOCKING DEVICE, AIR- OR SPACECRAFT HATCH AND AIR- OR SPACECRAFT


    Weitere Titelangaben:

    KLAPPENVERRIEGELUNGSVORRICHTUNG, LUFT- ODER RAUMFAHRZEUGKLAPPE UND LUFT- ODER RAUMFAHRZEUG
    DISPOSITIF DE VERROUILLAGE DE TRAPPE, TRAPPE D'AIR OU D'ENGIN SPATIAL ET ENGIN SPATIAL


    Beteiligte:
    OHLE SÖREN (Autor:in)

    Erscheinungsdatum :

    18.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / E05B LOCKS , Schlösser



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