A rotary wing aircraft (100) extending along an associated roll axis (R) between a nose region (101) and an aft region (102) and that comprises a fuselage (110) with a front section (112) and a rear section (114), the rotary wing aircraft (100) comprising: a main rotor (120) that is rotatably mounted at the front section (112), and a stabilizer arrangement (130) that is arranged at the rear section (114) in the aft region (102), wherein the rear section (114) extends between the front section (112) and the stabilizer arrangement (130) and comprises an asymmetrical cross-sectional profile (190) in direction of the associated roll axis (R).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    A ROTARY WING AIRCRAFT WITH A STABILIZER ARRANGEMENT


    Weitere Titelangaben:

    DREHFLÜGELFLUGZEUG MIT EINER STABILISATORANORDNUNG
    AÉRONEF À VOILURE TOURNANTE COMPORTANT UN AGENCEMENT DE STABILISATEUR


    Beteiligte:
    PFALLER RUPERT (Autor:in) / RIES TOBIAS (Autor:in)

    Erscheinungsdatum :

    08.11.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotary wing aircraft with a stabilizer arrangement

    PFALLER RUPERT / RIES TOBIAS | Europäisches Patentamt | 2024

    Freier Zugriff

    ROTARY WING AIRCRAFT WITH A STABILIZER ARRANGEMENT

    PFALLER RUPERT / RIES TOBIAS | Europäisches Patentamt | 2022

    Freier Zugriff

    ROTARY-WINGED AIRCRAFT WITH STABILIZER WING

    EMBACHER MARTIN / RIES TOBIAS / ECKERT CHRISTIAN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Pitch stabilizer and rotary-wing aircraft equipped with such stabilizer

    BEROUL FREDERIC | Europäisches Patentamt | 2015

    Freier Zugriff

    ROTARY WING AIRCRAFT WITH A FIREWALL ARRANGEMENT

    FINK AXEL / KEMPF MANUEL | Europäisches Patentamt | 2021

    Freier Zugriff