In this paper, a complete simulation model of steering system of nose landing gear and towbarless traction is established based on LMS Virtual.Lab Motion. And the B737-800 aircraft was taken as the research object to simulate the steering condition of the towbarless traction. The load of the steering system of the nose gear are simulated and analyzed under various steering conditions. The simulation results show the influence of the changes in the steering angle, steering rate and traction rate on the steering system, and provide some reference for further research on the safety of towbarless traction.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Analysis of effects on the steering system of nose landing gear by towbarless traction


    Beteiligte:
    Kong, Xiangjie (Herausgeber:in) / Falcone, Francisco (Herausgeber:in) / Huang, Hao (Autor:in) / Liu, Hui (Autor:in) / Mu, Mengxin (Autor:in)

    Kongress:

    3rd International Conference on Internet of Things and Smart City (IoTSC 2023) ; 2023 ; Chongqing, China


    Erschienen in:

    Proc. SPIE ; 12708


    Erscheinungsdatum :

    14.06.2023





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Analysis of effects on the steering system of nose landing gear by towbarless traction

    Huang, Hao / Liu, Hui / Mu, Mengxin | British Library Conference Proceedings | 2023


    Aircraft nose landing gear steering test mechanism

    LI SHUTIAN / ZHU YUNLI / LIU ZHIJUN et al. | Europäisches Patentamt | 2021

    Freier Zugriff