The analysis of transport category airplane fuselage design features and master geometry modeling methods showed that the methods should be updated to provide quicker automated editing of the model as well as improvement of its quality and accuracy. Transport category airplane fuselage master geometry parametrical modeling method was developed basing on specification requirements, general view drawing, generalised theoretical drawing and fuselage parameters matrix. The method takes in account main geometrical parameters and allows their variation in wide range with automatic model update for providing required characteristics. Proposed method is verified using data of airplanes made by SC “Antonov”. Fuselage parameters influence on its volume and washed surface area was studied. Fuselage master geometry parametrical modeling method implementation in frontend design of passenger airplane for local airlines allowed quick geometrical characteristics determination on early design stage and provide meeting the requirements of specification and aviation regulations.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Transport Category Airplane Fuselage Master Geometry Parametrical Modeling Method


    Additional title:

    Advs in Intelligent Syst., Computing



    Conference:

    International scientific-practical conference ; 2020 ; Chernihiv, Ukraine June 29, 2020 - July 01, 2020



    Publication date :

    2020-08-30


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Transport Airplane Fuselage Section Longitudinal Impact Test

    Wade, Barry / Blaker, Jim / Johnson, Richard et al. | SAE Technical Papers | 1988


    Transport Category Aircraft Fuselage Integrated Design

    Dveirin, Oleksandr / Hrebenikov, Oleksandr / Humennyi, Andriy et al. | Springer Verlag | 2023


    Rear fuselage structure of airplane

    LI HONGYANG / SUN CHAO / ZHU YU et al. | European Patent Office | 2022

    Free access

    Full-Scale Air Transport Category Fuselage Burnthrough Tests

    H. Webster / G. Geyer / D. Do et al. | NTIS | 1990


    Airplane and rear fuselage structure thereof

    WANG BAOSHENG / LI JIANGHAI / LIU WENRUI et al. | European Patent Office | 2024

    Free access