The reduced thrust takeoff is a practical method for cutting off airplane maintenance costs. To satisfy the various takeoff targets, different types of civil aircrafts have different reduced thrust takeoff functions. Correctly designed thrust reduction function is crucial for the competitiveness of a newly developed aircraft. However, the design of the reduced thrust takeoff function including the coupling of several disciplines, which results in challenges. To solve the problem, the benefits of reduced thrust takeoff under various takeoff conditions are computed. The calculation results are used to discuss the design method of the reduced thrust takeoff function of civil aircrafts.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The benefit and design method of reduced thrust takeoff for civil aircraft


    Contributors:
    Easa, Said (editor) / Wei, Wei (editor) / Wei, Niu (author)

    Conference:

    Eighth International Conference on Electromechanical Control Technology and Transportation (ICECTT 2023) ; 2023 ; Hangzhou, China


    Published in:

    Proc. SPIE ; 12790 ; 1279027


    Publication date :

    2023-09-07





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    The benefit and design method of reduced thrust takeoff for civil aircraft

    Wei, Niu | British Library Conference Proceedings | 2023


    Implementation method of thrust-reduced takeoff function of aircraft

    SHANG LIYING / REN JIANGTAO / ZHANG YANJUN et al. | European Patent Office | 2025

    Free access



    CONTROLLERS AND AIRCRAFT WITH VARIABLE ENGINE THRUST TAKEOFF SYSTEM

    HORNE THOMAS C / LANDERS THOMAS / LAVRISA THOMAS P et al. | European Patent Office | 2022

    Free access