This invention provides construction variants of a cruise miniflap that is added to the trailing edge flap of an aircraft wing and can be used for improving the aerodynamic properties of an aircraft. In the rear edge of the cruise miniflap, it has a cavity with a height of up to 1 % of the wing chord.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT WING COMPRISING CRUISE MINI FLAPS


    Additional title:

    FLUGZEUGFLÜGEL UMFASSEND FLUGMINIKLAPPEN
    AILE D'AÉRONEF COMPRENANT DES MINI-VOLETS DE CROISIÈRE


    Contributors:
    LAUK PEEP (author)

    Publication date :

    2020-12-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Wing flaps in light aircraft design

    Garbell, M.A. | Engineering Index Backfile | 1945


    Cruise miniflaps for aircraft wing

    LAUK PEEP | European Patent Office | 2019

    Free access

    Wing Flaps

    Online Contents | 1999


    AIRCRAFT WING FLAPS HAVING AERODYNAMIC RESTORATION DOORS

    MILLIGAN ERIC / GRUNER BRYAN JACOB | European Patent Office | 2023

    Free access

    SLOTTED WING FLAPS FOR A VTOL AIRCRAFT

    KAREM ABE / PARCELL JOHN PAUL | European Patent Office | 2020

    Free access