A circulation control aircraft rotor blade having a spanwise Coanda surface 16 and a plurality of spanwise extending flexible composite material panels 18 cooperating with the surface to define slots for the discharge of compressed air from within the blade with each panel having first flexure means 60 associated with screw adjustments 36 for establishing a slot opening preload and second flexure means 62 associated with screw adjustments 38 for establishing a slot maximum opening.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Rotor blade construction for circulation control aircraft


    Contributors:

    Publication date :

    1986-12-02


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    MISSION-ADAPTIVE ROTOR BLADE WITH CIRCULATION CONTROL

    VAN DER WESTHUIZEN JACOB JOHANNES | European Patent Office | 2016

    Free access

    Mission-adaptive rotor blade with circulation control

    VAN DER WESTHUIZEN JACOB JOHANNES | European Patent Office | 2017

    Free access

    Rotor blade for aircraft

    KOBAYASHI WATARU / YAMANE HOKUTO / HAYASHI HIROTAKA et al. | European Patent Office | 2022

    Free access

    Single-blade aircraft rotor

    SIMON JEAN-MICHEL / CHEMOUNI LOUIS | European Patent Office | 2024

    Free access

    AIRCRAFT ROTOR BLADE INSERT

    THOMAS JUSTIN / KOPANSKI KRZYSZTOF / SCOTT MARK W | European Patent Office | 2020

    Free access