Provided is an aircraft wing (100) with a spoiler (101), the spoiler (101) is being movable from a reference position with a deflection angle ± ref to a given target deflection angle ± target by an actuator powered mechanism (102). The aircraft wing (100) is characterized in that the spoiler (101) is interconnected with the aircraft wing exclusively via a strip element (103) and via the actuator powered mechanism (102), wherein an upstream edge of the spoiler (101) is being interconnected with the aircraft wing (100) exclusively via the strip element (103) made of a resiliently flexible material, wherein a downstream edge of the strip element (103) is extending along the whole upstream edge of the spoiler (101) or at least along a major part of the upstream edge of the spoiler (101) and wherein a whole upstream edge of the strip element is connected to an upper surface of the aircraft wing, and the actuator powered mechanism (102) is constructed and arranged such that, while moving the spoiler (101) from the reference angle ± ref to the given target deflection angle ± target , the strip element (103) is being bent with a constant strain along the strip element (103), wherein a cross-section of the strip element (103) for all deflection angles ± assumes the form of a ring segment with a radius R(±) at least within a given margin of failure, with ±, ± target , ± ref [-± 1 ; ± 2 ].


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT WING WITH SPOILER


    Weitere Titelangaben:

    FLUGZEUGFLÜGEL MIT SPOILER
    AILE D'AERONEF AVEC PANNEAU DEPORTEUR


    Beteiligte:
    HANSEN HEINZ (Autor:in) / KIRN JOHANNES (Autor:in) / MACHUNZE WOLFGANG (Autor:in) / METZNER CHRISTIAN (Autor:in) / WEBER MARKUS J (Autor:in)

    Erscheinungsdatum :

    2019-07-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT WING WITH SPOILER

    HANSEN HEINZ / KIRN JOHANNES / MACHUNZE WOLFGANG et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT WING, METHOD OF DEPLOYING A SPOILER AND METHOD OF RETRACTING A SPOILER

    BENJAMIN BISHOP / ANTHONY BRYANT | Europäisches Patentamt | 2022

    Freier Zugriff

    Fixing device of spoiler wing, spoiler wing assembly and vehicle

    LI ZERONG / LONG SHUAI / CHEN JIN | Europäisches Patentamt | 2023

    Freier Zugriff

    Energy-harvesting spoiler on a wing of an aircraft

    SIEGMETH JEFF S | Europäisches Patentamt | 2023

    Freier Zugriff

    ENERGY-HARVESTING SPOILER ON A WING OF AN AIRCRAFT

    SIEGMETH JEFF S | Europäisches Patentamt | 2020

    Freier Zugriff