PROBLEM TO BE SOLVED: To provide a flap for wings for airplanes.SOLUTION: An embodiment comprises: a seal 304 coupled to and extending from a fixed portion of a wing; a high-lift device surface coupled to the wing having an as-built shape. While not in flight, the high-lift device surface in the as-built shape does not make contact with the seal or partially makes contact with the seal such that air can flow between the seal and the high-lift device surface. In one or more flight conditions, the high-lift device surface, under aerodynamic force, deforms from the as-built shape to a second shape such that in the second shape the high-lift device surface fully contacts the seal to prevent an air flow between the seal and the high-lift device surface.SELECTED DRAWING: Figure 5

    【課題】飛行機用の翼用のフラップを提供する。【解決手段】翼の固定部分に結合され、翼の固定部分から延びるシール304と、アズビルト形状を有する、に結合された高揚力装置面とを備え、飛行中でない間、アズビルト形状の高揚力装置面は、空気が前記シールと高揚力装置面との間を流れることができるように、シールと接触しない、またはシールと部分的に接触し、1つ以上の飛行状態において、高揚力装置面は、空気力学的な力を受けて、アズビルト形状から第2の形状に変形し、第2の形状において、高揚力装置面は、シールと高揚力装置面との間の空気の流れを妨げるように、シールと完全に接触する。【選択図】図5


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    Title :

    WING FLAP DEFLECTION CONTROL REMOVAL


    Additional title:

    翼フラップ偏位制御除去



    Publication date :

    2018-08-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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