PROBLEM TO BE SOLVED: To provide an active winglet and a controllable airflow modification device that improve efficiency and performance of an aircraft.SOLUTION: An active winglet 100 includes an angled portion 106 on the outer side of a body portion 104, and a controllable airflow modification device 110 in the form of control surfaces 112. The control surfaces are operated by a control system, and the influence of the winglet on the fatigue life of a wing is reduced. Further, the overall load capacity of the wing carrying capability of the aircraft is increased, and thus the gross weight potential of the aircraft is increased.SELECTED DRAWING: Figure 1

    【課題】航空機の効率、性能を改善するアクティブウィングレット及び制御可能空気流修正装置を提供する。【解決手段】アクティブウィングレット100は、本体部分104の外側に傾斜部分106、制御面112の形を取る制御可能空気流修正装置110を含む。制御面は制御システムにより操作され、翼の疲労寿命に与えるウィングレットの影響を削減する。更に、航空機の翼積載能力の総耐荷重も増加し、航空機の総重量の可能性を高める。【選択図】図1


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    Titel :

    AIRCRAFT WING AND CONTROLLABLE AIRFLOW MODIFICATION DEVICE ADJUSTMENT METHOD


    Weitere Titelangaben:

    航空機の翼および制御可能空気流修正装置の調整方法


    Beteiligte:

    Erscheinungsdatum :

    22.06.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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