To reduce the weight of a wing structure and that of an aircraft, which include a movable wing configured to introduce air into a gap formed between the movable wing and a stationary wing.SOLUTION: A wing structure according to an embodiment is for an aircraft, and includes a stationary wing, a movable wing disposed such that a gap is always formed between the movable wing and the stationary wing, and at least one plasma actuator for controlling an air flow formed in the gap. An aircraft according to an embodiment includes the above-described wing structure. A method for controlling a movable wing according to an embodiment is for a wing structure for an aircraft, in which the movable wing is disposed such that a gap is always formed between the movable wing and a stationary wing, and the method comprises using at least one plasma actuator to control an air flow formed in the gap.SELECTED DRAWING: Figure 1

    【課題】静翼との間に形成される隙間に空気を導くようにした動翼を備えた翼構造体及び航空機の重量を軽減することである。【解決手段】実施形態に係る翼構造体は、航空機用の翼構造体であって、静翼と、前記静翼との間に常時隙間が形成されるように配置される動翼と、前記隙間に形成される空気の流れを制御するための少なくとも1つのプラズマアクチュエータとを備えるものである。また、実施形態に係る航空機は、上述した翼構造体を備えたものである。また、実施形態に係る動翼の制御方法は、静翼との間に常時隙間が形成されるように動翼が配置される航空機用の翼構造体の制御方法であって、少なくとも1つのプラズマアクチュエータを用いて前記隙間に形成される空気の流れを制御するものである。【選択図】 図1


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    Title :

    WING STRUCTURE, METHOD FOR CONTROLLING WING STRUCTURE, AND AIRCRAFT


    Additional title:

    翼構造体、翼構造体の制御方法及び航空機


    Contributors:

    Publication date :

    2019-10-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / H05H Plasmatechnik , PLASMA TECHNIQUE



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