To maximize lift generation with compact and light wings.SOLUTION: An aircraft includes a fuselage and at least one primary wing. The at least one primary wing has an upper surface, at least one recess in the upper surface, and at least one conduit in fluid communication with the at least one recess. At least one ejector is disposed within the at least one recess and is configured to receive compressed air via the at least one conduit.SELECTED DRAWING: Figure 1

    【課題】小型かつ軽量の翼での揚力発生を最大限にする。【解決手段】航空機は、胴体と、少なくとも1つの主翼とを含み、少なくとも1つの主翼は、上面と、上面内の少なくとも1つの凹部と、少なくとも1つの凹部と流体連通する少なくとも1つの導管とを有する。少なくとも1つのエジェクタは、少なくとも1つの凹部内に配置されており、少なくとも1つの導管を介して圧縮空気を受け取るように構成されている。【選択図】図1


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    Title :

    FLUIDIC PROPULSIVE SYSTEM


    Additional title:

    流体推進システム


    Contributors:

    Publication date :

    2024-10-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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