A vehicle includes a body and at least one wing coupled to the body. A source of compressed fluid is coupled to the body. The vehicle further includes first and second propellers, each of the first and second propellers having an air intake structure, and each of the first and second propellers is in fluid communication with the source. The first thruster is coupled to the main body and the second thruster is coupled to the at least one wing. The first and second propellers, when in a first configuration, are positioned such that at least a portion of a boundary layer resulting from movement of the vehicle is drawn by the air intake structures of the first and second propellers. The vehicle further includes a system for selectively providing the compressed fluid to the first and second propellers.

    一种运载工具包含主体和联接到所述主体的至少一个机翼。压缩流体源联接到所述主体。所述运载工具进一步包含第一和第二推进器,每个所述第一和第二推进器具有进气结构,并且每个所述第一和第二推进器与所述源进行流体连通。所述第一推进器联接到所述主体,并且所述第二推进器联接到所述至少一个机翼。所述第一和第二推进器在第一配置中时被定位成使得由于所述运载工具的运动而产生的边界层的至少一部分由所述第一和第二推进器的所述进气结构吸入。所述运载工具进一步包含用于将所述压缩流体选择性地提供给所述第一和第二推进器的系统。


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    Title :

    Streamlined fuselage with boundary suction fluid propulsion elements


    Additional title:

    具有边界吸入流体推进元件的流线型机身


    Contributors:

    Publication date :

    2024-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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