The aircraft comprises a fuselage, side wings are fixed to the left side and the right side of the fuselage, first mounting holes are formed in the front faces of the two side wings, a lifting propeller is fixed between the inner walls of the first mounting holes, an empennage is fixed to the bottom face of the fuselage, an overturning groove is formed in the front face of the empennage, and a sliding groove is formed in the empennage; connecting shafts are slidably connected into the sliding grooves, a driving bin is fixed between the connecting shafts, a dual-purpose propeller is rotatably connected to the bottom face of the driving bin, and an adjusting mechanism is arranged in the empennage. During use, the dual-purpose propeller is adjusted through the adjusting mechanism to enable the transmission shaft of the dual-purpose propeller to be in a vertical state, at the moment, the fuselage is started to drive the dual-purpose propeller and the lifting propeller to assist the fuselage in vertical take-off, after take-off is stable, the adjusting mechanism adjusts the dual-purpose propeller to enable the transmission shaft of the dual-purpose propeller to be in a horizontal state, and at the moment, the dual-purpose propeller horizontally propels the fuselage. Therefore, vertical take-off and parallel flight dual-purpose power output is achieved.

    本发明涉及一款具有多功能固定翼飞行器,包括机身,机身的左右两侧均固定有侧翼,两个侧翼的正面均开设有第一安装孔,第一安装孔内壁之间固定有升降螺旋桨,机身的底面固定有尾翼,尾翼的正面开设有翻转槽,尾翼内开设有滑槽,滑槽内滑动连接有连接轴,连接轴之间固定有驱动仓,驱动仓的底面转动连接有两用螺旋桨,尾翼内设有调节机构。在使用时,通过调节机构调节两用螺旋桨,使其传动轴呈垂直状态,此时,启动机身带动两用螺旋桨与升降螺旋桨辅助机身垂直起飞,当起飞稳定后,调节机构调节两用螺旋桨,使其传动轴呈水平状态,此时,两用螺旋桨水平推进机身,从而实现垂直起飞和平行飞行两用动力输出。


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    Titel :

    Multifunctional fixed wing aircraft


    Weitere Titelangaben:

    一款具有多功能固定翼飞行器


    Beteiligte:
    NING LISHUANG (Autor:in)

    Erscheinungsdatum :

    2023-01-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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