The invention discloses a fixed-wing aircraft capable of taking off and landing vertically and a control method thereof.The fixed-wing aircraft comprises a front wing and a rear wing which are fixedly connected to an aircraft body and further comprises a front power device and a rear power device, the front power device is installed on the front wing at a fixed angle, and the rear power device is installed on the rear wing at a fixed angle; the mounting angles of the front wing and the rear wing are both 20-60 degrees, and the included angles between the axes of the front power device and the rear power device and the longitudinal axis of the fuselage are both 20-60 degrees. The front power device and the rear power device are arranged on the front wing and the rear wing, the front power device and the rear power device are installed on the front wing and the rear wing at fixed angles, power devices with tilting axes are not arranged, the complexity and the failure rate of an aircraft power system are greatly reduced, and reliability and safety are improved. The invention caan realize vertical take-off and landing, and has the absolute advantages of high cruise efficiency, long voyage, large load, simplicity in manufacturing, low cost and the like.

    本发明公开了一种可垂直起降的固定翼飞机及其控制方法,所述固定翼飞机包括固定连接在机身上的前机翼和后机翼,还包括前动力装置和后动力装置,前动力装置以固定角度安装在前机翼上,后动力装置以固定角度安装在后机翼上,所述前机翼和后机翼的安装角均为20‑60度,前动力装置和后动力装置的轴线与机身纵轴线之间的夹角均为20‑60度。本发明在前后机翼上分别设置前后动力装置,且前后动力装置均以固定角度安装在前后机翼上,不设置轴线可倾转的动力装置,大大降低了飞机动力系统的复杂性和故障率,提高了可靠性和安全性。本发明可实现垂直起降,具有巡航效率高、航程远、载荷大、制造简单、成本低等绝对优势。


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    Title :

    Fixed-wing aircraft capable of taking off and landing vertically and control method thereof


    Additional title:

    可垂直起降的固定翼飞机及其控制方法


    Contributors:
    WANG LIN (author)

    Publication date :

    2021-12-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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