The invention relates to the technical field of aircrafts, and especially relates to an aircraft convenient for controlling flight attitude. The aircraft comprises a cabin, a propulsion device arranged at the tail of the cabin and used for controlling the aircraft to move forward, an undercarriage is arranged at the bottom of the cabin, and a power device and a control circuit board are arranged in the cabin and are electrically connected with each other. A flight device and a flight attitude adjusting device are arranged at the top of the cabin, the flight device and the flight attitude adjusting device are respectively driven by a power device, the flight device comprises a first sleeve, a first transmission rod, a first rotating bearing and first rotor wings symmetrically fixed on two sides of the first rotating bearing, and the first sleeve is fixed at the top of the cabin. The upper end of the first transmission rod is fixed to the first rotating bearing, the lower end of the first transmission rod penetrates through the first sleeve and is connected to the power device in the cabin, the power device drives the first transmission rod to vertically reciprocate up and down in the first sleeve, and the flight attitude adjusting device comprises a first control device and a second control device which are symmetrically arranged on the two sides of the flight device.

    本发明涉及飞行器技术领域,特指一种便于控制飞行姿态的飞行器,包括机舱,机舱尾部设有用于控制飞行器前行的推进装置,机舱底部设有起落架,机舱内设有动力装置与控制电路板,动力装置与控制电路板电路连接,机舱顶部设有飞行装置以及飞行姿态调节装置,飞行装置以及飞行姿态调节装置分别通过动力装置驱动,飞行装置包括套筒一、传动杆一、转动轴承一以及对称固定于转动轴承一两侧的旋翼一,套筒一固定于机舱顶部,传动杆一上端固定于转动轴承一,传动杆一下端穿过套筒一,并连接于机舱内的动力装置,动力装置驱动传动杆一在套筒一内作垂直上下往复动作,飞行姿态调节装置包括对称设于飞行装置两侧的第一控制装置与第二控制装置。


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    Title :

    Aircraft convenient for controlling flight attitude


    Additional title:

    一种便于控制飞行姿态的飞行器


    Contributors:

    Publication date :

    2021-03-09


    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 / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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