The invention relates to a helicopter crossed forward and reverse rotor wing parallel driving device. The device comprises a support assembly, rotor wing assemblies and a transmission assembly; the rotor wing assemblies are symmetrically connected to the left side and the right side of the upper portion of the support assembly through revolute pairs and incline outwards by a certain angle; the transmission assembly is arranged in the middle of the interior of the support assembly; the two sides of the transmission assembly are connected with the corresponding rotor wing assemblies; a driver isfixed to the bottom of the support assembly and is in coaxial key connection with the bottom of the transmission assembly; the outer side of the middle of the support assembly is connected with a base through a ball sleeve; the middle of the base is connected with the ball sleeve through a ball pair; the ball sleeve is connected with the outer side of the middle of the support assembly through acylinder pair; and linear driving rod assemblies are circumferentially and evenly distributed between the base and the bottom of the support assembly. According to the device, gears are driven by thedriver to drive the rotor wing assemblies to rotate forwards and backwards in a meshed transmission mode, empennage transmission can be avoided, and cross rotation interference of the rotor wing assemblies is prevented; the linear driving rods drive the support assembly to swing in a three-dimensional mode, the synchronous swing of the rotor wing assemblies is guaranteed, and flight directions canbe flexibly changed.

    直升机交叉式正反转旋翼并联驱动装置,包括支架组件、旋翼组件和传动组件,所述旋翼组件分别对称转动副联接在支架组件上部左右两侧且向外倾斜一定角度,所述传动组件设置在支架组件内中部且两侧分别与旋翼组件连接;所述支架组件底部固定有驱动器,所述驱动器与传动组件底部同轴键连接;所述支架组件中部外侧通过球套连接有机座,所述机座中部与球套球副联接,所述球套与支架组件中部外侧圆柱副联接;所述机座与支架组件底部之间圆周均布直线驱动杆组件。本装置通过驱动器驱动各齿轮啮合传动带动旋翼组件正反旋转,既可免除尾翼传动,又防止旋翼组件交叉转旋干涉;直线驱动杆驱动支架组件三维摆动,保证旋翼组件同步摆动,灵活改变飞行方向。


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    Title :

    Helicopter crossed forward and reverse rotor wing parallel driving device


    Additional title:

    直升机交叉式正反转旋翼并联驱动装置


    Contributors:
    LU YI (author) / LU YANG (author) / YE NIJIA (author)

    Publication date :

    2020-08-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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