Disclosed is an aircraft tail comprising:-a rear fuselage section,-an adjustable horizontal tail plane comprising a first lateral torsion box and a second lateral torsion box, each torsion box comprising a front spar and a rear spar,-a front fitting and a rear fitting,-an actuator,-a rear fuselage section,-an adjustable horizontal tail plane comprising a first lateral torsion box and a second lateral torsion box, each torsion box comprising a front spar and a rear spar, and an actuator acting on the front fitting for rotating the adjustable horizontal tail plane about a hinge axis passing through the rear fitting,-the front fitting comprising a first front fitting unit and a second front fitting unit connected to a front spar of the lateral torsion box, and-the actuator comprises a first actuator unit and a second actuator unit, each actuator unit acting on the first front fitting unit and the second front fitting unit, respectively.

    披露了一种飞行器尾翼,所述飞行器尾翼包括:‑后机身区段,‑可调水平尾翼平面,所述可调水平尾翼平面包括第一侧向抗扭箱和第二侧向抗扭箱,每个抗扭箱包括前翼梁和后翼梁,‑前配件和后配件,‑致动器,所述致动器作用在所述前配件上,用于使所述可调水平尾翼平面围绕经过所述后配件的铰接轴线旋转,‑所述前配件包括第一前配件单元和第二前配件单元,所述第一前配件单元和所述第二前配件单元连结到所述侧向抗扭箱的前翼梁,并且‑所述致动器包括第一致动器单元和第二致动器单元,每个致动器单元分别作用在所述第一前配件单元和所述第二前配件单元上。


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    Title :

    Aircraft empennage


    Additional title:

    飞行器尾翼


    Contributors:

    Publication date :

    2022-09-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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