To simplify a structure of an aircraft landing gear including a steering mechanism.SOLUTION: A landing gear 1 includes a shock strut 2 having a cylinder 3 and a piston 4, and a wheel 5 supported by the piston. The shock strut has a steering mechanism 21 for rotating the wheel around a strut shaft Z together with the piston, and a power source of the steering mechanism is an electric motor 6 having a rotor 61 and a stator 62, and the rotor and the stator are coaxial with the strut shaft.SELECTED DRAWING: Figure 1

    【課題】ステアリング機構を備えた航空機の着陸装置の構造を簡略にする。【解決手段】着陸装置1は、シリンダ3とピストン4とを有するショックストラット2と、ピストンに支持された車輪5と、を備え、ショックストラットは、車輪を、ピストンと共に、ストラット軸Zを中心に回動させるステアリング機構21を有し、ステアリング機構の動力源は、回転子61と固定子62とを有する電気モータ6であり、回転子及び固定子は、ストラット軸と同軸である。【選択図】図1


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    Title :

    AIRCRAFT LANDING GEAR


    Additional title:

    航空機の着陸装置


    Contributors:

    Publication date :

    2023-07-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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