The present invention relates to a landing apparatus for an aircraft and, more specifically, relates to a landing apparatus for an aircraft, in which a weight thereof is reduced through change of a steering system, and a structure thereof is simplified. According to the landing apparatus for an aircraft of the present invention, a piston assembly of the landing apparatus is directly rotated by using a steering motor, thereby simplifying the configuration of the steering system. In addition, according to the landing apparatus for an aircraft of the present invention, the steering system is simplified, thereby reducing the weight thereof. In addition, according to the landing apparatus for an aircraft of the present invention, external components of the steering system are disposed in the landing apparatus, thereby avoiding an interference problem caused by components of the steering system at the time of folding the landing apparatus.

    본 발명은 항공기용 착륙장치에 대한 것으로, 보다 구체적으로는 조향시스템의 변경을 통해 중량이 절감되고, 구조가 단순화된 항공기용 착륙장치에 관한 것이다. 본 발명의 항공기용 착륙장치에 의하면 조향모터를 이용하여 착륙장치의 피스톤조립체를 직접 회전시킴으로써 조향시스템의 구성을을 단순화시킬 수 있는 효과가 있다. 또한, 본 발명의 항공기용 착륙장치에 의하면 조향시스템을 단순화시킴으로써 중량을 절감시킬 수 있는 효과가 있다. 또한, 본 발명의 항공기용 착륙장치에 의하면 외부에 있던 조향시스템 구성품들을 착륙장치의 내부에 배치시킴으로써 착륙장치 접힘 시 조향시스템 구성품에 의한 간섭 문제를 회피할 수 있는 효과가 있다.


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    Titel :

    Landing device for air plane


    Weitere Titelangaben:

    항공기용 착륙장치


    Beteiligte:
    LEE JEONG SUN (Autor:in)

    Erscheinungsdatum :

    10.03.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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