PROBLEM TO BE SOLVED: To provide a landing gear deploying device for an aircraft, which can perform deploying and shock-absorbing of a landing gear of the aircraft with a simpler configuration.SOLUTION: A landing gear deploying device 1 for an aircraft has an expansion and contraction mechanism 3 and a motor 4. The expansion and contraction mechanism is connected to a landing gear 2A of the aircraft to deploy and store the landing gear and absorb a shock on the landing gear. The motor expands and contracts the expansion and contraction mechanism. In a method of deploying a landing gear of an aircraft, deployment and storage of the landing gear and shock-absorbing of the landing gear are performed using the landing gear deploying device for the aircraft. A control circuit 5 can exert control for mitigating a roll in wing low landing under the situation of a cross wind.SELECTED DRAWING: Figure 1

    【課題】より簡易な構成で航空機の脚の展開と緩衝とを行える航空機用の脚展開装置を提供する。【解決手段】航空機用の脚展開装置1は、伸縮機構3とモータ4とを有する。伸縮機構は、航空機の脚2Aと連結され、前記脚の展開及び収納並びに前記脚の緩衝を行う。モータは、前記伸縮機構を伸縮させる。航空機の脚展開方法は、前記航空機用の脚展開装置を用いて前記脚の展開及び収納並びに前記脚の緩衝を行う。制御回路5は、横風がある状況下のウイングロー着地においてロールを緩和するための制御を行うことができる。【選択図】図1


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    Titel :

    LANDING GEAR DEPLOYING DEVICE FOR AIRCRAFT, METHOD OF DEPLOYING LANDING GEAR OF AIRCRAFT, AND AIRCRAFT


    Weitere Titelangaben:

    航空機用の脚展開装置、航空機の脚展開方法及び航空機


    Beteiligte:
    HITOMI ATSUSHI (Autor:in)

    Erscheinungsdatum :

    09.08.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge





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