PROBLEM TO BE SOLVED: To provide a disengagement device which can reduce a movement amount and backlash upon separation, and transmit a high torque with a compact size, compared with the conventional art.SOLUTION: A disengagement device 1 for disengaging linkage of an automatic steering system comprises: a rotor 2 and a stator 3 which are arranged in parallel along an axial direction, have gears 21 and 31 on respective rear surfaces thereof, and disengage and establish linkage by being separated from and coupled to each other; an armature 4 which is arranged behind the rotor 2 and the stator 3, has a gear 41 engageable simultaneously with the respective gears 21 and 31, on the front surfaces thereof, makes the rotor 2 and the stator 3 coupled to each other by engagement to the gear 41, and is provided movably backward; a spring 8 which energizes the armature 4 backward; and a latch 5 configured so as to press the armature 4 forward with a pressing force equal to or more than an energizing force of the spring 8, and be able to disengage the pressing force in association with operation of a pilot.SELECTED DRAWING: Figure 4

    【課題】従来に比べ、分離時の移動量とバックラッシュを低減させるとともに、コンパクトなサイズで高トルクを伝達させる。【解決手段】ディスエンゲージ装置1は、自動操縦系統のリンケージを解除するものであり、軸方向に沿って並設されるとともに各後面にギア21,31を有し、互いの分離・結合によりリンケージを解除・成立させるローター2及びステーター3と、ローター2及びステーター3の後方に配置されて、その各ギア21,31と同時に噛合可能なギア41を前面に有し、当該ギア41の噛合によりローター2及びステーター3を互いに結合させるとともに、後方に移動可能に設けられたアーマチュア4と、アーマチュア4を後方に付勢するスプリング8と、スプリング8の付勢力以上の押圧力でアーマチュア4を前方に押圧するとともに、パイロットの操作に連動して当該押圧を解除可能に構成されたラッチ5とを備える。【選択図】図4


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    Title :

    DISENGAGEMENT DEVICE


    Additional title:

    ディスエンゲージ装置


    Contributors:

    Publication date :

    2017-03-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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