To downsize a simulation control device.SOLUTION: A simulation control device 100, which is provided with a housing 1, comprises, inside the housing 1: a control stick 10 that has a first control member 12 rotatable around a first rotation shaft 14, and a second control member 13 located below the first rotation axis 14, and rotatable around a second rotation shaft 15 vertical to the first rotation shaft 14; a first reaction force generation unit 20 that has a spring 22 displaced by rotation of the first control member 12, to generate control reaction force of the first control member 12; a second reaction force generation unit 50 that has a spring 52 displaced by rotation of the second control member 13, to generate control reaction force of the second control member 13; a motor 31 that displaces the spring 22 so that the control reaction force of the first control member 12 becomes zero and changes a neutral position of the first control member 12; and a motor 61 that displaces the spring 52 so that the control reaction force of the second control member 13 becomes zero, and changes a neutral position of the second control unit 13. An output shaft 32 of the motor 31 is located below the first reaction force generation unit 20, and an output shaft 62 of the motor 61 is located above the second reaction force generation unit 50.SELECTED DRAWING: Figure 4

    【課題】模擬操縦装置のコンパクト化を図ること。【解決手段】模擬操縦装置100は、筐体1を備える一方、第1回転軸14周りに回転自在な第1操縦部材12、第1回転軸14の下方に位置し且つ第1回転軸14に垂直な第2回転軸15周りに回転自在な第2操縦装置13を有する操縦桿10と、第1操縦部材12の回転によって変位し第1操縦部材12の操縦反力を生成するバネ22を有する第1反力生成部20と、第2操縦部材13の回転によって変位し第2操縦部材13の操縦反力を生成するバネ52を有する第2反力生成部50と、第1操縦部材12の操縦反力がゼロになるようにバネ22を変位させて第1操縦部材12の中立位置を変更するモータ31と、第2操縦部材13の操縦反力がゼロになるようにバネ52を変位させて第2操縦部材13の中立位置を変更するモータ61とを筐体1内に備え、モータ31の出力軸32は、第1反力生成部20よりも下方に位置し、モータ61の出力軸62は、第2反力生成部50よりも上方に位置する。【選択図】図4


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    Titel :

    AIRCRAFT SIMULATION CONTROL DEVICE


    Weitere Titelangaben:

    航空機の模擬操縦装置


    Beteiligte:
    KOMATSU SEIJI (Autor:in) / MURATA YOSHIO (Autor:in) / KOBAYASHI TAKUMI (Autor:in) / KURACHI OSAMU (Autor:in) / NISHIMURA HIROSHI (Autor:in) / SHIMIZU YUICHI (Autor:in) / KAWABE YUJI (Autor:in) / KONDO HIROKI (Autor:in) / SHINKAI SOMA (Autor:in)

    Erscheinungsdatum :

    2022-02-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    G09B Unterrichts- oder Vorführungsgeräte , EDUCATIONAL OR DEMONSTRATION APPLIANCES / B64C AEROPLANES , Flugzeuge / G05G CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY , Steuer- oder Regelvorrichtungen oder Steuer- oder Regelsysteme gekennzeichnet ausschließlich durch mechanische Einzelheiten



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