发明名称 ADAPTIVE LOAD SIMULATOR FOR CONTROL LEVERS OF AIRCRAFT SIMULATOR
摘要 FIELD: training equipment. ^ SUBSTANCE: proposed load simulator includes control lever, sensor showing displacement of control lever, computer complex, engine control system and loading unit. Lever is made in form of control stick provided with axle and dork. Control lever is additionally provided with hollow axle for fork made integral with this fork. Hollow axle of fork and axle of control stick are provided with wire guides made in two perpendicular planes. Segments of loading are connected with electric motor of loading unit. ^ EFFECT: increased speed of response; simplified construction. ^ 4 dwg
申请公布号 RU2231127(C1) 申请公布日期 2004.06.20
申请号 RU20020126811 申请日期 2002.10.09
申请人 发明人 ELISEEV ALEKSANDR VIKTOROVICH
分类号 G09B9/28 主分类号 G09B9/28
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