ADAPTIVE LOAD SIMULATOR FOR CONTROL LEVERS OF AIRCRAFT SIMULATOR Russian patent published in 2004 - IPC

Abstract RU 2231127 C1

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

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RU 2 231 127 C1

Authors

Eliseev Aleksandr Viktorovich

Dates

2004-06-20Published

2002-10-09Filed