FIELD: servo drives; control systems of manned flying vehicles. SUBSTANCE: drive includes hydraulic distributor 8 made in form of two cylindrical spool valves, one inside other; outer spool valve is rigidly connected with rod 21 of servo unit and inner spool valve is connected with bell crank which consists of two articulated levers 9 and 10 for emergency automatic control in case of seizure of mechanical control linkage of flying vehicle; provision is made for relative motion of said levers by means of mechanical retainer 11 made in form of two spring-loaded plungers located inside lever 10 connected with inner spool valve of hydraulic distributor 8. EFFECT: simplified construction; reduced overall dimensions of drive. 2 cl, 2 dwg
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Authors
Dates
2002-10-20—Published
2000-08-18—Filed