| 摘要 |
FIELD: aircraft pilotage equipment with processor control sets; actuating aircraft controls for change or maintenance of its in-flight position. ^ SUBSTANCE: proposed system includes complex control system, control stations of first and second cabins which are mechanically interconnected, trim effect mechanisms in pitch, roll and course channels, control panels of complex control system, flap flexible trim control tubes, planetary reduction gears-articulations for extension and retraction of flaps and deceleration flap control system. Complex control system consists of four-fold redundant digital computer part, four-fold redundant in electrical part and two-fold redundant in hydraulic part of electro-hydraulic actuators of four-fold redundant in electrical part and two-fold redundant in hydraulic part electro-hydraulic actuator of stabilizer, rotating electro-hydraulic drive of flaps, three-position hydraulic cylinders of wing leading edges, electro-hydraulic control cocks of wing leading edges and deceleration flap drive. Each channel of computer part of complex control system is made for determination of control signal by "channel-model" structure. ^ EFFECT: extended functional capabilities. ^ 8 cl, 4 dwg |
