AIRCRAFT WITH GENERAL-PURPOSE EQUIPMENT CONTROL SYSTEM

FIELD: aeronautical engineering; control of training and practicing flights. ^ SUBSTANCE: proposed aircraft has fuselage, wing, tail unit, landing gear, engines of main power plant and air intakes with passages bounded by wing. Door turnably secured on wing is flush with upper surface. Auxiliary power plant is arranged in tail fuselage across longitudinal axis. Provision is made control system of general-purpose aircraft equipment. Two automatic control loops are provided in main and reserve conversion and calculation units which are connected to actuators through monitoring and control unit. Manual control loop is provided with control panels, enunciator panel and central signal light. Control system is engageable via multiplex channel with onboard digital computer, electronic control systems of port and starboard engines, recording and monitoring system, guidance and landing equipment and complex control system. Performed by code communication lines is tie-in with fuel control and monitoring system, voice message equipment, complex electron display system and auxiliary power plant. Provision is made for control of general-purposed aircraft equipment both in automatic and manual modes. ^ EFFECT: enhanced mobility of aircraft. ^ 2 cl, 1 dwg