AIRCRAFT MANUAL CONTROL SYSTEM

摘要

aeronautical engineering. SUBSTANCE: control system includes two control stations with control sticks and cut-out mechanism connected with each stick by means of articulation rods. Cut-out mechanism has body which is rotatably secured on fixed axle and is articulated with rod running to control stick which is not switched-off; it also has rod moving inside body perpendicularly relative to above-mentioned axle; it is connected with rod running to control stick which is switched-off by means of articulation; it is also connected with link which is articulated with on/off lever. EFFECT: possibility of pilotage with one of control sticks disconnected. 2 cl, 2 dwg