FIELD: transport.
SUBSTANCE: invention relates to aircrafts of light-motor aviation. The motor-glider includes fuselage, engine, lifting wing and auxiliary wing, drive arms in wing rudder, wheel, elevator control. The lifting wing is fitted with articulated units two of which are located symmetrically relative transversal axis of symmetry on longeron. One articulated unit is located on auxiliary longeron and fixed on column which is hinged on sliding member movably installed in frame guides. The unit is linked with control wheel column by spring-loaded tie-rod. Auxiliary wing consists of two independent consoles movably fitted on transversal axis immovably fixed in frame nose part. The consoles are equipped with arms linked by tie-rods with double-armed lever of steering wheel. Front wheel pillar movably fixed in frame bushing is equipped with wheel spat made in the form of turning keel and provided with double-armed lever provided with compensators.
EFFECT: higher flight safety.
2 cl, 9 dwg
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