FIELD: aircraft engineering.
SUBSTANCE: invention relates to bringing aircraft carried to drop point by aircraft carrier to flight configuration. Method of unfolding wings 1, 2 of aircraft to be dropped from aircraft carrier consists in determination of position of aerodynamic control elements 3, 4 (ACE) arranged on outer wings creating the aerodynamic force displacing said outer wings 1, 2 to flight position, placing said ACE 3, 4 to aforesaid position at folding the outer wings to transport position, synchronous shift of outer wings to flight position by incident airflow and retention of outer wings in flight position. Incident airflow brings its effects on ACE at dropping of aircraft at drop point at preset aircraft carrier flight parameters or at shifting before aircraft drop to position whereat is located in incident airflow at connection with carrier.
EFFECT: higher reliability of unfolding, simplified design and decreased weight.
5 cl, 16 dwg
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