FIELD: transportation; aviation.
SUBSTANCE: aircraft adaptive stabilizer is installed on a longitudinal tail beam, which makes it possible to simultaneously vary angles of stabilizer deflection in flight in two mutually perpendicular directions: in respect to axis perpendicular to longitudinal axis of the aircraft and in respect to axis parallel to longitudinal axis of the aircraft.
EFFECT: increased longitudinal stability and manageability in maneuvering with increased attack angles.
4 dwg
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