FIELD: aircraft engineering.
SUBSTANCE: claimed brake comprises extending controlled water intake, air duct with intake and discharge pipes and intake pipe control drive. Said water intake is composed of the bent intake pipe telescopically articulated with the water duct and control drive. Discharge pipe is also provided with the control drive and coupled with the water duct by cylindrical moving joint. Discharge pipe is brought outboard the aircraft to eject water in direction approximating to the aircraft mirror plane at 0-180 degrees from the flight direction.
EFFECT: controlled deceleration at gliding modes and decreased alighting run, higher safety.
3 dwg
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