Recovery and rescue system for aircraft

摘要

The recovery and rescue system includes a sail (5) with rigging (10) fitted around a spreader conduit (4), with an intake and outlet nozzle, wherein a starting system (6) is provided, including mechanical (12-13) and electromechanical (17-18) opening mechanisms, in the first case operated by a manual lever (16) and in the second case operated by a button (19). Air driven through the intake of the spreading conduit (4) activates the starting system (6) in order to spread the sail (5) and by parachute means retain or brake the aircraft wherein the said system assembly is fitted. Said system can be housed inside the aircraft in a container provided for the purpose.