Patent ID: 8123170
Filing Date: 2012-02-28
Classification: B64D

Abstract:
1. A recovery and rescue system for aircrafts comprising a spreader conduit with an inlet nozzle and an outlet nozzle, finishing off in correspondence with said outlet nozzle in an initiation subsystem, inflatable by the effect of air which penetrates the conduit through the inlet nozzle, and whose system is connected to a sail suitably folded around the conduit, characterized in that the spreading conduit wherein the inlet nozzle and the outlet nozzle are established is mounted inside a casing which is fused to the upper part of the fuselage of the aircraft, said casing which is elongated and adopts an ellipsoidal configuration, adapting to the nose cone of the aircraft with the collaboration of a support frame provided with a shroud, having been provided that the inlet nozzle is equipped with two covers, while the outlet nozzle is equipped with a single cover, covers which have corresponding opening mechanisms and which are actuated from the control cabin of the aircraft, and wherein the opening mechanisms are electromechanical, which are actuated by a button with the energy supplied by a battery; and wherein the sail is mounted on the spreading conduit and finishes off in a rigging duly fastened to the fixed structure of the system, which acts as a spacer between the sail and the aircraft, when the extension of said sail is produced.