Recovery and rescue system for aircraft
View Patent ↗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.
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.
2. The recovery and rescue system for an aircraft, according to claim 1 , characterized in that the sail finishes off in an opposite direction to that of said initiation subsystem, in an annular lag catch, whereto the rigging is fastened, which is in turn fastened to a midpoint of the structure of the aircraft, in correspondence with a centre of gravity thereof.
3. The recovery and rescue system for an aircraft, according to claim 1 , characterized in that the rigging is rolled up on the initial area of the spreading conduit.
4. The recovery and rescue system for an aircraft, according to claim 1 , characterized in that the opening mechanisms are mechanical and are connected to a manual lever by means of cables.
5. The recovery and rescue system for an aircraft, according to claim 1 , characterized in that the spreading conduit, with the sail, the initiation subsystem and the opening mechanisms, are mounted on a housing or container established on the aircraft itself; said rescue system comprises an air compressor system materialized in a tank wherein air is applied to the spreading conduit to extend the sail in correspondence with the frontal area of the inlet of the spreading conduit.