Nacelle air intake provided with a mixed ice protection system
An optimized protection against ice on the inner and outer faces of an aircraft engine nacelle air intake with the air intake including an outer face and an inner face meeting at a line at the longitudinally extreme, called extremum line, an acoustic panel being installed on the inner surface of a part of the inner face. An elimination system based on vibration of the ice formed is put in place on at least a part of the outer face and an ice formation prevention system using a hot fluid is put in place on at least a part of the inner face and either an ice elimination system or an ice formation prevention system using a hot fluid is installed on the inner face and on the outer face, a marking line marking the boundary between the two systems.
1. An air intake comprising
an outer face and an inner face meeting at a line at a longitudinally extreme, called extremum line,
an acoustic panel being installed on an inner surface of a part of the inner face,
wherein, an elimination system based on vibration of ice formed is put in place on at least a part of the outer face and an ice formation prevention system using a hot fluid is put in place on at least a part of the inner face, and
wherein, either the ice elimination system or the ice formation prevention system using a hot fluid is installed on the inner face and on the outer face, a marking line marking a boundary between the ice elimination system and the ice formation prevention system.
2. The air intake according to claim 1 , wherein the marking line corresponds to an upstream end of the acoustic panel incorporating the ice formation prevention system.
3. The air intake according to claim 2 , wherein the formed ice elimination system comprises piezoelectric devices distributed over at least a part of an inner surface of the outer face.
4. The air intake according to claim 3 , wherein thermoelectric generators are placed on a hot surface of the air intake and connected to the piezoelectric devices to supply the piezoelectric devices from a temperature difference between the interior of the air intake and the hot surface inside the air intake.
5. The air intake according to claim 1 , wherein the ice formation prevention system comprises longitudinal ducts distributed over at least a part of the inner surface of the inner face, an upstream end of the longitudinal ducts receives hot air discharged into an internal space of the air intake through a downstream end of said ducts.
6. The air intake according to claim 5 , wherein the longitudinal ducts are distributed over an entire transverse annular periphery of the inner face.
7. The air intake according to claim 5 , wherein the upstream end of the ducts emerges in a transverse chute leading the hot air to the longitudinal ducts.
8. An air intake comprising;
an outer face and an inner face meeting at a line at a longitudinally extreme, called extremum line,
an acoustic panel being installed on an inner surface of a part of the inner face,
wherein, an elimination system based on vibration of ice formed is put in place on at least a part of the outer face and an ice formation prevention system using a hot fluid is put in place on at least a part of the inner face, and
wherein, either the ice elimination system or the ice formation prevention system using a hot fluid is installed on the inner face and on the outer face, a marking line marking a boundary between the ice elimination system and the ice formation prevention system,
wherein the marking line corresponds to an upstream end of the acoustic panel incorporating the ice formation prevention system,
wherein the formed ice elimination system comprises piezoelectric devices distributed over at least a part of an inner surface of the outer face,
wherein thermoelectric generators are placed on a hot surface of the air intake and connected to the piezoelectric devices to supply the piezoelectric devices from a temperature difference between the interior of the air intake and the hot surface inside the air intake,
wherein the ice formation prevention system comprises longitudinal ducts distributed over at least a part of the inner surface of the inner face, an upstream end of the longitudinal ducts receives hot air discharged into an internal space of the air intake through a downstream end of said ducts,
wherein the upstream end of the ducts emerges in a transverse chute leading the hot air to the longitudinal ducts, and
wherein a surface of the chute constitutes the hot surface and the generators are fixed onto an outer surface of the chute.
9. The air intake according to claim 7 , wherein an acoustic panel is superposed on the longitudinal ducts and extends longitudinally from the chute over at least a part of the inner face.
10. The air intake according to claim 5 , wherein the longitudinal ducts form part of one or more reheating panels over an entire annular transverse periphery of the air intake.
11. The air intake according to claim 10 , wherein the downstream transverse end of the reheating panel forms a step towards the interior of the air intake to house an acoustic panel in a cavity formed by the step and allow the ducts to be able to discharge the hot air in an internal space of the air intake without having to cross said acoustic panel.
12. The air intake according to claim 1 , wherein an ice formation prevention system that does not use a hot fluid is combined with at least one of the ice elimination system or with the ice formation prevention system using a hot fluid.
13. A nacelle provided with an air intake according to claim 1 .
14. A propulsive assembly of an aircraft provided with a nacelle according to claim 13 .