System for the spraying of spray liquid for aircraft windshield, and cockpit provided with such a spraying system
View Patent ↗A system for spraying liquid for a windshield of an aircraft includes a spray-liquid supply circuit, a pressurized-gas supply circuit designed to purge the spray-liquid supply circuit, and at least one nozzle disposed downstream from the circuits and designed to spray the spray liquid and pressurized gas on an aircraft windshield, wherein the system includes a control device able to simultaneously actuate the temporary spraying of spray liquid and of pressurized gas respectively in the spray-liquid spraying circuit and in the pressurized-gas spray circuit in such a way that a pressurized-gas spraying time is strictly greater than a spraying-liquid spraying time. For example, the control device includes a time-lag relay controlling the pressurized-gas supply circuit.
1. A system for spraying liquid for a windshield of an aircraft comprising a spray-liquid supply circuit, a pressurized-gas supply circuit designed to purge the spray-liquid supply circuit, the spray-liquid circuit and the pressurized-gas supply circuit being combined to form a combined liquid-gas supply circuit at an end of the spray-liquid circuit to be purged, and at least one nozzle being coupled to the combined liquid-gas supply circuit and disposed downstream from said circuits and designed to spray the spray liquid and pressurized gas on an aircraft windshield, wherein the system comprises a control device able to simultaneously actuate the temporary spraying of spray liquid and of pressurized gas respectively in the spray-liquid spraying circuit and in the pressurized-gas spray circuit in such a way that a pressurized-gas spraying time is strictly greater than a spraying-liquid spraying time, and wherein the pressure of the pressurized gas flowing in the pressurized-gas supply circuit is strictly lower than the pressure of the spray liquid flowing in the spray-liquid supply circuit, when they reach the nozzles.
2. A system for spraying spray liquid according to claim 1 , wherein the control device has a time-lag relay controlling the pressurized-gas supply circuit.
3. A system for spraying spray liquid according to claim 1 , wherein the pressurized-gas supply circuit has compression means to compress the air intended for circulation in said circuit.
4. A system for spraying spray liquid according to claim 3 , wherein the compression means comprise a compressor positioned downstream from the air tap of said pressurized-gas supply circuit.
5. A system for spraying spray liquid according to claim 1 , wherein the pressurized-gas supply circuit comprises an air tap capable of tapping pressurized gas from an engine of an aircraft.
6. A system for spraying spray liquid according to claim 1 , wherein the pressurized-gas supply circuit has a filter positioned at the level of the air tap of said pressurized-gas supply circuit.
7. A system for spraying spray liquid according to claim 1 , wherein the pressurized-gas supply circuit is provided with at least one backflow check valve capable of preventing the passage of spray liquid in the portion of the pressurized-gas supply circuit positioned upstream from said backflow check valve.
8. A system for spraying spray liquid according to claim 1 , wherein the pressurized-gas supply circuit is provided with a recovery tank capable of receiving the spray liquid flowing in the pressurized-gas supply circuit.
9. An aircraft cockpit comprising at least one system for spraying spray liquid according to claim 1 .
10. An aircraft cockpit according to claim 9 , wherein compression means to compress the gas designed to flow in the pressurized-gas supply circuit are positioned beneath the floor of said cockpit.
11. An aircraft cockpit according to claim 9 , wherein the air tap of the pressurized-gas supply circuit is situated beneath the floor of said cockpit.
12. An aircraft cockpit according to claim 9 , wherein the air tap of the pressurized-gas supply circuit is situated in the radome.
13. An aircraft cockpit according to claim 9 , wherein the air tap of the pressurized-gas supply circuit is situated on the external skin of the cockpit.
14. The aircraft cockpit according to claim 9 wherein the spray-liquid supply circuit and the pressurized-gas supply circuit are coupled together by at least one check valve to form a combined liquid-gas supply circuit.
15. The system for spraying liquid for a windshield of an aircraft according to claim 1 wherein the spray-liquid supply circuit and the pressurized-gas supply circuit are coupled together by at least one check valve to form a combined liquid-gas supply circuit.
16. The system for spraying liquid for a windshield of an aircraft according to claim 1 further comprising at least one check valve between the spray-liquid supply circuit and the pressurized-gas supply circuit prior to the single liquid-gas supply circuit.
17. A system for spraying liquid for a windshield of an aircraft comprising a spray-liquid supply circuit, a pressurized-gas supply circuit designed to purge the spray-liquid supply circuit, and at least one nozzle disposed downstream from said circuits and designed to spray the spray liquid and pressurized gas on an aircraft windshield, wherein the system comprises a control device able to simultaneously actuate the temporary spraying of spray liquid and of pressurized gas respectively in the spray-liquid spraying circuit and in the pressurized-gas spray circuit, wherein a pressurized-gas spraying time is strictly greater than a spraying-liquid spraying time, and the pressure of the pressurized gas flowing in the pressurized-gas supply circuit is strictly lower than the pressure of the spray liquid flowing in the spray-liquid supply circuit, when they reach the nozzles.
18. The aircraft cockpit according to claim 17 wherein spray-liquid supply circuit and the pressurized-gas supply circuit are combined into a single liquid-gas supply circuit, the at least one nozzle being coupled to the single liquid-gas supply circuit.