Device for draining liquids for an aircraft engine
Device for draining liquids for an aircraft engine, comprising a collector designed to collect liquids drained from the engine, said device comprising means for pumping the liquids held in the collector and for discharging said liquids, and monitoring means designed to indicate when the liquids have been collected by the collector in an anomalous manner, said monitoring means being designed to be activated when the flow rate of collected liquids is greater than the delivery of the pumping means.
1. A device for draining liquids of an aircraft engine, comprising:
a collector designed to collect liquids drained from the engine;
means for pumping liquids collected in the collector from the collector for discharging said liquids; and
monitoring means designed to indicate when the liquids have been collected by the collector in an anomalous manner, said monitoring means being designed to be activated when the flow rate of collected liquids is greater than the delivery of the pumping means;
wherein the collector comprises an overflow designed to allow liquids to escape from the collector when the flow of collected liquids is greater than the delivery of the pumping means.
2. The device according to claim 1 , wherein the pumping means comprises a jet pump ejector, said jet pump ejector comprising a first line for the flow of drained liquids, one end of which forms an inlet for the liquids held in the collector and the other end of which forms an outlet for discharging the liquids, and a second line for atomizing pressurized gas, which line extends around or inside the first line and is designed so that the atomized gas leaving said second line forces the liquids to be discharged through the outlet of the first line.
3. The device according to claim 2 , wherein the first line is connected to a valve.
4. The device according to claim 2 , wherein the second line comprises a gas inlet that is connected to a source of pressurized gas.
5. The device according to claim 1 , wherein the pumping means are incorporated in the collector or are located at a distance from the collector and connected to a liquid outlet thereof by a conduit.
6. The device according to claim 1 , wherein the monitoring means comprise a visual and/or electrical alarm designed to be visible to an operator inspecting the collector or to emit a signal intended for the cockpit of the aircraft.
7. An aircraft engine, comprising:
an exhaust nozzle for combustion gases; and
at least one device according to claim 1 , wherein an outlet of the pumping means leading into the exhaust nozzle directly or by a conduit.
8. The aircraft engine according to claim 7 , wherein the pumping means are connected to a compressor or a system for removing gas from the engine.
9. A method for inspecting an engine according to claim 7 , said method comprising:
maintaining the engine after the means for monitoring the device have been activated.
10. The device according to claim 1 , wherein the pumping means includes an electric pump, a mechanical pump, a pneumatic pump, or a jet pump ejector.
11. A device for draining liquids for an aircraft engine, comprising:
a collector configured to collect liquids drained from the engine via one or more drain lines, wherein the liquids comprise hydrocarbons;
one of an ejector or a pump, in fluid communication with the collector and configured to discharge the liquids collected by the collector; and
an overflow alert configured to indicate a collector overflow condition, wherein the collector overflow condition occurs when the flow rate of collected liquids in the collector is greater than the outflow of liquids from the collector; and
an overflow pipe associated with the overflow alert, the overflow pipe configured and arranged to permit the collected liquids to exit the collector when the collection overflow condition occurs.
12. The device of claim 11 , wherein the overflow alert includes a visual or audible alarm.
13. The device of claim 11 , wherein the overflow alert is visual and includes a window mounted to the collector for allowing visual confirmation of a fluid level of the liquids collected in the collector.
14. The device of claim 11 , wherein the overflow alert is configured to generate a signal based on the collector overflow condition, and wherein the collector overflow condition occurs when liquids collected by the collector are abnormal.
15. The device of claim 14 , wherein the overflow alert includes a sensor configured to detect a fluid level of the liquids collected in the collector.
16. The device of claim 11 , wherein said one of an ejector or a pump is an ejector comprising a first line for outflow of liquids from the collector, one end of the first line forming an inlet for the liquids held in the collector and the other end of first line forming an outlet for discharging the liquids toward a jet nozzle, and a second line for atomizing pressurized gas, the second line communicating with the first line and configured so that the atomized gas leaving the second line forces the liquids to be discharged through the outlet of the first line.
17. The device of claim 16 , wherein the second line is connected to a valve.
18. The device of claim 17 , wherein the second line comprises a gas inlet that is selectively connected to a source of pressurized gas by the valve.
19. The device of claim 11 , wherein said one of an ejector or a pump is an ejector comprising a first line for outflow of liquids from the collector, one end of the first line forming an inlet for the liquids held in the collector and the other end of first line forming an outlet for discharging the liquids toward a jet nozzle, and wherein said ejector further comprises a second line in communication with a source of pressurized gas, the second line having an outlet positioned to discharge pressurized gas adjacent the outlet of the first line.