Device for detecting leaks in an aircraft engine lubricating oil circuit
Leaks in an oil lubrication circuit, in particular through a heat exchanger communicating with another circuit, are measured by the movements of a piston that is sensitive to variations in flow rates and pressure drops at two calibrated ports on either side of the predicted location of the leak. In one intended application, the second circuit contains overpressurised fuel which is used to constantly cool the oil.
1. A device for detecting leaks in a lubricating oil circuit of an aircraft engine between at least two points of the circuit, the device comprising a piston formed by a plurality of plates stepped over a movable rod which connects said plates, a plurality of fixed chambers in which the plates slide respectively by splitting each of them into two separate compartments, two calibrated ports located respectively at two distinct positions of the circuit, the two compartments of each of the chambers being respectively connected to the circuit by two respective and distinct connecting conduits leading to the circuit on either side of a calibrated port, the device further comprising a sensor ( 29 ) for detecting the position or movement of the piston.
2. The leak detection device according to claim 1 , wherein the circuit comprises a heat exchanger, and the calibrated ports are placed on either side of the exchanger along the circuit.
3. An arrangement comprising the oil circuit and the leak detection device according to claim 2 , wherein the heat exchanger is also placed on a second circuit, through which a fluid flows in heat exchange with the oil.
4. The arrangement according to claim 3 , wherein the second circuit is a fuel supply circuit of the aircraft engine.
5. The leak detection device according to claim 1 , wherein the position or movement sensor is connected to an anomaly diagnosis device, sensitive to a displacement of the rod out of an equilibrium position.
6. The leak detection device according to claim 1 , wherein the plates, the chambers and the calibrated ports are each at least three in number.
7. The leak detection device according to claim 1 , wherein the piston is connected to a fixed location of the device by a return spring ( 32 ) at an initial position of the piston.