Oil tank for a turbomachine with level measurement

Abstract

An oil tank fitted to a turbomachine, for example an aeroplane turbo-jet engine. The tank includes an inner chamber containing the oil of the turbomachine, a wall with an inner surface surrounding the inner chamber, and a capacitive device for measuring the oil level. The device includes at least one electrode and potentially two parallel electrodes forming the inner surface. These electrodes are immersed in the oil to measure the oil level by measuring capacitance. A method for manufacturing a tank in which the electrodes are printed on the wall.

Claims

1. A tank for a turbomachine, the tank designed to contain a liquid of the turbomachine, said tank comprising: an inner chamber structured to contain the liquid in the tank, a wall with an inner surface surrounding the inner chamber, and a capacitive device structured and operable to measure a level of the liquid within the inner chamber, wherein the capacitive device includes at least one electrode, the at least one electrode applied against the wall in order to form the inner surface, and designed to be in electrical contact with the liquid in order to measure the level of the liquid, the tank further comprising an electrically insulating layer insulating the wall from the at least one electrode.

2. The tank according to claim 1, wherein the at least one electrode comprises two electrodes and the two electrodes extend in parallel over at least most of the height of the inner chamber.

3. The tank according to claim 2, wherein the inner surface has a portion delimited by the two electrodes, the portion extending mostly vertically.

4. The tank according to claim 1 further comprising an angular sector containing the at least one electrode of the capacitive device, an angle of the angular sector being equal to or less than 90.

5. The tank according to claim 1, wherein the inner chamber includes a bottom and a top, the at least one electrode being separated vertically from the bottom and from the top.

6. The tank according to claim 1, wherein the wall includes a weld about the inner chamber.

7. The tank according to claim 1, wherein the tank includes a lower portion and an upper portion that is separated from the at least one electrode by a weld.

8. The tank according to claim 1, wherein the wall includes a metal sheet forming a substantially cylindrical compartment designed to contain the at least one electrode.

9. The tank according to claim 1, wherein the thickness of the at least one electrode is equal to or less than 1.00 mm.

10. A turbomachine, said turbomachine comprising: a lubrication circuit with an oil tank, wherein the oil tank comprises: an inner chamber structured to contain the liquid in the oil tank, a wall, an inner surface that surrounds the inner chamber and is partially formed by the wall, and a capacitive device structured and operable to measure a level of the liquid, the capacitive device including at least one electrode that partially forms the inner surface of the wall and is structured to be in electrical contact with the liquid in order to measure the level of liquid, wherein the capacitive device is designed to adjust to the presence of gas in the oil and the presence of solid particles in the oil.

11. The turbomachine according to claim 10, wherein the capacitive device is designed to measure the capacitance of the fluid using the at least one electrode.

12. An oil tank comprising: a concave wall with an inner surface delimiting an inner chamber for containing oil, a capacitive device structured and operable to measure a level of oil within the inner chamber, wherein the capacitive device includes two electrodes applied against the concave wall in order to form the inner surface, and designed to be in electrical contact with the liquid in order to measure the level of the liquid.

13. The oil tank of claim 12, wherein the two electrodes are distant from one another such as to define an angular sector of 90, measured from a vertical central axis of the tank.

Description

DRAWINGS

(1) FIG. 1 shows an axial turbomachine with a tank according to various embodiments of the invention.

(2) FIG. 2 shows a turbomachine tank according to various embodiments of invention.

(3) FIG. 3 is a cross section of the tank along the line 3-3 shown in FIG. 2 according to various embodiments of the invention.

(4) FIG. 4 is a diagram of a method for manufacturing a tank according to various embodiments of invention.

DETAILED DESCRIPTION

(5) In the description below, the axial direction corresponds to the direction running along the axis of rotation of the turbomachine. The radial direction is perpendicular to the axis of rotation. Upstream and downstream refer to the main direction of flow of the flow in the turbomachine. The height and vertical aspect of the tank relate to the normal assembly direction.

(6) FIG. 1 is a simplified representation of an axial turbomachine. In this example, it is a dual-flow turbo-jet engine. The turbo-jet engine 2 has a first compression level, referred to as the low-pressure compressor 4, a second compression level, referred to as the high-pressure compressor 6, a combustion chamber 8, and one or more turbine levels 10. When in operation, the mechanical power of the turbines 10 transmitted via the shafts to the rotor 12 moves the two compressors 4 and 6. These latter have several rows of rotor blades associated with rows of stator vanes. The rotation of the rotor about the axis of rotation 14 thereof thereby enables an air flow to be generated and progressively compressed until entry into the combustion chamber 8.

(7) An inlet fan 16 is coupled to the rotor 12 and generates an air flow that is divided into a primary flow 18 passing through the different levels mentioned above of the turbomachine, and a secondary flow 20 that passes through an annular duct. Reduction means, such as an epicycloidal step-down gear 22, can be used to reduce the rotational speed of the fan 16 and/or of the low-pressure compressor 4 in relation to the related turbine level 10. The secondary flow 20 can be accelerated to generate a thrust reaction useable in aeroplane flight.

(8) The primary flow 18 and the secondary flow 20 are radially concentric annular flows. Such progressive flows are enabled by several rotors 12 with independent shafts 24. These shafts 24 can be coaxial and fitted into one another. The shafts are moveable in rotation on bearings 26 arranged at the interfaces of same with the housing of the turbomachine 2, or using bearings at the inter-shaft interfaces of same.

(9) The bearings 26 and the optional epicycloidal step-down gear 22 are cooled and/or lubricated by an oil circuit, which can be closed. This circuit can belong to the turbomachine 2. The circuit can also supply actuators such as cylinders (not shown). The oil circuit can also include a heat exchanger (not shown) for cooling the oil. The bearings 26 are arranged in enclosures, which are usually sealed by gaskets arranged about the shafts. The enclosures enable the bearings 26 to be lubricated by oil spray. The oil takes on air when in contact with the bearings 26, such that the recovered oil is a liquid air/oil mix, for example containing at least 1% of air by volume.

(10) The enclosures, which can be dry housings, are provided with aspiration orifices, also known as drainage orifices, in communication with the pumps 28. The pumps 28 can be volumetric pumps, for example to control the flow rate. The oil circuit can thus include several oil recovery lines converging on a tank 30, which can be the main tank. The tank 30 is also the starting point for several feed lines (not shown) for the bearings 26 and other miscellaneous equipment.

(11) The tank 30 can be attached to the nacelle of the turbomachine, or to a compressor housing. Attachment to an intermediate housing is possible. The tank 30 can be placed between two annular walls guiding the concentric flows, for example the secondary flow 20 and the flow surrounding the turbomachine, or between the primary flow 18 and the secondary flow 20. In order to increase the useable volume of same, the tank 30 is essentially elongate, while having a general curved shape. This curvature enables arrangement between two curved, close partitions. The tank can, for example, be close to a source of heat, and the temperature of same can reach 100 C., and moreover can be exposed to the vibrations of the turbomachine.

(12) Furthermore, operation of the turbomachine causes wear to the bearings 26 and the pumps 28. This wear releases metal particles into the lubrication circuit. These particles are also found in the oil in the tank, and can change the electrical properties of the oil.

(13) FIG. 2 is a cross section of an oil tank 30 such as the one in FIG. 1.

(14) The tank 30 is partially filled with oil. The lower portion 32 of same contains a mixture of oil, air and impurities, such as the metal particles generated by wear. The upper portion 34 of same can contain air, or at least an essentially gas phase. The tank 30 is provided with a level measurement device in the inner chamber 36 of the tank 30 in order to monitor the liquid level therein. The inner chamber 36 can be the main chamber of the tank 30. The principal aspect refers to the largest receptacle of the tank.

(15) The device is capacitive. The device includes at least one electrode 38 or two electrodes 38 placed in the inner chamber 36 and in electrical contact with the oil. The electrodes are immersed in the oil. The volume or mass of oil in the tank 30 can be determined by measuring the capacitance of the oil. The oil then becomes an electrical capacitor.

(16) The measurement device can also use data supplied by a module for detecting metal particles in the oil. The device can estimate and correct the oil level measured as a function of the influence of the metal particles in the oil. The extent of the gas phase in the oil can also be taken into account.

(17) The electrodes 38 form part of the inner surface 40 of the tank 30, this inner surface also being formed by the wall 42 of the tank 30. This wall 42 forms the structure of the tank 30, delimiting the storage volume and the outer surface 44 thereof. This wall can include brackets for attachment to the structure of the turbomachine.

(18) The electrodes 38 can form two parallel ribbons. The electrodes can be of the same length, the same width and the same thickness. The length can be the same as the height of the electrodes. The height of the electrodes can be at least 10% of the height of the tank 30, or the majority of the height of the tank. The electrodes can cover the majority of the height of the useable volume of the tank and/or the entire height of the zone through which the liquid level varies. This is intended to improve measurement precision.

(19) The wall 42 can include a lower portion 46, a central portion 48 and an upper portion 50. These portions can be welded to one another, for example using weld seams 52 forming loops. Each of these portions can be integrally formed. Alternatively, the central portion can be made from a metal sheet. The central portion is optional, since the lower and upper portions can be connected directly to one another.

(20) The tank 30 can include other equipment. For example, the tank can have inlet and outlet orifices (not shown). A stopper (not shown) can be placed in the upper portion, for example at the top of same. A deserter, a vent and/or an oil separator (not shown) can be associated with the tank 30. Valves can also be associated with the inlet and/or the outlet.

(21) FIG. 3 is a cross section of the tank 30 taken along the line 3-3 shown in FIG. 2. The electrodes 38 are shown here in cross section. The electrodes occupy a concave face of the wall 42.

(22) If the wall 42 is made of an electrically conductive material, one or more insulating layers 54 can be provided. Each insulating layer 54 electrically insulates the wall 42 from the electrodes. The layers break the contact at the wall/electrode interface. The wall 42 is thicker than the electrode 38. The thickness of these latter can be equal to or less than 0.10 mm.

(23) The two electrodes 38 can be essentially close to one another. The electrodes can be positioned in an angular sector forming a fraction of one turn of the tank 30. The angular sector can be measured in relation to a vertical axis 56 at the centre of the tank 30. The angular sector containing the electrodes 38 can have an angle equal to or less than 90.

(24) According to one variant of the invention, a single electrode is placed in the tank, the device using the metal wall of the tank as the other electrode.

(25) FIG. 4 is a diagram of a manufacturing method for a tank. The tank can be the tank described in relation to FIGS. 1 to 3.

(26) The method can include the following steps, in various instances carried out in the following order:

(27) The first stem (e.g., step (a)) is manufacturing a tank wall forming at least part of an inner chamber designed to contain a liquid, the wall in various instances being made of several portions, as indicated at 100.

(28) A subsequent step (e.g., step (b)) is printing one or more electrodes of a capacitive device for measuring the level of the liquid on the inner face of the wall of the tank, as indicated at 102

(29) A subsequent step (e.g., step (c)) is welding the portions of the wall such as to close the inner chamber, as indicated at 104.

(30) A subsequent step (e.g., step (d)) is machining the tank to make attachment surfaces, connections, which are in various instances separated from the electrodes, as indicated at 106.

(31) A subsequent step (e.g., step (e)) is electrical connection of the electrodes outside the tank, as indicated at 108.

(32) During the manufacturing step (a) 100, the wall can be manufactured at least in part by additive layer manufacturing, for example powder-based. The wall can comprise several portions that are welded together during the welding step (c) 104 to form a sealed assembly. This method enables complex shapes to be produced. The wall can be made of metal, for example steal, and/or using aluminium or titanium alloys.

(33) The printing step (b) 102 uses electrically conductive ink, in various instances with electrically conductive pigments. The ink used makes it possible to provide electrodes containing copper and/or silver and/or nickel and/or platinum and/or graphene oxide and/or graphite oxide and/or organic polymers. These materials provide corrosion resistance that is useful in the context of turbo-jet engine oil, in particular due to the presence of corrosive additives.

(34) According to various embodiments of the invention, the manufacturing step (a) 100 and the printing step (b) 102 are performed simultaneously. For example, the wall can be made by printing in three dimensions, as can the electrodes. The layers of material forming the electrodes can be made at the same rate as the layers progressively building the walls.

(35) The present teachings have been provided in relation to an oil tank. However, these teachings can also be applied to a fuel tank or to any other tank of the turbomachine containing another liquid required by the turbomachine.