LEAK DETECTION METHOD AND SYSTEM

Abstract

The present invention relates to a leak detection system for checking the leak-tightness of an object, the system including: a device for pressurising a space; a first pressure sensor configured to measure the variations in pressure of the pressurised space; a second pressure sensor configured to measure the variations in ambient pressure, such as atmospheric pressure; an electronic entity configured to determine a leak depending on the variations in the pressure ΔP in the pressurised space and the variations in the ambient pressure ϕP.sub.ext, the variations ΔP, ΔP.sub.ext being measured over a predetermined test time interval t.sub.test by the first and second sensors, respectively.

Claims

1. A leak detection system (1) for checking the tightness of an object, said system (1) comprising: a device (5) for pressurising a space; a first pressure sensor (7) configured to measure pressure variations of the pressurised space; a second pressure sensor (9) configured to measure pressure variations of the environment, such as atmospheric pressure; an electronic entity (15) configured to determine a leak F′, F″ depending on the pressure variations ΔP in the pressurised space and the pressure variations ΔP.sub.ext of the environment, said variations ΔP, ΔP.sub.ext being measured over a predetermined test time interval t.sub.test, respectively by the first (7) and second (9) sensors.

2. The system according to the preceding claim, characterised in that said pressure variations ΔP in said space are corrected depending on said pressure variations ΔP.sub.ext of the environment.

3. The system according to claim 1 or 2, characterised in that the first pressure sensor (7) and/or the second pressure sensor (9) are differential pressure sensors.

4. The system according to any of the preceding claims, the electronic entity (15) and said first (7) and second (9) sensors making it possible to generate, over the test time interval t.sub.test: a curve of the pressure variations ΔP in said space; a curve of the pressure variations ΔP.sub.ext of the environment.

5. The system according to any of the preceding claims, characterised in that the electronic entity (15) determines the level of leak F′ of the tested object based on a corrected pressure variation ΔP′, said corrected pressure variation ΔP′ being calculated as follows:
F′=C.sub.1ΔP′=C1(ΔP−k.sub.SΔP.sub.ext) where k.sub.S is a normalisation coefficient specific to said first (7) and second (9) sensors, and C.sub.1 is a constant depending on the time and space of the tested object.

6. The system according to the preceding claim, characterised in that the normalisation coefficient k.sub.S is determined: based on the curve of the pressure variations ΔP in said space and the curve of the pressure variations ϕP.sub.ext of the environment, or prior to said measurement of the pressure variation ΔP in said space and the measurement of the pressure variation ϕP.sub.ext of the environment, the value of said normalisation coefficient k.sub.S being stored in a memory of the electronic entity (15).

7. The system according to any of the preceding claims, characterised in that it comprises a third pressure sensor (17) configured to measure the pressure P in the pressurised space.

8. The system according to any of the preceding claims, characterised in that said electronic entity (15) determines, through at least one sensor, a pressure variation Δ.sub.TP related to an average temperature variation of the object per unit of time, said pressure variation Δ.sub.TP being also used to determine the leak F″ of the tested object depending on the pressure variations ΔP in the pressurised space and the pressure variations of the environment ΔP.sub.ext.

9. The system according to the preceding claim, the electronic entity (15) determining the level of leak F″ of the tested object depending on the following formula:
F″=C.sub.1ΔP″=C.sub.1(ΔP−k.sub.SΔP.sub.ext−Δ.sub.TP) where ΔP″ is the corrected pressure variation of the tested object, Δ.sub.TP is the pressure variation depending on the average temperature variation of the tested object during the test time of said object, and C.sub.1 is a constant depending on the time and space of the tested object.

10. The system according to any of the preceding claims, characterised in that it comprises a thermally insulated enclosure configured to accommodate the object to be tested.

11. A leak detection method (100) implemented within a leak detection system (1) according to one of claims 1 to 10, said method comprising the following steps: pressurising (S1) a space by a pressurising device (5); measuring the pressure variation (S2) of the pressurised space by a first pressure sensor (7); and measuring the pressure variations of the environment (S3) by a second sensor (9); detecting a leak (S4) depending on the pressure variations of the pressurised space ΔP and the pressure variations of the environment ΔP.sub.ext.

Description

[0042] The invention will be better understood, and further purposes, details, characteristics and advantages thereof will become clearer throughout the following description of particular embodiments of the invention, given by way of illustration only and not limitation, with reference to the appended drawings, in which:

[0043] FIG. 1, referred to as [FIG. 1], is a highly schematic representation of a leak detection system according to the invention;

[0044] FIG. 1a, referred to as [FIG. 1a], which is a schematic and enlarged view of a pressure sensor of the system of FIG. 1;

[0045] FIG. 2, referred to as [FIG. 2], is a schematic perspective view of the system of FIG. 1 for checking the tightness of an object, when the object is an electric battery for an electric automobile vehicle;

[0046] FIG. 3, referred to as [FIG. 3], is a flow chart representing the steps of the leak detection method according to the invention;

[0047] FIG. 4, referred to as [FIG. 4], is a graph of the pressure variation in the space during different steps of the method of FIG. 3;

[0048] FIG. 5, referred to as [FIG. 5], is a graph representing, as curves, an example of pressure variations in a space relating to the tested object and to the environment during a tightness checking of the object;

[0049] FIG. 6, referred to as [FIG. 6], is a curve of the pressure variation in a space relating to the tested object determined from the curves in FIG. 5.

[0050] FIG. 1 is thus a highly schematic representation of a leak detection system for checking the tightness of an object 10, in the example described below the tested object is an electric battery for an automobile vehicle, but can be any object whose tightness has to be checked and whose level of leak that is to be detected is in the order of magnitude of the disturbances related to the environment of said system.

[0051] Said system thus comprises: [0052] a device 5 for pressurising a space relating to the tested object 10, such as the characteristic space of the electric battery 10, that is, this may be an internal space of the battery (direct method) or a closed space surrounding the battery (indirect method); [0053] a first pressure sensor 7 configured to measure the pressure variations of said characteristic space for checking the tightness of the battery 10; [0054] a second pressure sensor 9 configured to measure the pressure variations of the environment, typically atmospheric pressure; [0055] a third pressure sensor 17, which is an optional sensor, configured to measure the pressure applied in said characteristic space by said device 5; [0056] aeraulic connections 11 configured to connect the pressurising device 5 to the object 10 and to a reference 13; [0057] an electronic entity 15, such as an electronic circuit, connected to the various pressure sensors 7, 9, 17 and configured to recover the pressure values measured by one or more of said sensors 7, 9 and 17.

[0058] The first and second pressure sensors 7 and 9 are preferably differential pressure sensors. Whereas the third sensor 17 is advantageously an absolute pressure sensor.

[0059] It will be noted that a differential pressure sensor is for example a sensor including a diaphragm where each face of the diaphragm is exposed to a pressure, the displacement of the diaphragm (measured for example by capacitive effect) enabling the pressure difference of each face of the diaphragm to be measured.

[0060] [FIG. 1a] is a highly schematic view of the second differential pressure sensor 9 configured to measure the pressure variations of the environment, such as atmospheric pressure.

[0061] More particularly, the sensor 9 comprises a diaphragm 201 with each face located in a separate cavity 203, 205. Each of the cavities 203, 205 of the sensor 9 communicates with the outside (in this case the atmosphere), however one of the cavities 205 is configured to filter out rapid pressure variations that may occur in that environment, thus pressure values P.sub.ext and P′.sub.ext prevailing in each of the cavities 203, 206 can be defined, the difference of which provides pressure variations P.sub.ext of the environment.

[0062] Similarly, in the present example, the leak detection is done by means of a reference 13, but the latter can be: [0063] a reference piece (that is, the same object having the required level of tightness), in which case the measurement of a pressure variation is performed between a test piece and a reference piece; [0064] a plug, the measurement of a pressure variation between a test piece and a reference side plug; [0065] another similar object to be tested, thus two pieces are tested at the same time, one at the test side, the other at the reference side.

[0066] More particularly, the device 5 comprises: [0067] a compressed air supply 51; [0068] an aeraulic circuit including a plurality of valves 57 and which is, on the one hand, connected to the supply 51 and, on the other hand, is configured to regulate the supply of compressed air to the various parts of the aeraulic circuit, that is, to at least one of said sensors 7, 17 and/or at least one characteristic space of the object 10 to be tested and of the reference 13 (via the aeraulic connections 11).

[0069] Generally, the device 5 and its elements 51, 57, the electronic entity 15, as well as the various sensors 7, 9 and 17 are arranged inside a casing 20. However, the various elements, such as the sensor 9, can be offset and arranged outside the casing 20.

[0070] Said electronic entity 15 is also connected to said valves 57, in order to control said valves 57 during the various steps necessary for checking the tightness of the object 10.

[0071] As for [FIG. 2], it is a schematic perspective view of the system of [FIG. 1] used for checking the tightness of an electric battery 10.

[0072] Thus, said system 1 furthermore comprises an enclosure 30 comprising a base 30a and a cover 30b. The base 30a is configured to accommodate the battery 10 and the cover 30b to cover said battery 10 in order to limit environmental influences when detecting leaks.

[0073] For this, said enclosure 30 may be made of a material having a thermal conductivity of less than 0.05 W.Math.m.sup.−1.Math.K.sup.−1 at 20° C., preferably less than 0.03 W.Math.m.sup.−1.Math.K.sup.−1 at 20° C., and even more advantageously less than 0.01 W.Math.m.sup.−1.Math.K.sup.−1 at 20° C.

[0074] In an alternative embodiment not represented, said enclosure 30 comprises one or more cavities capable of accommodating the object to be tested 10 and the reference 13.

[0075] In another alternative embodiment not represented, the system 1 comprises a ventilation device configured to stir the gas, preferably inert, or air of the internal space of the enclosure 30.

[0076] Thus, as illustrated in [FIG. 3], when it is desired to check the tightness of an object 10, such as a battery, said system 1 performs the following method 100: [0077] pressurising S1 a characteristic space of the object 10, for example the internal space of the battery, via the pressurising device 5; [0078] measuring the pressure variation S2 of the pressurised space of the object 10 by the first pressure sensor 7; [0079] measuring the pressure variations of the environment S3 by the second sensor 9; [0080] detecting a leak S4 depending on the pressure variations of the pressurised space ΔP and the pressure variations of the environment ϕP.sub.ext (in this case the atmospheric pressure).

[0081] It will be noted that some of the steps of the method 100 are part of an aeraulic leak detection management method that can be divided into four phases, more particularly illustrated in [FIG. 4]: [0082] a phase of filling I the space with compressed air, the pressure increases to a desired pressure value P1; [0083] a stabilisation stage II, after having pressurised the space, waiting for it to return to thermal and mechanical equilibrium, so that phenomena do not disturb the measurement of the leak, it should be noted that the filling and stabilisation phases I and II correspond to the pressurisation step S1; [0084] a test phase III, during which the pressure variations in the pressurised space and the pressure variations of the environment are measured for a predetermined test time t.sub.test (the test phase III thus corresponds to steps S2 and S3 above); [0085] a draining phase IV, during which the pressurised space is returned to atmospheric pressure.

[0086] The various steps and phases described below are controlled by the electronic entity 15 which manages the opening and closing of the various valves 57 accordingly.

[0087] Additionally, said electronic entity 15 is configured to determine a leak F′ and F″ depending on the pressure variations in the pressurised space ΔP and the pressure variations of the environment ϕP.sub.ext, said variations ΔP, ϕP.sub.ext being measured, over a predetermined time interval t.sub.test, by the first and second sensors 7 and 9.

[0088] FIG. 5 illustrates an example of pressure values measured by the first and second sensors 7 and 9, as curves. There is a curve illustrating the variation in the pressurised space ΔP and another curve illustrating the pressure variation of the environment ΔP.sub.ext over the test time t.sub.test. Said curves are generated via the electronic entity and the first and second sensors 7 and 9.

[0089] The electronic entity 15 is thus configured to correct the curve ΔP by the curve ΔP.sub.ext, in order to obtain a corrected pressure variation ΔP′ which is no longer influenced by the environment (pressure and/or temperature variations from the environment).

[0090] More particularly, said corrected pressure variation ΔP′ is calculated as follows:

ΔP′=(ΔP−k.sub.SΔP.sub.ext)

where k.sub.S is a normalisation coefficient specific to the sensors 7 and 9 allowing the values of each of the curves to be subtracted from each other.

[0091] An example of a corrected pressure curve ΔP′ based on the curves in [FIG. 5] is illustrated in [FIG. 6].

[0092] Said normalisation coefficient k.sub.S is for example: [0093] determined based on the measurement curves ΔP, ΔP.sub.ext, for example by making the ratio of extreme values; [0094] determined beforehand and its value is stored in a memory of the electronic entity 15.

[0095] Thus, the electronic unit 15 determines the level of leak F′, also called corrected level of leak, from the corrected pressure variations ΔP′ according to the following formula:

[00002]$F^{\prime }=k\frac{\Delta P^{\prime }}{\Delta t}V=C_1\Delta P^{\prime }$

where C.sub.1 is a constant depending on the time (for example the test time t.sub.test) and the space V of the tested object (that is, the space of the object whose tightness is to be determined).

[0096] Depending on the value of the leak F′, and according to the required threshold, the electronic entity 15 indicates the compliance or not of the tested object.

[0097] In an alternative embodiment, said electronic entity 15 determines an average temperature variation per unit of time of the tested object, via at least one sensor, for example the second or third sensor 9, 17.

[0098] Said average temperature variation is then used to determine a corrected leak F″ depending on the pressure variations ΔP measured in the pressurised space and the pressure variations ΔP.sub.ext of the environment.

[0099] More particularly, in a step prior to the test, the second 9 or third 17 sensor is configured to measure a pressure variation Δ.sub.TP (in Pa/s) depending on the average temperature variation of the object per unit of time.

[0100] This measurement can for example be carried out during a step prior to filling or during the stabilisation phase, but it is necessary that the object to be tested and/or the reference are isolated from the outside.

[0101] The electronic entity 15 then determines a corrected pressure variation in ΔP″ of the characteristic space of the tested object depending on the following formula:

ΔP″=ΔP−k.sub.SΔP.sub.ext−Δ.sub.TP

[0102] Then, as previously, the electronic entity 15 calculates a corrected level of leak F″ based on ΔP″ according to the previous equation.