DEVICE FOR SUPPLYING A PLURALITY OF CATHODES OF A FUEL SYSTEM

20240136553 ยท 2024-04-25

Assignee

Inventors

Cpc classification

International classification

Abstract

The invention relates to a supply device for compressed air to a plurality of cathodes (100a-100d) of a fuel cell system, characterized in that it comprises a motorized compressor (12) configured to provide a source of compressed air to all of the cathodes (100a-100d), a group of ducts configured to conduct the compressed air to each cathode (100a-100d), for each cathode (100a-100d), a proportioning valve (20a-20d) upstream or downstream of said cathode (100a-100d) which is configured to regulate the flow rate of compressed air passing through said cathode (100a-100d), anti-pumping protection means (30, 32) configured to allow the flow of a minimum flow rate of compressed air leaving the compressor (12), and a control device (24) configured to control the speed of the compressor (12) and the opening or closing of each proportioning valve (20a-20d) and/or the operation of the anti-pumping protection means (30, 32).

Claims

1. A device for supplying compressed air to a plurality of cathodes of a fuel cell system, comprising: a motorized compressor configured to provide a source of compressed air to all the cathodes; a group of ducts configured to conduct the compressed air towards each cathode; for each cathode, a proportioning valve upstream or downstream of said cathode configured to regulate the flow rate of compressed air passing through said; anti-pumping protection means configured to permit the flow of a minimum flow rate of compressed air leaving the compressor, a control device configured to control the speed of the compressor and the opening or closing of each proportioning valve and/or the operation of the anti-pumping protection means, and in that at least one proportioning valve comprises a minimum passage section configured to permit the passage of a minimum flow rate of compressed air when said proportioning valve is in the closed position, each minimum passage section forming an anti-pumping protection means.

2. The supply device as claimed in claim 1, wherein the anti-pumping protection means comprises a duct for bypassing all the cathodes, and a bypass valve configured to allow the flow of no compressed air, some of the compressed air or all the compressed air in the bypass duct, and in that the control device is configured to control the opening or closing of the bypass valve.

3. The supply device as claimed in claim 1, further comprising means for measuring the pressure of the compressed air leaving the compressor, and in that the control device is configured to control the speed of the compressor and the opening or closing of each proportioning valve and the anti-pumping protection means depending on the data coining from the means for measuring the pressure of the compressed air leaving the compressor.

4. The supply device as claimed in claim 1, further comprising means for measuring the temperature of the compressed air leaving the compressor, and in that the control device is configured to control the speed of the compressor and the opening or closing of each proportioning valve and the anti-pumping protection means depending on the data coining from the means for measuring the temperature of the compressed air leaving the compressor.

5. The supply device as claimed in claim 1, further comprising means for measuring the flow rate of the compressed air leaving the compressor, and in that the control device is configured to control the speed of the compressor and the opening or closing of each proportioning valve and the anti-pumping protection means depending on the data coining from the means for measuring the flow rate of the compressed air leaving the compressor.

6. The supply device as claimed in claim 1, characterized in that the control device is configured to control the speed of the compressor and the opening or closing of each proportioning valve and of the anti-pumping protection means depending on the power to be provided by the fuel cell system.

7. The supply device as claimed in claim 1, characterized in that the control device is supplied with power by at least one fuel cell of the fuel cell system.

8. The supply device as claimed in claim 1, further comprising at least one heat exchanger arranged downstream of the compressor and upstream of the cathodes, which is configured to cool the compressed air.

9. The supply device as claimed in claim 1, further comprising an output turbine arranged downstream of the cathodes and configured to regulate the pressure of the compressed air downstream of the cathodes.

10. A fuel cell system comprising a plurality of fuel cells, each fuel cell comprising a cathode configured to receive compressed air, characterized in that the fuel cell system comprises a supply device configured to supply compressed air to at least two cathodes of said fuel cell system the supply device comprising: a motorized compressor configured to provide a source of compressed air to all the cathodes; a group of ducts configured to conduct the compressed air towards each cathode; for each cathode, a proportioning valve upstream or downstream of said cathode configured to regulate the flow rate of compressed air passing through said; anti-pumping protection means configured to permit the flow of a minimum flow rate of compressed air leaving the compressor, a control device configured to control the speed of the compressor and the opening or closing of each proportioning valve and/or the operation of the anti-pumping protection means, and in that at least one proportioning valve comprises a minimum passage section configured to permit the passage of a minimum flow rate of compressed air when said proportioning valve is in the closed position, each minimum passage section forming an anti-pumping protection means.

Description

LIST OF FIGURES

[0047] Other aims, features and advantages of the invention will become apparent upon reading the following description given solely in a non-limiting way and which makes reference to the attached figures in which:

[0048] FIG. 1 is a schematic view of a supply device in accordance with a first embodiment of the invention.

[0049] FIG. 2 is a schematic view of a supply device in accordance with a second embodiment of the invention.

[0050] FIG. 3 is a schematic view of a supply device in accordance with a third embodiment of the invention.

[0051] FIG. 4 is a schematic view of a supply device in accordance with a fourth embodiment of the invention.

DETAILED DESCRIPTION OF AN EMBODIMENT OF THE INVENTION

[0052] In the figures, for the purposes of illustration and clarity, scales and proportions have not been strictly respected.

[0053] Furthermore, identical, similar or analogous elements are designated by the same reference signs in all the figures.

[0054] FIGS. 1 to 4 schematically illustrate a supply device 10 respectively according to a first embodiment of the invention, a second embodiment of the invention, a third embodiment of the invention and a fourth embodiment of the invention.

[0055] The supply device 10 is configured to supply compressed air to a plurality of cathodes 100a, 100b, 100c, 100d of a fuel cell system, only four of which are shown here. In practice, some tens of cathodes can be supplied with air, preferably around ten cathodes.

[0056] In order to do this, the supply device 10 comprises a compressor 12 motorized by a motor 14, the speed of which is controlled by a motor controller 16. The compressor 12 can form part of a motorized turbocompressor and thus be associated with a turbine 18 intended e.g. to assist the motor 14 in recovering energy by expansion of an air source. In particular, the air source can be the outlet of the supply device 10 as described below.

[0057] The compressor 12 makes it possible to provide the cathodes 100a, 100b, 100c, 100d with compressed air necessary to the operation of the fuel cells of the fuel cell system. The compressed air is thus distributed to each of the cathodes 100a, 100b, 100c, 100d. The compressed air can be cooled by one or a plurality of heat exchangers 19 arranged downstream of the compressor and upstream of the cathodes.

[0058] The supply device 10 comprises, for each cathode, a proportioning valve configured to regulate the flow rate of compressed air passing through said cathode.

[0059] In the first and third embodiments, with reference to FIG. 1 and FIG. 3, the proportioning valves 20a, 20b, 20c, 20d are disposed upstream of the cathode.

[0060] In the second and fourth embodiments, with reference to FIG. 2 and FIG. 4, the proportioning valves 22a, 22b, 22c, 22d are disposed downstream of the cathode.

[0061] In the four embodiments, the proportioning valves are controlled by a control device 24. The control device 24 receives data from a sensor 26 disposed at the outlet of the compressor 12, and configured to measure the pressure, temperature and/or flow rate of compressed air leaving the compressor 12.

[0062] According to the data received from the sensor 26 and the power requirements of the fuel cells of the fuel cell system, the control device 24 regulates the flow rate of compressed air passing through each cathode by virtue of the proportioning valves. The control device 24 is also configured to control the speed of the compressor 12 by sending commands to the controller 16 of the motor 14.

[0063] At the outlet of the cathodes, an outlet turbine 28 makes it possible to regulate the pressure of the compressed air, in particular to regulate the back pressure phenomena. In a preferred embodiment, as shown in FIG. 2 and FIG. 4, the turbine 28 and the turbine 18 assisting the motor 14 are one and the same turbine, some of the residual energy in the compressed air leaving the cathodes thus being recovered in order to assist the motor 14 driving the compressor 12, and thus to reduce its consumption of electricity.

[0064] The supply device 10 also comprises anti-pumping protection means which ensure the flow of a minimum flow rate of compressed air leaving the compressor.

[0065] In all the embodiments, anti-pumping protection means are integrated in the proportioning valves which each comprise a minimum passage section 34a, 34b, 34c, 34d configured to permit the passage of a minimum flow rate of compressed air when said proportioning valve is in the closed position. The minimum flow rates taken as a whole for each proportioning valve having a minimum passage section make it possible to ensure a minimum flow rate downstream of the compressor 12 in order to avoid pumping. According to the embodiments. one or some or all of the proportioning valves can comprise a minimum passage section, depending on the desired minimum flow rate of air. In the first and fourth embodiments, with reference to FIG. 1 and FIG. 4, the anti-pumping protection means also comprise a duct 30 for bypassing all of the cathodes, comprising a bypass valve 32 configured to permit the flow of no compressed air, some of the compressed air or all the compressed air in the bypass duct 30. The opening or the closing of the bypass valve 32 is controlled by the control device 24 so as to ensure the flow of a minimum flow rate in order to avoid pumping of the compressor.

[0066] In the second embodiment, with reference to FIG. 2, the anti-pumping protection means are only integrated in the proportioning valves 22a, 22b, 22c, 22d which each comprise a minimum passage section 34a, 34b, 34c, 34d configured to permit the passage of a minimum flow rate of compressed air when said proportioning valve 22a, 22b, 22c, 22d is in the closed position.

[0067] In the third embodiment, with reference to FIG. 3, the anti-pumping protection means are only integrated in the proportioning valves 20a, 20b, 20c, 20d which each comprise a minimum passage section 34a, 34b, 34c, 34d configured to permit the passage of a minimum flow rate of compressed air when said proportioning valve 20a, 20b, 20c, 20d is in the closed position.

[0068] The invention is not limited to the embodiments described. In particular, the turbine 18 and the turbine 28 can be one and the same turbine or two different turbines in the different embodiments illustrated.