CN112421075A - Air supply system of fuel cell engine - Google Patents
Air supply system of fuel cell engine Download PDFInfo
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- CN112421075A CN112421075A CN202011287018.6A CN202011287018A CN112421075A CN 112421075 A CN112421075 A CN 112421075A CN 202011287018 A CN202011287018 A CN 202011287018A CN 112421075 A CN112421075 A CN 112421075A
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- fuel cell
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/04—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
- H01M8/04082—Arrangements for control of reactant parameters, e.g. pressure or concentration
- H01M8/04089—Arrangements for control of reactant parameters, e.g. pressure or concentration of gaseous reactants
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/04—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
- H01M8/04082—Arrangements for control of reactant parameters, e.g. pressure or concentration
- H01M8/04089—Arrangements for control of reactant parameters, e.g. pressure or concentration of gaseous reactants
- H01M8/04104—Regulation of differential pressures
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/04—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
- H01M8/04082—Arrangements for control of reactant parameters, e.g. pressure or concentration
- H01M8/04089—Arrangements for control of reactant parameters, e.g. pressure or concentration of gaseous reactants
- H01M8/04111—Arrangements for control of reactant parameters, e.g. pressure or concentration of gaseous reactants using a compressor turbine assembly
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/04—Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
- H01M8/04082—Arrangements for control of reactant parameters, e.g. pressure or concentration
- H01M8/04201—Reactant storage and supply, e.g. means for feeding, pipes
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/24—Grouping of fuel cells, e.g. stacking of fuel cells
- H01M8/2465—Details of groupings of fuel cells
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/50—Fuel cells
Abstract
The invention discloses an air supply system of a fuel cell engine, comprising: a fuel cell stack; one end of the main gas supply path is connected with a cathode inlet of the fuel cell stack, the other end of the main gas supply path is communicated with the external environment, and a gas compressor is arranged on the main gas supply path; one end of the main exhaust path is connected with a cathode outlet of the fuel cell stack, the other end of the main exhaust path is communicated with the external environment, and a turbine is arranged on the main exhaust path; one end of the gas supply bypass branch is connected with the gas supply main path, the connection point of the gas supply bypass branch is positioned behind the gas compressor, the other end of the gas supply bypass branch is connected with the exhaust main path, the connection point of the gas supply bypass branch is positioned in front of the turbine, and a bypass valve is arranged on the gas supply bypass branch; and one end of an output shaft of the driving motor is connected with the gas compressor, and the other end of the output shaft of the driving motor is connected with the turbine. The air supply system of the fuel cell engine can recover the exhaust energy of the fuel cell and simultaneously avoid the surge of the air compressor.
Description
Technical Field
The invention relates to the technical field of fuel cells, in particular to an air supply system of a fuel cell engine.
Background
A fuel cell is an energy conversion device that converts chemical energy into electrical energy by means of an electrochemical reaction between hydrogen and oxygen. The fuel cell has the characteristics of high efficiency and no pollution, so the fuel cell is widely applied to the field of automobiles and is used as an engine of the automobiles.
In order to operate the fuel cell efficiently and reliably, it is necessary to provide sufficient air to the cathode of the fuel cell, and also to meet the requirements of temperature, humidity, and pressure, and therefore an air supply system is required to provide air to the fuel cell. The air compressor is an important part of the air supply system, can provide enough air flow and pressure for the fuel cell, and is also the most energy-consuming part in the air supply system. With the increasing power of the fuel cell, the pressure ratio and the flow requirement on the air compressor are also increased, and the energy consumption of the air compressor is also increased. In addition, the air compressor is generally a centrifugal air compressor, but the centrifugal air compressor can generate surge under low-load working conditions, and the air compressor is easy to generate surge due to the fact that the air flow required when the fuel cell stack enters the low-load working conditions is reduced, so that the air compressor is damaged, and the working stability of an air supply system is influenced.
Disclosure of Invention
In order to solve the technical problems, the invention provides an air supply system of a fuel cell engine, which can recover the exhaust energy of a fuel cell, reduce the energy consumption of an air compressor and simultaneously avoid the surge of the air compressor.
The invention adopts the following technical scheme:
a fuel cell engine air supply system comprising:
a fuel cell stack;
one end of the main gas supply path is connected with a cathode inlet of the fuel cell stack, the other end of the main gas supply path is communicated with the external environment, and a gas compressor is arranged on the main gas supply path;
one end of the main exhaust path is connected with a cathode outlet of the fuel cell stack, the other end of the main exhaust path is communicated with the external environment, and a turbine is arranged on the main exhaust path;
one end of the gas supply bypass branch is connected with the gas supply main path, the connection point of the gas supply bypass branch is positioned behind the gas compressor, the other end of the gas supply bypass branch is connected with the gas exhaust main path, the connection point of the gas supply bypass branch is positioned in front of the turbine, and an air bypass valve is arranged on the gas supply bypass branch;
and one end of an output shaft of the driving motor is connected with the gas compressor, and the other end of the output shaft of the driving motor is connected with the turbine.
Optionally, a back pressure valve is arranged on the exhaust main path to adjust the cathode pressure of the fuel cell stack by adjusting the back pressure valve.
Optionally, the fuel cell engine air supply system further includes a turbine bypass branch, two ends of the turbine bypass branch are respectively connected to the front end and the rear end of the turbine, and a turbine bypass valve is arranged on the turbine bypass branch.
Optionally, the fuel cell engine air supply system further includes a gas-liquid separator provided on the exhaust main passage and between the back pressure valve and the turbine.
Optionally, an intercooler is disposed on the air supply main circuit between the air compressor and the fuel cell stack.
Optionally, one end of the air supply bypass branch connected to the main air supply path is disposed between the air compressor and the intercooler, and one end of the air supply bypass branch connected to the main exhaust path is disposed between the gas-liquid separator and the turbine.
Optionally, the fuel cell engine air supply system further comprises a humidifier and a humidifier bypass branch;
the humidifier is arranged on the main gas supply path and the main gas exhaust path, so that the gas flowing through the humidifier in the main gas exhaust path can humidify the gas flowing through the humidifier on the main gas supply path;
the humidifier bypass branch is provided with a humidifier bypass valve and used for adjusting the air flow passing through the humidifier on the air supply main path or adjusting the air flow passing through the humidifier on the air exhaust main path.
Optionally, an air inlet shutdown valve is arranged at the front end of the cathode inlet of the fuel cell stack;
and an exhaust shutdown valve is arranged at the front end of the cathode outlet of the fuel cell stack.
Optionally, an air filter is arranged at the front end of the air compressor on the air supply main path.
Optionally, the liquid outlet of the gas-liquid separator is sequentially connected with a water storage tank and a drain valve.
The invention has the advantages that: the air supply bypass branch is arranged on the air supply main path and connected to the exhaust main path, and an air bypass valve is arranged on the air supply bypass branch; the exhaust main path is provided with a turbine, the exhaust energy of the fuel cell can be recovered, and meanwhile, the air bypassed by the air supply bypass branch path can work on the turbine, so that the turbine can recover part of energy additionally consumed by the compressor due to surge prevention, and the energy consumption of the driving motor is reduced.
Drawings
FIG. 1 is a schematic configuration diagram of a first embodiment of a fuel cell engine air supply system according to the present invention;
FIG. 2 is a schematic configuration diagram of a second embodiment of the air supply system for a fuel cell engine according to the present invention;
FIG. 3 is a schematic configuration diagram of a third embodiment of the air supply system for a fuel cell engine according to the present invention;
FIG. 4 is a schematic configuration diagram of a fourth embodiment of the air supply system for a fuel cell engine according to the present invention;
FIG. 5 is a schematic configuration diagram of a fifth embodiment of the air supply system for a fuel cell engine according to the present invention;
FIG. 6 is a schematic configuration diagram of a sixth embodiment of the air supply system for a fuel cell engine according to the present invention;
fig. 7 is a schematic configuration diagram of a seventh embodiment of the air supply system for a fuel cell engine in the present invention.
In the figure:
101. a fuel cell stack; 102. a drive motor; 103. a humidifier; 104. a humidifier bypass valve;
110. a main gas supply path; 111. a compressor; 112. an intake shutdown valve; 113. an air filter; 114. an intercooler;
120. a gas supply bypass branch; 121. an air bypass valve;
210. an exhaust main path; 211. a turbine; 212. a back pressure valve; 213. a gas-liquid separator; 214. an orifice; 215. a water storage tank; 216. a drain valve; 217. an exhaust shutdown valve;
220. a turbine bypass branch; 221. a turbine bypass valve.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the invention and are not limiting of the invention. It should be further noted that, for the convenience of description, only some of the structures related to the present invention are shown in the drawings, not all of the structures.
In the description of the present invention, unless expressly stated or limited otherwise, the terms "connected," "connected," and "fixed" are to be construed broadly, e.g., as meaning permanently connected, removably connected, or integral to one another; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
The technical scheme of the invention is further explained by the specific implementation mode in combination with the attached drawings.
The present invention provides a fuel cell engine air supply system, fig. 1 is a schematic structural diagram of a first embodiment of the fuel cell engine air supply system of the present invention, and as shown in fig. 1, the fuel cell engine air supply system includes a fuel cell stack 101, a main air supply path 110, a main exhaust path 210, a bypass air supply path 120, and a driving motor 102.
One end of the main gas supply path 110 is connected to the cathode inlet of the fuel cell stack 101, and the other end of the main gas supply path 110 communicates with the external environment, so that the main gas supply path 110 can supply gas to the cathode of the fuel cell stack 101. The main air supply path 110 is provided with a compressor 111, and the compressor 111 presses air of the external environment into the main air supply path 110 to make the air flow into the cathode of the fuel cell stack 101.
One end of the main exhaust path 210 is connected to the cathode outlet of the fuel cell stack 101, and the other end is communicated with the external environment, so that the main exhaust path 210 exhausts the gas to the external environment. A turbine 211 is provided in the main exhaust path 210, and the turbine 211 can use the air in the main exhaust path 210 to perform work.
One end of an output shaft of the driving motor 102 is connected with the compressor 111, the other end of the output shaft of the driving motor 102 is connected with the turbine 211, the driving motor 102 can drive the compressor 111 to rotate, and the other end of the driving motor 102 is also connected with the turbine 211, so that exhaust energy recovered by the turbine 211 can be directly transmitted to the compressor 111 through the output shaft of the driving motor 102, and power consumption of the driving motor 102 is reduced. In one embodiment, the output shaft of the drive motor 102 is supported by an air bearing, the air supply line of which is integrated in the compressor 111 and the air exhaust line of which is integrated in the turbine 211.
As shown in fig. 1, one end of the bypass branch line 120 is connected to the main supply line 110, and the connection point is located after the compressor 111, and the other end of the bypass branch line 120 is connected to the main exhaust line 210, and the connection point is located before the turbine 211, where "front" and "rear" refer to a place where air flows first and a place where air flows later are "front" and "rear" respectively, in terms of the flow direction of air. The bypass air supply branch 120 is provided with an air bypass valve 121, which is an electromagnetic valve capable of controlling the flow and the stop of the air in the bypass branch and adjusting the flow rate. Due to the arrangement of the air supply bypass branch 120, the air flow of the air supply bypass branch 120 can be adjusted by controlling the opening of the air bypass valve 121 on the air supply bypass branch 120, when the fuel cell stack 101 enters a low-load working condition, the air bypass valve 121 is opened, and part of air of the main air supply path 110 is bypassed from the air supply bypass branch 120, so that the flow of the air compressor 111 is ensured to be larger than a surge limit, and meanwhile, the air flow required by the fuel cell stack 101 can be ensured. Since the outlet of the bypass air supply branch 120 is located in front of the inlet of the turbine 211, the air of the bypass air supply branch 120 can do work on the turbine 211, and the turbine 211 can recover part of energy additionally consumed by the compressor 111 due to surge prevention, thereby reducing energy consumption of the driving motor 102.
Referring to fig. 1, in one embodiment, a back pressure valve 212 is disposed on the main exhaust path 210, and the back pressure valve 212 can control the cathode pressure of the fuel cell stack 101. The turbine 211 has a capability of building an air supply system pressure, which refers to the cathode pressure of the fuel cell stack 101, during normal operation, so that the back pressure valve 212 is fully opened as much as possible, so that more air flows through the turbine 211, which is beneficial for the turbine 211 to recover more energy, and when the pressure built by the turbine 211 is insufficient, that is, the cathode pressure of the fuel cell stack 101 is insufficient, the back pressure valve 212 is adjusted to reduce the opening of the back pressure valve 212, so as to assist the turbine 211 in building the air supply system pressure, which makes the cathode of the fuel cell stack 101 have sufficient pressure.
Further, referring to fig. 1, the fuel cell engine air supply system further includes a turbine bypass branch 220, two ends of the turbine bypass branch 220 are respectively connected to the front end and the rear end of the turbine 211, that is, one end of the turbine bypass branch 220 is located in front of an inlet of the turbine 211, the other end of the turbine bypass branch 220 is located behind an outlet of the turbine 211, a turbine bypass valve 221 is disposed on the turbine bypass branch 220, the turbine bypass valve 221 is similar to the air bypass valve 121, and the turbine bypass valve 221 can control the flow rate of the turbine bypass branch 220. The turbine bypass valve 221 is normally closed, and when the back pressure valve 212 is fully opened and the cathode pressure of the fuel cell stack 101 is still greater than the target pressure, the turbine bypass valve 221 is adjusted to increase the opening of the turbine bypass valve 221, and part of the gas flows out through the turbine bypass branch 220 to reduce the cathode pressure of the fuel cell stack 101.
With continued reference to fig. 1, in one embodiment, the fuel cell engine air supply system further includes a gas-liquid separator 213, the gas-liquid separator 213 being disposed on the main exhaust gas path 210 and between the backpressure valve 212 and the turbine 211. Specifically, as shown in fig. 1, an inlet of the gas-liquid separator 213 is connected to the back pressure valve 212, an outlet of the gas-liquid separator 213 is connected to an inlet of the turbine 211, and an outlet of the gas-liquid separator 213 is connected to the external environment, so as to discharge the separated liquid. The gas-liquid separator 213 separates liquid water in the cathode exhaust gas of the fuel cell stack 101 and discharges the liquid water to the external environment, and the remaining gas enters the turbine 211 to apply work to the turbine 211, thereby preventing the liquid water discharged from the fuel cell stack 101 from damaging the turbine 211. Preferably, the outlet of gas-liquid separator 213 is in communication with the external environment via orifice 214.
Fig. 2 is a schematic structural view of a second embodiment of the air supply system of the fuel cell engine of the present invention, and as shown in fig. 2, the liquid outlet of the gas-liquid separator 213 is sequentially connected to a water storage tank 215 and a drain valve 216, and after the liquid separated by the gas-liquid separator 213 is drained to the water storage tank 215, the water storage tank 215 is controlled by the drain valve 216 to drain water, so that the water drainage can be controlled, and the liquid can be drained once at regular intervals, thereby preventing the gas-liquid separator 213 from continuously draining water.
In one embodiment, as shown in fig. 1, the fuel cell engine air supply system further includes a humidifier 103 and a humidifier bypass branch, the humidifier bypass branch having a humidifier bypass valve 104 disposed thereon, the humidifier bypass valve 104 being similar to the air bypass valve 121, the humidifier bypass valve 104 being operable to regulate a flow rate of the humidifier bypass branch. The humidifier 103 is disposed on the main air supply path 110 and the main exhaust path 210, specifically, as shown in fig. 1, the air on the main air supply path 110 and the main exhaust path 210 both passes through the humidifier 103, moisture exchange is performed in the humidifier 103 through the main air supply path 110 and the main exhaust path 210, moisture in the air in the main exhaust path 210 enters the air in the main air supply path 110, so as to humidify the air in the main air supply path 110, a specific moisture exchange principle is the prior art, and details are not repeated herein. The humidifier bypass branch may be disposed on the main gas supply path 110 to adjust the amount of gas passing through the humidifier on the main gas supply path 110, or disposed on the main exhaust path 210 to adjust the amount of gas passing through the humidifier on the main exhaust path 210. In fig. 1, the humidifier bypass branch is disposed on the main exhaust path 210, and as shown in fig. 1, when the air discharged from the fuel cell stack 101 reaches the humidifier 103, the air is divided into two paths, one path enters the humidifier 103, the other path passes through the humidifier bypass valve 104 on the humidifier bypass branch, and finally passes through the back pressure valve 212 after being merged, and the amount of air flow passing through the humidifier bypass branch in the main exhaust path 210 can be adjusted by adjusting the opening degree of the humidifier bypass valve 104, so as to control the amount of air flow passing through the humidifier 103 in the main exhaust path 210, thereby achieving adjustment of the air humidity on the main air supply path 110. As shown in fig. 3, the humidifier bypass branch is disposed on the main air supply branch 110, when the air in the main air supply branch 110 reaches the humidifier 103, the air is divided into two paths, one path enters the humidifier 103, the other path passes through the humidifier bypass valve 104 on the humidifier bypass branch, and finally enters the fuel cell stack 101 after being merged, the air flow passing through the humidifier bypass branch in the main air supply branch 110 can be adjusted by adjusting the opening degree of the humidifier bypass valve 104, so as to control the air flow passing through the humidifier 103 in the main air supply branch 110, thereby realizing the adjustment of the air humidity on the main air supply branch 110.
Referring to fig. 1, the fuel cell engine air supply system further includes an intake stop valve 112 and an exhaust stop valve 217, the intake stop valve 112 is disposed at the front end of the cathode inlet of the fuel cell stack 101, and the exhaust stop valve 217 is disposed at the front end of the cathode outlet of the fuel cell stack 101. The humidity and the cleanliness of the fuel cell stack 101 can be guaranteed by arranging the stop valve, the air inlet stop valve 112 is close to the cathode inlet of the fuel cell stack 101, the exhaust stop valve 217 is close to the cathode outlet of the fuel cell stack 101, and when the fuel cell stack 101 stops, the air inlet stop valve 112 and the exhaust stop valve 217 are closed to play a role in sealing.
In order to ensure the cleanliness of air in the air supply system of the fuel cell engine, as shown in fig. 1, an air filter 113 is disposed on the main air supply path 110 at the front end of the compressor 111, the inlet of the air filter 113 is connected to the external environment, the outlet of the air filter 113 is connected to the inlet of the compressor 111, and the air filter 113 can remove particulate matter and harmful components from the external environment.
Referring to fig. 1, the fuel cell engine air supply system further includes an intercooler 114, the intercooler 114 is disposed between the compressor 111 and the fuel cell stack 101 on the main air supply path 110, and when the humidifier 103 is disposed, the intercooler 114 is disposed between the compressor 111 and the humidifier 103. The intercooler 114 may control the inlet air temperature of the cathode of the fuel cell stack 101, so as to lower the temperature of the air pressurized by the compressor 111.
Referring to fig. 1, the positions of the two ends of the bypass branch 120 on the main supply path 110 and the main exhaust path 210 can be flexibly adjusted. In one embodiment, as shown in fig. 1, one end of the bypass branch air supply 120 connected to the main air supply path 110 is disposed between the compressor 111 and the intercooler 114, and one end of the bypass branch air supply 120 connected to the main exhaust path 210 is disposed between the gas-liquid separator 213 and the turbine 211.
In the first embodiment, as shown in fig. 4, the end of the bypass gas supply branch 120 connected to the main gas supply branch 110 is provided between the intercooler 114 and the humidifier 103, and the end of the bypass gas supply branch 120 connected to the main exhaust branch 210 is provided between the back pressure valve 212 and the gas-liquid separator 213.
As shown in fig. 5, the end of the bypass air supply branch 120 connected to the main air supply branch 110 is provided between the intercooler 114 and the humidifier 103, and the end of the bypass air supply branch 120 connected to the main exhaust branch 210 is provided between the gas-liquid separator 213 and the turbine 211.
As shown in fig. 6, one end of the bypass branch line 120 connected to the main supply line 110 is provided between the compressor 111 and the intercooler 114, and one end of the bypass branch line 120 connected to the main exhaust line 210 is provided between the back pressure valve 212 and the gas-liquid separator 213.
In one embodiment, as shown in fig. 7, the fuel cell engine air supply system does not need to be provided with the humidifier 103 and a humidifier bypass branch, so that the overall structure is simplified and the cost is saved.
It should be understood that the above-described embodiments of the present invention are merely examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention. Numerous obvious variations, adaptations and substitutions will occur to those skilled in the art without departing from the scope of the invention. And are neither required nor exhaustive of all embodiments. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be included in the protection scope of the claims of the present invention.
Claims (10)
1. A fuel cell engine air supply system, comprising:
a fuel cell stack (101);
a main gas supply path (110), one end of which is connected with the cathode inlet of the fuel cell stack (101), and the other end of which is communicated with the external environment, wherein a gas compressor (111) is arranged on the main gas supply path (110);
a main exhaust path (210) having one end connected to a cathode outlet of the fuel cell stack (101) and the other end communicating with the outside environment, the main exhaust path (210) being provided with a turbine (211);
an air supply bypass branch (120), one end of which is connected with the air supply main path (110) and the connection point of which is positioned behind the compressor (111), and the other end of which is connected with the exhaust main path (210) and the connection point of which is positioned in front of the turbine (211), wherein an air bypass valve (121) is arranged on the air supply bypass branch (120);
one end of an output shaft of the driving motor (102) is connected with the compressor (111), and the other end of the output shaft of the driving motor (102) is connected with the turbine (211).
2. The fuel cell engine air supply system according to claim 1, wherein a back pressure valve (212) is provided on the exhaust main passage (210) to adjust a cathode pressure of the fuel cell stack (101) by adjusting the back pressure valve (212).
3. The fuel cell engine air supply system according to claim 2, further comprising a turbine bypass branch (220), both ends of the turbine bypass branch (220) being connected to front and rear ends of the turbine (211), respectively, the turbine bypass branch (220) being provided with a turbine bypass valve (221).
4. The fuel cell engine air supply system according to claim 2, further comprising a gas-liquid separator (213), the gas-liquid separator (213) being provided on the exhaust main passage (210) and between the back pressure valve (212) and the turbine (211).
5. A fuel cell engine air supply system according to claim 4, characterized in that an intercooler (114) is provided on the main air supply path (110) between the compressor (111) and the fuel cell stack (101).
6. The fuel cell engine air supply system according to claim 5, wherein an end of the air supply bypass branch passage (120) connected to the main air supply passage (110) is provided between the compressor (111) and the intercooler (114), and an end of the air supply bypass branch passage (120) connected to the main exhaust passage (210) is provided between the gas-liquid separator (213) and the turbine (211).
7. The fuel cell engine air supply system according to claim 1, further comprising a humidifier (103) and a humidifier bypass branch;
the humidifier (103) is arranged on the main gas supply path (110) and the main gas exhaust path (210) so that the gas flowing through the humidifier (103) in the main gas supply path (210) can humidify the gas flowing through the humidifier (103) on the main gas supply path (110);
the humidifier bypass branch is provided with a humidifier bypass valve (104) and used for adjusting the air quantity passing through the humidifier (103) on the air supply main path (110) or adjusting the air quantity passing through the humidifier (103) on the air exhaust main path (210).
8. A fuel cell engine air supply system according to claim 1, characterized in that the cathode inlet front end of the fuel cell stack (101) is provided with an intake air stop valve (112);
and an exhaust stop valve (217) is arranged at the front end of the cathode outlet of the fuel cell stack (101).
9. A fuel cell engine air supply system according to claim 1, wherein an air filter (113) is provided on the main air supply path (110) at a front end of the compressor (111).
10. The fuel cell engine air supply system according to claim 4, wherein a water storage tank (215) and a drain valve (216) are connected to an outlet of the gas-liquid separator (213) in this order.
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CN114177954A (en) * | 2021-11-10 | 2022-03-15 | 上海凌逐新能源科技有限公司 | Following air inlet fresh air system of environmental test chamber of fuel cell system |
CN114497636A (en) * | 2022-04-18 | 2022-05-13 | 山东国创燃料电池技术创新中心有限公司 | Fuel cell system and energy recovery control method thereof |
CN114725446A (en) * | 2022-05-09 | 2022-07-08 | 一汽解放汽车有限公司 | Flow control method for fuel cell system |
CN114759229A (en) * | 2022-05-09 | 2022-07-15 | 一汽解放汽车有限公司 | Fuel cell control system |
WO2022151574A1 (en) * | 2021-01-12 | 2022-07-21 | 海德韦尔(太仓)能源科技有限公司 | Compressor, air compressor comprising compressor, and fuel cell device |
CN114865009A (en) * | 2022-06-14 | 2022-08-05 | 一汽解放汽车有限公司 | Fuel cell gas path control system and electric pile inlet pressure control method |
CN114899450A (en) * | 2022-04-08 | 2022-08-12 | 海德韦尔(太仓)能源科技有限公司 | Fuel cell system with gas turbine supercharger |
CN116169319A (en) * | 2023-03-01 | 2023-05-26 | 广州汽车集团股份有限公司 | Air supply system and control method for air supply system |
WO2023237309A1 (en) * | 2022-06-10 | 2023-12-14 | Robert Bosch Gmbh | Method for operating a fuel cell system |
WO2024003169A1 (en) * | 2022-06-30 | 2024-01-04 | Mahle International Gmbh | Fuel cell system and operating method |
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