CN216524688U - Fuel cell experiment system capable of reducing turbulence - Google Patents
Fuel cell experiment system capable of reducing turbulence Download PDFInfo
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- CN216524688U CN216524688U CN202122646254.9U CN202122646254U CN216524688U CN 216524688 U CN216524688 U CN 216524688U CN 202122646254 U CN202122646254 U CN 202122646254U CN 216524688 U CN216524688 U CN 216524688U
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Abstract
The utility model discloses a fuel cell experimental system for reducing turbulence, and relates to the technical field of fuel cell cabin testing. The utility model discloses a for solve the test cabin inner flow field control problem of fuel cell system, avoid the under-deck local torrent to appear, set up the miniflow channel on the cabin body, the miniflow channel is the small-size wind gap of opening in the lateral wall and the bottom surface of fuel cell system test cabin air intake one side, and it is continuous through pipeline and miniflow channel fan, and each miniflow channel wind gap unit can switching alone. Small air suction openings are formed in the top of the fuel cell system test cabin and one side of each air suction opening and are connected with the air suction openings through pipelines. When the fuel cell system works at high power, the micro-channel can be used for blowing the turbulent flow formed during the circulation of the main air channel and changing a dispersion flow field; and can be used for blowing off the locally gathered hydrogen in the cabin; when the fuel cell system is used for cold soaking experiments, the main air channel is closed, and the temperature of air in the cabin is stable under the condition of keeping lower wind speed by means of micro-channel circulation.
Description
Technical Field
The utility model relates to the technical field of fuel cell cabin testing, in particular to a fuel cell experiment system capable of reducing turbulence.
Background
With the increasing severity of energy crisis and environmental pollution problems, new energy automobiles have rapidly developed opportunities, wherein hydrogen fuel cell automobiles are used as ultimate clean energy, have unique technical and environmental protection advantages in the application aspect of trucks and large passenger automobiles, and are one of the main directions for the development of new energy automobiles in the future. The test chamber of the hydrogen fuel cell power generation system (hereinafter referred to as system) is restricted by the prior art due to the factors of high hydrogen-related safety requirement, large heat productivity, large fresh air demand and the like, and the common environmental test chamber which is conventionally used at present cannot meet the test requirement of the fuel cell and cannot support the high-power continuous operation of the fuel cell system. The existing universal environmental test chamber has the following defects:
1. the traditional environmental test chamber adopts a heat exchange mode of convection in the chamber, so that the temperature difference is large due to overlarge heat in the chamber and limited air quality in the chamber, the temperature in the chamber is further disordered, and the test work cannot be carried out;
2. the traditional environmental test chamber adopts a circulating mode of convection in the chamber to cause humidity disorder, so that the test work can not be carried out;
3. local turbulence is more in traditional environmental test cabin, and the space that traditional environmental chamber of flow field took up is big.
An environmental chamber for fuel cell system performance testing is disclosed in utility model application No. CN 201621205466.
Although the utility model discloses a some problems have been solved, still have following scheduling problem to solve when using:
based on the electrochemical characteristics of the fuel cell system, the ratio of the chemical energy converted into the heat generation amount to the electricity generation amount in the operation is about 55% to 45%, and the heat generation amount is about 185kw taking the fuel cell system with 150kw of electricity generation power as an example. According to the cabin capacity of the fuel electric system test cabin, taking a 60m3 cabin as an example, the air density is 1.2kg/m3The total mass of air in the cabin is about 72kg, the total specific heat, constant pressure and specific heat capacity cp is 1.003 kJ/(kg), and the temperature difference delta t is required to be less than 2 ℃ according to the environment test working condition, as shown in the following formula:
Q＝Cp.r.Vs.ΔT
q is the cabin air heat load, and the unit is: kw, Cp is the specific heat capacity at constant pressure, unit kj/kg/DEG C; r is the air density in kg/m3(ii) a Vs is the cabin volume inm 3; delta. T is the temperature difference in the cabin and has the unit of ℃. Substituted into the above formula
Q＝Cp.r.Vs.ΔT
＝1.003kJ/(kg*℃)*1.2kg/m3*60m3*2℃
＝144kj
P is the scattered power in the fuel cell system cabin and has the unit of kw (kj/s); t is time in units of s. Taking a fuel cell with 150kw power generation capacity as an example, the heat generation amount is 185kw according to the following formula:
P＝Q/t
so that there are
t＝Q/P
＝144kj÷185kj/s
≈0.8s
According to the calculation result, if the traditional convection cabin is adopted, the convection cabin is arranged at 60m3The cabin capacity of the fuel cell system loaded with power generation of 150kw is 0.8 second, the temperature difference of air in the cabin exceeds 2 ℃, and the reliability test requirement of the fuel cell system cannot be met.
In addition, the turbulence in the cabin can cause that gas can not participate in circulation in the turbulent cyclone all the time, so that the heat exchange effect in the cabin is poor, and meanwhile, hydrogen can be slowly gathered in the cabin to cause greater danger. It is therefore necessary to design a new fuel cell module to solve the above problems.
Therefore, the applicant inherits the experience of abundant design development and actual manufacturing in the related industry for many years, researches and improves the existing structure and deficiency, and provides a fuel cell experimental system for reducing turbulence so as to achieve the aim of higher practical value.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Aiming at the defects of the prior art, the utility model provides a fuel cell experiment system for reducing turbulence, which solves the problems that the heat exchange quantity of the existing fuel cell bin is insufficient and the turbulence in the fuel cell bin cannot be coped with.
(II) technical scheme
In order to meet the requirement of a fuel system environment reliability test, the utility model adopts a wind tunnel type circulating air flow channel, simulates a flow field model that fresh air is blown into a vehicle body from the front of a vehicle head and hot air is blown out from the rear part of the vehicle body when the vehicle travels, and adopts an air advection flow field design in a cabin. The temperature-controlled fresh air is blown to the fuel cell system and the radiator of the fuel cell system from one side of the bulkhead, the hot air is sucked out from the other side of the bulkhead through the air suction duct, and then is blown out through the bulkhead air suction port after the temperature and humidity are controlled by equipment such as an extravehicular heat exchanger, a heater, a humidifying dehumidifier and the like, so as to circulate (as shown in figure 3).
By adopting the circulation mode, the air flowing through the air compressor of the fuel cell system and the radiator of the fuel cell which are sensitive to the ambient temperature is the circulating air subjected to temperature control and humidity control, and the circulating air heated by the fuel cell system and the heat exchanger of the fuel cell in the cabin is timely sucked away by the air suction opening, so that the circulation is prevented from being reserved in the cabin, the problem of cross convection circulation of cold air and hot air in the cabin is solved, and the temperature disorder in the cabin is prevented.
The utility model aims to solve the problem of flow field control in a fuel cell system test cabin and avoid local turbulence in the cabin, and one innovation is a micro-channel. The micro-channel is a small air port formed in the side wall and the bottom surface of one side of an air inlet of the fuel cell system test chamber, and is connected with a micro-channel fan through a pipeline, and each micro-channel air port unit can be independently opened and closed. Small air outlets are arranged at the top of the fuel cell system test chamber and one side of the air suction opening and are connected with the air inlet through a pipeline, and each micro-channel air outlet can be independently opened and closed. When the fuel cell system works at high power, the micro-channel can be used for blowing the turbulent flow formed during the circulation of the main air channel and changing a dispersion flow field; and can be used for blowing off locally gathered hydrogen in the cabin; when the fuel cell system is used for cold immersion experiments, the main air channel is closed, and the temperature of air in the cabin is stable under the condition that low air speed can be kept by means of micro-channel circulation.
In order to achieve the purpose, the utility model is realized by the following technical scheme: the utility model provides a reduce fuel cell experimental system of torrent, includes the cabin body, air intake and inlet scoop have been seted up on the cabin body, the inlet scoop is connected with the wind channel, the other end in wind channel and the air intake intercommunication of the cabin body, be provided with circulating fan and heat exchanger in the wind channel, set up on the cabin body and say the wind gap for the miniflow, circulating fan exports and miniflow way wind gap intercommunication.
Preferably, the inlet of the circulating fan is provided with a fresh air inlet.
Preferably, the outlet of the circulating fan is provided with a hydrogen discharge port.
Preferably, a flow guide plate is arranged at a corner in the air duct between the outlet of the circulating fan and the air inlet of the cabin body.
Preferably, a rectifying plate is arranged in the air inlet of the cabin body.
Preferably, an air outlet of the air inlet is provided with an air direction adjusting plate.
Preferably, a sample platform is arranged at the bottom in the cabin body.
Preferably, the heat exchanger is one of a refrigerating heat exchanger and a heating heat exchanger.
Preferably, the top of the cabin body is provided with an inclined top with inclination larger than 5 degrees, the highest position of the inclined top is provided with a strong exhaust port, and a micro-channel air port arranged at the top of the cabin body is communicated with the strong exhaust port.
Preferably, an explosion-proof fan is installed in the strong exhaust port.
(III) advantageous effects
The utility model provides a fuel cell experimental system capable of reducing turbulence. The method has the following beneficial effects:
(1) this fuel cell experimental system who reduces torrent adopts wind tunnel formula design, improves the heat transfer volume, sets up the microchannel wind gap on the bulkhead in environment cabin, can blow away the cyclone that the air current torrent and produce and further promote the heat transfer effect to can close the air intake of the cabin body in cold test, open the microchannel wind gap, utilize the amount of wind in microchannel wind gap can accomplish the experiment.
(2) The fuel cell experiment system for reducing turbulence is provided with the forced exhaust port at the top of the cabin body, so that hydrogen in the cabin can be exhausted, and the danger caused by hydrogen aggregation is reduced.
Drawings
FIG. 1 is a system diagram illustrating the use state of the present invention;
FIG. 2 is a schematic view of the structure of the cabin;
fig. 3 is a schematic view of an air cycle.
In the figure: 1. a cabin body; 2. a forced discharge port; 3. an air suction opening; 4. an air duct; 5. a fresh air inlet; 6. a circulating fan; 7. a heat exchanger; 8. a medium heater; 9. a baffle; 10. a hydrogen discharge port; 11. a rectifying plate; 12. a wind direction adjustment plate; 13. a microchannel tuyere; 14. a sample piece; 15. and a sample platform.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example 1: the most basic unit for realizing the functions of the utility model
The utility model provides a reduce fuel cell experimental system of torrent, includes the cabin body 1, has seted up air intake and inlet scoop 3 on the cabin body 1, and inlet scoop 3 is connected with wind channel 4, and the other end of wind channel 4 and the air intake intercommunication of the cabin body 1 are provided with circulating fan 6 and heat exchanger 7 in the wind channel 4, set up on the cabin body 1 for miniflow channel wind gap 13, circulating fan 6 export and miniflow channel wind gap 13 intercommunication.
Wherein:
cabin body 1: the cabin body 1 is formed by assembling heat insulation plates, and the inner side of the cabin body 1 is welded by a stainless steel inner container to realize air tightness.
Air inlet 3: the suction opening 3 is provided above the bulkhead side to facilitate the removal of hot air and hydrogen so that hydrogen and hot air having a density lower than the average density of air are sucked out.
Air duct 4: the air duct 4 is assembled by heat-insulating plates, and the inner side of the air duct is formed by welding stainless steel linings so as to increase the cross-sectional area of air circulation and reduce the air flow rate, so that hydrogen with the average density smaller than that of air can be conveniently removed from the separation.
And (7) a heat exchanger: the heat exchanger 7 may be a cooling heat exchanger or a heating heat exchanger.
And (6) a circulating fan: the explosion-proof circulating fan provides circulating power for the air in the cabin.
Micro flow channel tuyere 13: for auxiliary air outlet, a micro-channel air port 13 is generally arranged at a position where turbulent cyclone is easily formed in the cabin 1, and meanwhile, in order to facilitate the regulation and control of the flow of the micro-channel air port 13, a regulating valve is additionally arranged between the circulating fan 6 and the micro-channel air port 13.
In the implementation process, a micro-channel fan can be used for providing an air source for the micro-channel air port 13, and the inlet of the micro-channel fan can be communicated with the outlet of the circulating fan 6 or can be directly communicated with the air.
Each individual microchannel tuyere 13 can be provided with a regulating valve for regulation.
Example 2: in order to introduce fresh air into the cabin
The difference in embodiment 1 is that the inlet of the circulation fan 6 is provided with a fresh air inlet 5.
Example 3: in order to reduce the hydrogen concentration in the air duct 4
The difference in embodiment 1 is that the outlet of the circulation fan 6 is provided with a hydrogen discharge port 10.
Example 4:
the difference in embodiment 1 is that a baffle plate 9 is arranged at the turn in the air duct 4 between the outlet of the circulating fan 6 and the air inlet of the cabin 1.
Example 5: rectifying the air flow in the air duct
The difference of the embodiment 1 is that a rectifying plate 11 is arranged in the air inlet of the cabin 1 and is installed near the outlet of the air duct 4 to rectify the air in the air duct 4, so that the air outlet is smooth and has no turbulence.
Example 6: for adjusting the wind direction of the air inlet
The difference in embodiment 1 is that a wind direction adjusting plate 12 is provided at the air outlet of the air inlet.
Example 7: to place a sample 14
The difference in embodiment 1 is that a sample platform 15 is provided at the bottom inside the cabin 1.
Example 8: in order to reduce the hydrogen concentration in the cabin 1
The difference of the embodiment 1 is that the top of the cabin body 1 is provided with an inclined top with the inclination larger than 5 degrees, the highest part of the inclined top is provided with a strong exhaust port 2, and a micro-channel air port 13 arranged at the top of the cabin body 1 is communicated with the strong exhaust port 2.
Example 9: in order to further reduce the hydrogen concentration in the cabin 1
On the basis of any one of the embodiments 1 to 8, the explosion-proof fan is installed in the strong exhaust port 2.
Example 10: for adjusting the flow direction of the outlet air of the micro-channel tuyere 13
On the basis of the embodiment 1, the side wall of the air inlet side of the cabin body 1 and the micro-channel air port 13 on the bottom surface of the cabin body 1 are connected with a micro-channel fan (which can be a circulating fan 6) through a pipeline, and the side wall of the air suction port 3 side of the cabin body 1 and the micro-channel air port 13 on the top surface of the cabin body 1 are connected with the air suction port 3 through a pipeline.
When the system is in normal operation: the sample piece 14 is prevented from being arranged on a sample piece platform 15, air is pressurized by a circulating fan 6 in an air duct 4, then is cooled by a heat exchanger 7, then enters the cabin body 1 after passing through a medium heater 8, a guide plate 9 and a rectifying plate 11, meanwhile, a part of air is pressurized and then enters the cabin body 1 through a micro-channel air port 13, and because the micro-channel air port 13 is arranged at the position of turbulent cyclone, the turbulent cyclone at the corresponding position in the cabin body 1 can be blown away, so that the air in the cyclone enters the circulation. The air entering the cabin 1 cools the sample piece 14, enters the air duct 4 from the air suction opening 3, and then enters the circulating fan 6 together with the fresh air entering from the fresh air inlet 5. Wherein, the air duct 4 at the outlet of the medium heater 8 is provided with a hydrogen discharge port 10 which can discharge the hydrogen in the air duct 4.
When the system is used for cold dipping experiments: the sample piece 14 is prevented from being arranged on the sample piece platform 15, the air inlet of the cabin body 1 is closed by adjusting the angle of the wind direction adjusting plate 12, and meanwhile, the adjusting valve between the circulating fan 6 and the micro-channel air port 13 is also ensured to be opened, so that the air circulation in the cabin body 1 is ensured.
In conclusion, the fuel cell experiment system for reducing turbulence adopts a wind tunnel type design to improve the heat exchange amount, the micro-channel air port is arranged on the bulkhead of the environmental chamber, the cyclone generated by airflow turbulence can be blown away to further improve the heat exchange effect, the air inlet of the chamber body can be closed in a cold test, the micro-channel air port is opened, and the test can be completed by utilizing the air volume of the micro-channel air port.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. The utility model provides a reduce fuel cell experimental system of torrent, includes the cabin body (1), air intake and inlet scoop (3), its characterized in that have been seted up on the cabin body (1): the utility model discloses a wind channel, including inlet scoop (3), air inlet (3) are connected with wind channel (4), the other end in wind channel (4) and the air intake intercommunication of the cabin body (1), be provided with circulating fan (6) and heat exchanger (7) in wind channel (4), miniflow channel wind gap (13) have been seted up on the cabin body (1), miniflow channel wind gap (13) are relative with the torrent department in the cabin body (1), circulating fan (6) export and miniflow channel wind gap (13) intercommunication.
2. A fuel cell experimental system for reducing turbulence as set forth in claim 1, wherein: and a fresh air inlet (5) is formed at the inlet of the circulating fan (6).
3. A fuel cell experimental system for reducing turbulence as set forth in claim 1, wherein: and a hydrogen discharge port (10) is formed in the outlet of the circulating fan (6).
4. A fuel cell experimental system for reducing turbulence as set forth in claim 1, wherein: and a guide plate (9) is arranged at a corner in the air channel (4) between the outlet of the circulating fan (6) and the air inlet of the cabin body (1).
5. A fuel cell experimental system for reducing turbulence as set forth in claim 1, wherein: a rectifying plate (11) is arranged in an air inlet of the cabin body (1).
6. A fuel cell experimental system for reducing turbulence as set forth in claim 1, wherein: and an air outlet of the air inlet is provided with an air direction adjusting plate (12).
7. A fuel cell experimental system for reducing turbulence as set forth in claim 1, wherein: the bottom in the cabin body (1) is provided with a sample platform (15).
8. A fuel cell experimental system for reducing turbulence as set forth in claim 1, wherein: the heat exchanger (7) is one of a refrigerating heat exchanger and a heating heat exchanger.
9. A turbulence reducing fuel cell test system as claimed in any one of claims 1 to 8, wherein: the top of the cabin body (1) is provided with an inclined top with an inclination larger than 5 degrees, the highest position of the inclined top is provided with a strong exhaust port (2), and a micro-channel air port (13) arranged at the top of the cabin body (1) is communicated with the strong exhaust port (2).
10. A fuel cell experimental system for reducing turbulence as set forth in claim 9, wherein: an explosion-proof fan is arranged in the forced exhaust port (2).
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| CN202122646254.9U CN216524688U (en) | 2021-11-01 | 2021-11-01 | Fuel cell experiment system capable of reducing turbulence |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114001912A (en) * | 2021-11-01 | 2022-02-01 | 上海凌逐新能源科技有限公司 | Fuel cell environment cabin based on wind tunnel principle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114001912A (en) * | 2021-11-01 | 2022-02-01 | 上海凌逐新能源科技有限公司 | Fuel cell environment cabin based on wind tunnel principle |
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