阅读说明：本技术 能源综合利用系统 (Energy comprehensive utilization system ) 是由 胡松 杨福源 杨明烨 党健 王天泽 *** 李建秋 于 2020-04-21 设计创作，主要内容包括：本申请涉及一种能源综合利用系统。能源综合利用系统包括第一换热器、第二换热器和第三换热器。从冷却液出口出来的温度较高的冷却液在第一换热器内与空气完成换热。空气的温度升高。高温的空气通过第二出口为驾驶室或舱室升温。从第一换热器出来的冷却液继续进入第三换热器。在第三换热器内,冷却液与氢气换热。冷却液的温度继续降低,氢气的温度继续升高。从氢源出来的氢气在第二换热器中与空气完成换热。氢气的温度升高。空气的温度降低。低温的空气用于通过第四出口为驾驶室或舱室降温。能源综合利用系统实现了冷却液、空气和氢气之间能量的调配,进而实现燃料电池汽车内部能量的综合利用。(The application relates to an energy comprehensive utilization system. The energy comprehensive utilization system comprises a first heat exchanger, a second heat exchanger and a third heat exchanger. The cooling liquid with higher temperature from the cooling liquid outlet completes heat exchange with air in the first heat exchanger. The temperature of the air increases. The hot air heats the cab or cabin through the second outlet. And the cooling liquid from the first heat exchanger continues to enter the third heat exchanger. And in the third heat exchanger, the cooling liquid exchanges heat with the hydrogen. The temperature of the coolant continues to decrease and the temperature of the hydrogen gas continues to increase. Hydrogen from the hydrogen source exchanges heat with air in the second heat exchanger. The temperature of the hydrogen gas increases. The temperature of the air decreases. The low temperature air is used to cool the cab or cabin through the fourth outlet. The energy comprehensive utilization system realizes the allocation of energy among cooling liquid, air and hydrogen, and further realizes the comprehensive utilization of the internal energy of the fuel cell automobile.)

1. An energy comprehensive utilization system, comprising:

a first heat exchanger (210) comprising a first inlet (211), a second inlet (212), a first outlet (213) and a second outlet (214), the first inlet (211) being adapted to be connected to a coolant outlet (111) of the fuel cell stack (110), the second inlet (212) being adapted to be connected to a first blower (200), the second outlet (214) being adapted to warm the cabin or compartment (101);

a second heat exchanger (220) comprising a third inlet (221), a fourth inlet (222), a third outlet (223) and a fourth outlet (224), wherein the third inlet (221) is connected with a hydrogen source, the fourth inlet (222) is used for being connected with a second blower (300), and the fourth outlet (224) is used for cooling the cab or cabin (101);

the third heat exchanger (230) comprises a fifth inlet (231), a sixth inlet (232), a fifth outlet (233) and a sixth outlet (234), wherein the fifth inlet (231) is connected with the first outlet (213), the fifth outlet (233) is used for connecting with the hydrogen inlet (114) of the fuel cell stack (110), the sixth inlet (232) is used for connecting with the third outlet (223), and the sixth outlet (234) is used for connecting with the cooling liquid inlet (113) of the fuel cell stack (110).

2. The energy complex utilization system according to claim 1, further comprising:

a first pipe (310), one end of the first pipe (310) is connected with the second outlet (214), and the other end of the first pipe (310) is used for communicating with the cab or cabin (101);

a first heater (320) disposed in the first pipe (310);

an air conditioner evaporator (330) comprising a first air conditioner inlet (331) and a first air conditioner outlet (332), the first air conditioner inlet (331) being connected to the fourth outlet (224), the first air conditioner outlet (332) being connected to the first conduit (310).

3. The energy complex utilization system according to claim 1, further comprising:

a first proportional valve (340) comprising a first valve inlet (341), a first valve outlet (342) and a second valve outlet (343), the first valve inlet (341) for connection with the hydrogen source, the first valve outlet (342) connected with the third inlet (221), the second valve outlet (343) connected between the sixth inlet (232) and the third outlet (223).

4. The integrated energy utilization system according to claim 2, further comprising:

a second pipe (400), one end of the second pipe (400) being connected to the first air conditioner outlet (332), the other end of the second pipe (400) meeting the first pipe (310) at a first junction (401), and the first junction (401) being disposed between the second outlet (214) and the first heater;

a third pipeline (410), wherein one end of the third pipeline (410) is connected with the fourth outlet (224), and the other end of the third pipeline (410) is connected with the first air conditioner inlet (331);

a fourth pipeline (430), one end of the fourth pipeline (430) meeting the first pipeline (310) at a second junction (402), and the other end of the fourth pipeline (430) meeting the third pipeline (410) at a third junction (403);

a first valve (420) disposed in the first pipeline (310), the first valve (420) disposed between the first junction (401) and the second junction (402);

a second valve (440) disposed in the fourth conduit (430);

a seventh valve (570), a valve inlet of the seventh valve (570) and the fourth pipeline (430) meet at a fourth junction (406), the fourth junction (406) is disposed between the third junction (403) and the second valve (440), and a valve outlet of the seventh valve (570) is configured to communicate with the atmosphere;

a fifth valve (530) disposed in the fourth conduit (430), the fifth valve (530) disposed between the second valve (440) and the fourth junction (406).

5. The energy complex utilization system according to claim 4, further comprising:

a third valve (510) disposed in the third pipeline (410), wherein the third valve (510) is disposed between the third junction (403) and the first air conditioner inlet (331);

a fourth valve (520) disposed on the second pipeline (400), wherein the fourth valve (520) is disposed between the first junction (401) and the first air conditioner outlet (332).

6. The energy complex of claim 4, wherein the air conditioner evaporator (330) further comprises a second air conditioner inlet (333) and a second air conditioner outlet (334), the energy complex further comprising:

a fifth pipeline (540), one end of the fifth pipeline (540) is connected to the second air conditioner inlet (333), the other end of the fifth pipeline (540) and the fourth pipeline (430) meet at a fifth junction (404), and the fifth junction (404) is disposed between the second valve (440) and the second junction (402);

a sixth valve (550) disposed in the fifth pipeline (540);

a sixth pipeline (560), one end of the sixth pipeline (560) is connected to the second air conditioner outlet (334), the other end of the sixth pipeline (560) and the fourth pipeline (430) meet at a sixth junction (405), and the sixth junction (405) is disposed between the fourth junction (406) and the second valve (440).

7. The energy complex utilization system according to claim 1, further comprising:

a first heating device (610) for connecting between the fifth outlet (233) and a hydrogen inlet (114) of the fuel cell stack (110).

8. The integrated energy utilization system according to claim 7, further comprising:

an eighth valve (620) for connection between the first heating device (610) and a hydrogen inlet (114) of the fuel cell stack (110).

9. The integrated energy utilization system according to claim 8, further comprising:

a first temperature measuring device (630) connected between the first heating device (610) and the eighth valve (620).

10. The energy complex utilization system according to claim 1, further comprising:

a second heating device (640) for connecting between the sixth outlet (234) and a coolant inlet (113) of the fuel cell stack (110).

11. The integrated energy utilization system according to claim 10, further comprising:

a power plant (650) for connection between the second heating device (640) and the coolant inlet (113) of the fuel cell stack (110).

12. The integrated energy utilization system according to claim 11, further comprising:

and the second temperature measuring device (660) is connected between the power device (650) and the cooling liquid inlet (113) of the fuel cell stack (110).

13. The energy complex utilization system according to claim 1, further comprising:

and the third temperature measuring device (102) is arranged in the cab or the cabin (101).

Technical Field

The application relates to the technical field of new energy, in particular to an energy comprehensive utilization system.

Background

Energy exhaustion and environmental pollution caused by fossil energy consumption are becoming serious, and large-scale development and utilization of renewable energy are imperative. Hydrogen is an effective way of storing energy: the electric energy is converted into chemical energy to be stored in the hydrogen during the power generation peak period of the renewable energy source, and the energy carried by the hydrogen is converted into the electric energy again for use through the fuel cell during the power utilization peak period. The hydrogen fuel cell automobile has the characteristics of zero emission, no pollution and high efficiency, and is a new energy automobile with great potential.

When the hydrogen fuel cell engine is matched with a liquid hydrogen or high-pressure hydrogen system, the liquid hydrogen or the high-pressure hydrogen needs to be decompressed, vaporized or heated to about 50 ℃ before entering the fuel cell stack, and a large amount of heat needs to be absorbed in the process. The fuel cell stack can produce a large amount of waste heat in the course of working, adopt coolant liquid to dispel the heat to the stack usually to make the inside temperature of stack be in efficient operating temperature within range all the time. In order to ensure the power of the fuel cell stack, air entering the stack needs to be pressurized, the air temperature can be raised after the air is compressed by adopting a pressurizing device such as an air blower and the like, and the air is cooled before the compressed air enters the stack, so that the air inlet density can be increased, and the temperature of the air can meet the requirement before the air enters the stack. In addition, in order to ensure the comfort of the driver and passengers in the cab and the cabin, an air conditioning system is needed to keep the temperature in the cab and the cabin within a certain range, the temperature of the air in the cab and the cabin is increased when the weather is cold, and the temperature of the air in the cab or the cabin is decreased when the weather is hot. Therefore, how to realize the comprehensive utilization of the internal energy of the fuel cell automobile is a problem to be solved urgently.

Disclosure of Invention

In view of the above, it is necessary to provide an energy comprehensive utilization system for solving the problem of how to comprehensively utilize the internal energy of a fuel cell vehicle.

An energy comprehensive utilization system comprises a first heat exchanger, a second heat exchanger and a third heat exchanger. The first heat exchanger includes a first inlet, a second inlet, a first outlet, and a second outlet. The first inlet is used for being connected with a cooling liquid outlet of the fuel cell stack. The second inlet is used for being connected with the first air blower. The second outlet is used for heating the cab or the cabin. The second heat exchanger includes a third inlet, a fourth inlet, a third outlet, and a fourth outlet. The third inlet is connected with a hydrogen source. The fourth inlet is for connection with a second blower. The fourth outlet is used for cooling the cab or the cabin.

The third heat exchanger includes a fifth inlet, a sixth inlet, a fifth outlet, and a sixth outlet. The fifth inlet is connected to the first outlet. And the fifth outlet is used for connecting a hydrogen inlet of the fuel cell stack. The sixth inlet is used for being connected with the third outlet. And the sixth outlet is used for being connected with a cooling liquid inlet of the fuel cell stack.

In one embodiment, the energy source comprehensive utilization system further comprises a first pipeline, a first heater and an air conditioner evaporator. One end of the first pipeline is connected with the second outlet. The other end of the first pipeline is used for being communicated with the cab or the cabin. The first heater is arranged on the first pipeline. The air conditioning evaporator includes a first air conditioning inlet and a first air conditioning outlet. The first air conditioner inlet is connected with the fourth outlet. The first air conditioner outlet is connected with the first pipeline.

In one embodiment, the energy complex further comprises a first proportional valve. The first proportional valve includes a first valve inlet, a first valve outlet, and a second valve outlet. The first valve inlet is used for connecting with the hydrogen source. The first valve outlet is connected with the third inlet. The second valve outlet is connected between the sixth inlet and the third outlet.

In one embodiment, the energy comprehensive utilization system further comprises a second pipeline, a third pipeline, a fourth pipeline, a first valve, a second valve, a seventh valve and a fifth valve.

One end of the second pipeline is connected with the first air conditioner outlet. The other end of the second pipeline and the first pipeline are intersected at a first intersection point. And the first junction is disposed between the second outlet and the first heater. One end of the third pipeline is connected with the fourth outlet. The other end of the third pipeline is connected with the first air conditioner inlet.

One end of the fourth pipeline is intersected with the first pipeline at a second intersection point. The other end of the fourth pipeline and the third pipeline are intersected at a third intersection point. The first valve is arranged between the first intersection point and the second intersection point. The second valve is disposed in the fourth line.

A valve inlet of the seventh valve and the fourth pipeline intersect at a fourth intersection point, the fourth intersection point is disposed between the third intersection point and the second valve, and a valve outlet of the seventh valve is used for communicating with an atmospheric environment. The fifth valve is disposed in the fourth pipeline, and the fifth valve is disposed between the second valve and the fourth junction.

In one embodiment, the energy complex further comprises a third valve and a fourth valve. The third valve is arranged on the third pipeline, and the third valve is arranged between the third junction and the first air conditioner inlet. The fourth valve is arranged between the first intersection point and the first air conditioner outlet.

In one embodiment, the air conditioner evaporator further comprises a second air conditioner inlet and a second air conditioner outlet. The energy comprehensive utilization system further comprises a fifth pipeline, a sixth valve and a sixth pipeline.

And one end of the fifth pipeline is connected with the second air conditioner inlet. The other end of the fifth pipeline and the fourth pipeline are intersected at a fifth intersection point. The fifth junction is disposed between the second valve and the second junction.

The sixth valve is disposed in the fifth pipeline. And one end of the sixth pipeline is connected with the second air conditioner outlet. The other end of the sixth pipeline and the fourth pipeline are intersected at a sixth intersection point, and the sixth intersection point is arranged between the fourth intersection point and the second valve.

In one embodiment, the energy source complex utilization system further comprises a first heating device. The first heating device is used for being connected between the fifth outlet and the hydrogen inlet of the fuel cell stack.

In one embodiment, the energy complex further comprises an eighth valve. The eighth valve is used for connecting the first heating device and the hydrogen inlet of the fuel cell stack.

In one embodiment, the energy comprehensive utilization system further comprises a first temperature measuring device. The first temperature measuring device is connected between the first heating device and the eighth valve.

In one embodiment, the energy source complex utilization system further comprises a second heating device. The second heating device is used for being connected between the sixth outlet and a cooling liquid inlet of the fuel cell stack.

In one embodiment, the energy source complex utilization system further comprises a power plant. And the power device is used for being connected between the second heating device and a cooling liquid inlet of the fuel cell stack.

In one embodiment, the energy comprehensive utilization system further comprises a second temperature measuring device. And the second temperature measuring device is used for being connected between the power device and a cooling liquid inlet of the fuel cell stack.

In one embodiment, the energy comprehensive utilization system further comprises a third temperature measuring device. The third temperature measuring device is used for being arranged in the cab or the cabin. The energy comprehensive utilization system that this application embodiment provided includes first heat exchanger, second heat exchanger and third heat exchanger. The first heat exchanger includes a first inlet, a second inlet, a first outlet, and a second outlet. The first inlet is used for being connected with a cooling liquid outlet of the fuel cell stack. The second inlet is used for being connected with the first air blower. The second outlet is used for heating the cab or the cabin. The second heat exchanger includes a third inlet, a fourth inlet, a third outlet, and a fourth outlet. The third inlet is connected with a hydrogen source. The fourth inlet is for connection with a second blower. The fourth outlet is used for cooling the cab or the cabin. The third heat exchanger includes a fifth inlet, a sixth inlet, a fifth outlet, and a sixth outlet. The fifth inlet is connected to the first outlet. And the fifth outlet is used for connecting a hydrogen inlet of the fuel cell stack. The sixth inlet is used for being connected with the third outlet. And the sixth outlet is used for being connected with a cooling liquid inlet of the fuel cell stack.

The energy comprehensive utilization system comprises a first heat exchanger, a second heat exchanger and a third heat exchanger. The cooling liquid with higher temperature from the cooling liquid outlet completes heat exchange with air in the first heat exchanger. The temperature of the cooling fluid decreases. The temperature of the air increases. The high-temperature air heats the cab or the cabin through the second outlet. And the cooling liquid coming out of the first heat exchanger continues to enter the third heat exchanger. And in the third heat exchanger, the cooling liquid exchanges heat with hydrogen. The temperature of the coolant continues to decrease and the temperature of the hydrogen gas continues to increase. And the hydrogen from the hydrogen source exchanges heat with air in the second heat exchanger. The temperature of the hydrogen gas increases. The temperature of the air decreases. The low temperature air is used for cooling the cab or the cabin through the fourth outlet.

The energy comprehensive utilization system realizes the allocation of energy among cooling liquid, air and hydrogen through the first heat exchanger, the second heat exchanger and the third heat exchanger. The comprehensive energy utilization system realizes the heating of hydrogen, the cooling of cooling liquid and the regulation of the temperature of the cab, and further realizes the comprehensive utilization of the internal energy of the fuel cell automobile.

Drawings

In order to more clearly illustrate the technical solutions in the embodiments or the conventional technologies of the present application, the drawings used in the descriptions of the embodiments or the conventional technologies will be briefly introduced below, it is obvious that the drawings in the following descriptions are only some embodiments of the present application, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.

Fig. 1 is a schematic structural diagram of the energy comprehensive utilization system provided in an embodiment of the present application;

fig. 2 is a schematic structural diagram of the energy comprehensive utilization system provided in an embodiment of the present application;

fig. 3 is a schematic structural diagram of the energy comprehensive utilization system provided in an embodiment of the present application;

fig. 4 is a schematic structural diagram of the energy comprehensive utilization system provided in an embodiment of the present application.

Reference numerals:

energy comprehensive utilization system 10

Cab or cabin 101

Fuel cell stack 110

Coolant outlet 111

Cooling fluid inlet 113

Hydrogen inlet 114

First heat exchanger 210

The first inlet 211

Second inlet 212

First outlet 213

Second outlet 214

First blower 200

Second heat exchanger 220

Third inlet 221

Fourth inlet 222

Third outlet 223

Fourth outlet 224

Second blower 300

Third heat exchanger 230

Fifth inlet 231

Sixth inlet 232

Fifth outlet 233

Sixth outlet 234

First pipeline 310

First heater 320

Air conditioner evaporator 330

First air conditioner inlet 331

First air conditioner outlet 332

Second air conditioner inlet 333

Second air conditioner outlet 334

First proportional valve 340

First valve inlet 341

First valve outlet 342

Second valve outlet 343

Second pipeline 400

Third pipeline 410

Fourth pipeline 430

First valve 420

Second valve 440

Third valve 510

Fourth valve 520

Fifth valve 530

Fifth pipeline 540

Sixth valve 550

Sixth pipeline 560

Seventh valve 570

First heating device 610

Eighth valve 620

First temperature measuring device 630

Second heating device 640

Power plant 650

Second temperature measuring device 660

First junction 401

Second junction 402

Third junction 403

Fifth junction 404

Sixth junction 405

Fourth junction 406

Third temperature measuring device 102

Detailed Description

In order to make the aforementioned objects, features and advantages of the present application more comprehensible, embodiments accompanying the present application are described in detail below with reference to the accompanying drawings. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present application. This application is capable of embodiments in many different forms than those described herein and those skilled in the art will be able to make similar modifications without departing from the spirit of the application and it is therefore not intended to be limited to the embodiments disclosed below.

The numbering of the components as such, e.g., "first", "second", etc., is used herein for the purpose of describing the objects only, and does not have any sequential or technical meaning. The term "connected" and "coupled" when used in this application, unless otherwise indicated, includes both direct and indirect connections (couplings). In the description of the present application, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used only for convenience in describing the present application and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be considered as limiting the present application.

In this application, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may be directly contacting the first and second features or indirectly contacting the first and second features through intervening media. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.

Referring to fig. 1, an energy comprehensive utilization system 10 according to an embodiment of the present disclosure includes a first heat exchanger 210, a second heat exchanger 220, and a third heat exchanger 230. The first heat exchanger 210 includes a first inlet 211, a second inlet 212, a first outlet 213, and a second outlet 214. The first inlet 211 is configured to be connected to the coolant outlet 111 of the fuel cell stack 110. The second inlet 212 is adapted to be connected to the first blower 200. The second outlet 214 is used to warm the cabin or cabin 101. The second heat exchanger 220 includes a third inlet 221, a fourth inlet 222, a third outlet 223, and a fourth outlet 224. The third inlet 221 is connected to a hydrogen source. The fourth inlet 222 is adapted to be connected to a second blower 300. The fourth outlet 224 is used to cool the cab or cabin 101.

The third heat exchanger 230 includes a fifth inlet 231, a sixth inlet 232, a fifth outlet 233, and a sixth outlet 234. The fifth inlet 231 is connected to the first outlet 213. The fifth outlet 233 is used for connection of the hydrogen inlet 114 of the fuel cell stack 110. The sixth inlet 232 is adapted to be connected to the third outlet 223. The sixth outlet 234 is used to connect with the coolant inlet 113 of the fuel cell stack 110.

The energy comprehensive utilization system 10 provided by the embodiment of the application comprises a first heat exchanger 210, a second heat exchanger 220 and a third heat exchanger 230. The cooling liquid with higher temperature coming out from the cooling liquid outlet 111 completes heat exchange with air in the first heat exchanger 210. The temperature of the cooling fluid decreases. The temperature of the air increases. The air of high temperature heats the cab or cabin 101 through the second outlet 214. The coolant from the first heat exchanger 210 continues to enter the third heat exchanger 230. In the third heat exchanger 230, the coolant exchanges heat with hydrogen. The temperature of the coolant continues to decrease and the temperature of the hydrogen gas continues to increase. Hydrogen from the hydrogen source exchanges heat with air in the second heat exchanger 220. The temperature of the hydrogen gas increases. The temperature of the air decreases. The cool air is used to cool the cab or cabin 101 through the fourth outlet 224.

When the hydrogen fuel cell engine is matched with a liquid hydrogen or high-pressure hydrogen system, the liquid hydrogen or the high-pressure hydrogen needs to be decompressed, vaporized or heated to about 50 ℃ before entering the fuel cell stack, and a large amount of heat needs to be absorbed in the process. The fuel cell stack can produce a large amount of waste heat in the course of working, adopt coolant liquid to dispel the heat to the stack usually to make the inside temperature of stack be in efficient operating temperature within range all the time. In order to ensure the power of the fuel cell stack, air entering the stack needs to be pressurized, the air temperature can be raised after the air is compressed by adopting a pressurizing device such as an air blower and the like, and the air is cooled before the compressed air enters the stack, so that the air inlet density can be increased, and the temperature of the air can meet the requirement before the air enters the stack. In addition, in order to ensure the comfort of the driver and passengers in the cab and the cabin, an air conditioning system is needed to keep the temperature in the cab and the cabin within a certain range, the temperature of the air in the cab and the cabin is increased when the weather is cold, and the temperature of the air in the cab or the cabin is decreased when the weather is hot.

The energy comprehensive utilization system 10 realizes energy allocation among cooling liquid, air and hydrogen through the first heat exchanger 210, the second heat exchanger 220 and the third heat exchanger 230. The comprehensive energy utilization system realizes the heating of hydrogen, the cooling of cooling liquid and the regulation of the temperature of the cab, and further realizes the comprehensive utilization of the internal energy of the fuel cell automobile.

The fuel cell stack 110 is a device for generating electricity by reacting hydrogen with oxygen in air, and has a cooling pipe inside for dissipating heat from the stack.

The first heat exchanger 210, the second heat exchanger 220, and the third heat exchanger 230 may be of the same type or different types.

In one embodiment, the first heat exchanger 210 and the second heat exchanger 220 are air-cooled heat exchangers. The third heat exchanger 230 is a submerged heat exchanger.

In one embodiment, the temperature of the coolant exiting the first heat exchanger 210 is higher than the temperature of the air in the atmosphere, and the coolant exiting the first heat exchanger 210 enters the third heat exchanger 230. Air enters the first heat exchanger 210 through the first blower 200 to exchange heat with the cooling liquid. The temperature of the air is raised for heating the cabin or cabin 101.

When the cabin or cabin 101 does not require heating, the warmer air from the second outlet 214 is vented to the atmosphere.

The storage device of the hydrogen source comprises a high-pressure hydrogen storage tank or a liquid hydrogen storage tank.

Referring to fig. 2, in one embodiment, the integrated energy utilization system 10 further includes a first pipeline 310, a first heater 320, and an air conditioner evaporator 330. One end of the first pipe 310 is connected to the second outlet 214. The other end of the first conduit 310 is adapted to communicate with the cab or cabin 101. The first heater 320 is disposed in the first pipe 310. The air conditioner evaporator 330 includes a first air conditioner inlet 331 and a first air conditioner outlet 332. The first air conditioner inlet 331 is connected to the fourth outlet 224. The first air conditioner outlet 332 is connected to the first pipe 310.

In one embodiment, the first heater 320 and the air conditioner evaporator 330 are both part of an air conditioning system. The power of the first heater 320 and the air conditioner evaporator 330 may be individually adjusted.

The second heat exchanger 220 is used to assist the air conditioner evaporator 330 in cooling the cab or cabin 101. The first heat exchanger 210 is used to assist the first heater 320 in warming the cab or cabin 101.

In one embodiment, the second heat exchanger 220 and the first heat exchanger 210 are used to provide cooling or heating to the cab or cabin 101 alone. At this time, the first heater 320 or the air conditioner evaporator 330 does not operate.

When the cab or cabin 101 needs to be cooled, the air with lower temperature coming out of the fourth outlet 224 enters the pipeline of the air conditioner evaporator 330 through the first air conditioner inlet 331. The air conditioner evaporator 330 is in an inactive state. The outlet of the air conditioner evaporator 330 communicates with the inlet of the first heater 320. The first heater 320 is shut down. The low temperature air enters the cab or cabin 101 through the outlet of the first heater 320.

When the cabin or cabin 101 does not need to be cooled, the cooler air from the fourth outlet 224 is directed to the atmosphere.

When the low-temperature air obtained by only exchanging heat with the second heat exchanger 220 cannot meet the cooling requirement of the cab or the cabin 101, the air-conditioning evaporator 330 is controlled to work, so that the low-temperature air obtained by exchanging heat with the second heat exchanger 220 is further cooled to meet the cooling requirement of the cab or the cabin 101.

When the temperature of the cab or the cabin 101 needs to be raised, the first heat exchanger 210 exchanges heat to provide heat for the cab or the cabin 101. When the heat of the air at the second outlet 214 of the first heat exchanger 210 cannot meet the heat requirement of the cab or cabin 101, the first heater 320 is operated to further raise the temperature of the warm air obtained by heat exchange of the first heat exchanger 210 so as to meet the heat requirement of the cab or cabin 101.

In addition, the first heater 320 and the air conditioner evaporator 330 can be operated independently to provide heat and cold for the cab or cabin 101 to adjust the temperature of the cab or cabin 101.

Referring also to fig. 3, in one embodiment, the energy source complex utilization system 10 further includes a first proportional valve 340. The first proportional valve 340 includes a first valve inlet 341, a first valve outlet 342, and a second valve outlet 343. The first valve inlet 341 is adapted to be connected to the hydrogen source. The first valve outlet 342 is connected to the third inlet 221. The second valve outlet 343 is connected between the sixth inlet 232 and the third outlet 223.

When the second heat exchanger 220 needs to be shut down, the hydrogen may enter the sixth inlet 232 of the third heat exchanger 230 through the first valve inlet 341, the second valve outlet 343, and the third inlet 221.

In one embodiment, the integrated energy utilization system 10 further includes a second line 400, a third line 410, a fourth line 430, a first valve 420, a second valve 440, a seventh valve 570, and a fifth valve 530.

One end of the second pipe 400 is connected to the first air-conditioning outlet 332. The other end of the second pipeline 400 meets the first pipeline 310 at a first meeting point 401. And the first junction 401 is disposed between the second outlet 214 and the first heater. One end of the third pipeline 410 is connected to the fourth outlet 224. The other end of the third pipe 410 is connected to the first air conditioner inlet 331.

One end of the fourth pipeline 430 meets the first pipeline 310 at a second meeting point 402. The other end of the fourth pipeline 430 meets the third pipeline 410 at a third meeting point 403. The first valve 420 is disposed in the first pipeline 310, and the first valve 420 is disposed between the first junction 401 and the second junction 402. The second valve 440 is disposed in the fourth pipeline 430.

The valve inlet of the seventh valve 570 and the fourth pipeline 430 meet at a fourth junction 406, and the fourth junction 406 is disposed between the third junction 403 and the second valve 440. The valve outlet of the seventh valve 570 is adapted to communicate with the atmosphere. The fifth valve 530 is disposed on the fourth pipeline 430, and the fifth valve 530 is disposed between the second valve 440 and the third junction 403.

In one embodiment, the integrated energy utilization system 10 further includes a third valve 510 and a fourth valve 520. The third valve 510 is disposed on the third pipeline 410, and the third valve 510 is disposed between the third junction 403 and the first air conditioner inlet 331. The fourth valve 520 is disposed on the second pipeline 400, and the fourth valve 520 is disposed between the first junction 401 and the first air conditioner outlet 332.

Referring to fig. 3, when the second heat exchanger 220 needs defrosting, the second blower 300 is turned off. The first blower 200 is turned on. The third valve 510, the first valve 420, and the seventh valve 570 are closed. The second valve 440 and the fifth valve 530 are opened. A hydrogen source enters the sixth inlet 232 through the second valve outlet 343 of the first proportional valve 340. Air in the atmospheric environment is pressurized by the first blower 200 and then heated by the first heat exchanger 210. The heated air enters the second heat exchanger 220 through the second valve 440 and the fifth valve 530 to perform the purging defrosting operation.

Referring also to fig. 4, in one embodiment, the air conditioner evaporator 330 further includes a second air conditioner inlet 333 and a second air conditioner outlet 334. The integrated energy utilization system 10 further includes a fifth pipeline 540, a sixth valve 550, and a sixth pipeline 560.

One end of the fifth pipe 540 is connected to the second air conditioner inlet 333. The other end of the fifth pipeline 540 meets the fourth pipeline 430 at a fifth meeting point 404. The fifth junction 404 is disposed between the second valve 440 and the second junction 402.

The sixth valve 550 is disposed in the fifth pipeline 540. One end of the sixth pipe 560 is connected to the second air conditioner outlet 334. The other end of the sixth pipeline 560 meets the fourth pipeline 430 at a sixth meeting point 405. And the sixth junction 405 is disposed between the fifth valve 530 and the second valve 440.

The energy source comprehensive utilization system 10 has a plurality of operation modes.

Hydrogen source cold energy is used to refrigerate the cab or cabin 101:

the second blower 300 is turned on. The first blower 200 is turned on. The third valve 510, the fourth valve 520, and the second valve 440 are opened. The first valve 420 and the sixth valve 550 are closed. The opening degrees of the fifth valve 530 and the seventh valve 570 are adjusted according to the cooling capacity demand. The first heater 320 is turned off. The first heating means 610 and the second heating means 640 regulate the power according to the requirements. The air conditioning cooling power is adjusted according to the temperature demand of the cabin or cabin 101. The air in the atmospheric environment is pressurized by the second blower 300. Cooled by the second heat exchanger 220. Through the third valve 510 and into the air conditioning evaporator 330. The air conditioning evaporator 330 further cools the air. Through the fourth valve 520. Through the first heater 320 (inactive) and into the cab or cabin 101.

The residual heat of the cooling liquid is used for defrosting of the air conditioner evaporator 330:

the first blower 200 is turned on. The first valve 420, the second valve 440, and the fifth valve 530 are closed. The sixth valve 550 and the seventh valve 570 are opened. The air in the atmosphere is pressurized by the first blower 200. Heated by the first heat exchanger 210. And enters the air-conditioning evaporator 330 through the sixth valve 550 to perform the blowing and defrosting. And then discharged to the atmosphere through the seventh valve 570.

The waste heat of the cooling liquid is used for defrosting of the second heat exchanger 220:

the second blower 300 is turned off. The first blower 200 is turned on. The third valve 510, the first valve 420, the sixth valve 550, and the seventh valve 570 are closed. The second valve 440 and the fifth valve 530 are opened. A hydrogen source enters the sixth inlet 232 through the second valve outlet 343 of the first proportional valve 340. The air in the atmosphere is pressurized by the first blower 200. Heated by the first heat exchanger 210. The second heat exchanger 220 is purged and defrosted by entering through the second valve 440 and the fifth valve 530. And then discharged to the atmosphere via the second blower 300. And after defrosting is finished. The valves resume their pre-defrost state.

The waste heat of the cooling liquid is used for air conditioning heating:

the first blower 200 is turned on. The fourth valve 520, the sixth valve 550, and the second valve 440 are closed. Air in the atmospheric environment is pressurized by the first blower 200 and then heated by the first heat exchanger 210. The heated air enters the cab or cabin 101 through the first valve 420 and the first heater 320. The power of the first heater 320 is adjusted to assist heating according to the required temperature of the cab or cabin 101.

When the refrigerating and heating requirements do not exist, the waste heat of the cooling liquid is used for warming the hydrogen source:

the first blower 200 is turned on. The second blower 300 is turned off. The first valve 420, the sixth valve 550, the seventh valve 570, and the third valve 510 are closed. The second valve 440 and the fifth valve 530 are opened. The proportion of flow into or bypassing the second heat exchanger 220 is regulated by the first proportional valve 340. Air in the atmospheric environment is pressurized by the first blower 200 and then enters the first heat exchanger 210 for heating. The heated air enters the second heat exchanger 220 through the second valve 440 and the fifth valve 530 for heat exchange. The low-temperature air after heat exchange is then discharged to the atmosphere through the second blower 300. After being heated by the second heat exchanger 220, the liquid hydrogen or the high-pressure hydrogen enters the third heat exchanger 230 to exchange heat with the cooling liquid. The hydrogen gas further increases in temperature and then enters the first heating device 610. The first heating means 610 adjusts the heating power according to the hydrogen temperature demand. And then enters the fuel cell stack through the eighth valve 620. The second heat exchanger 220 and the third heat exchanger 230 are divided into two stages to heat and raise the temperature of the hydrogen source.

By adjusting the flow ratio of the first valve outlet 342 and the second valve outlet 343 of the first proportional valve 340, excessive freezing of the cooling liquid in the third heat exchanger 230 on the heat exchange surfaces can be prevented. When excessive ice builds up in the third heat exchanger 230, the hydrogen flow rate at the first valve outlet 342 is increased. When the third heat exchanger 230 is not frozen or the freezing is not severe, the flow rate of the second valve outlet 343 is increased. When the third heat exchanger 230 is not frozen or the freezing is not severe, the first proportional valve 340 may be adjusted such that the hydrogen is completely outputted from the second valve outlet 343. When all hydrogen is output from the second valve outlet 343, the fifth valve 530 is closed, and the seventh valve 570 is opened.

When hydrogen source cold energy is surplus but coolant liquid waste heat is not enough, directly arrange the cold energy to atmospheric environment:

the fifth valve 530 and the seventh valve 570 are opened. The sixth valve 550 and the second valve 440 are closed. The second blower 300 is turned on. Air in the atmospheric environment is pressurized by the second blower 300 and then enters the second heat exchanger 220 for heat exchange. The low-temperature air after heat exchange is directly discharged to the atmosphere through the fifth valve 530 and the seventh valve 570. The third valve 510 adjusts the opening of the solenoid valve according to the refrigeration requirement. In the absence of cooling demand, the third valve 510 is fully closed.

When the cold energy of the hydrogen source is insufficient but the waste heat of the cooling liquid is excessive, the excessive waste heat energy is directly discharged to the atmospheric environment:

the second valve 440 and the seventh valve 570 are opened. The first valve 420 and the sixth valve 550 are closed. The first blower 200 is turned on. Air in the atmospheric environment is pressurized by the first blower 200 and then enters the first heat exchanger 210 for heat exchange. And then directly discharged to the atmosphere through the second valve 440 and the seventh valve 570. The first valve 420 adjusts the opening of the solenoid valve according to the heating requirement. When there is no heating demand, the first valve 420 is completely closed.

In one embodiment, the integrated energy utilization system 10 further includes a first heating device 610. The first heating device 610 is used to be connected between the fifth outlet 233 and the hydrogen inlet 114 of the fuel cell stack 110. The first heating device 610 is used for heating hydrogen.

The energy comprehensive utilization system 10 can not only utilize the cold energy of hydrogen to cool the cab or the cabin 101, but also utilize the heat of the coolant to heat the cab or the cabin 101. The energy comprehensive utilization system 10 utilizes the cold energy of the hydrogen and the heat energy of the cooling liquid to realize the temperature regulation in the cab or the cabin 101. The integrated energy utilization system 10 may also utilize the heat of the cooling fluid to heat and defrost the air conditioner evaporator 330 or the second heater 220. The energy comprehensive utilization system 10 can also realize the adjustment of the temperature of the hydrogen and the cooling liquid through the heat exchange between the hydrogen and the cooling liquid. The energy comprehensive utilization system 10 realizes comprehensive utilization of internal energy of the fuel cell vehicle.

In one embodiment, the integrated energy utilization system 10 further includes an eighth valve 620. The eighth valve 620 is used to connect between the first heating device 610 and the hydrogen inlet 114 of the fuel cell stack 110. The eighth valve 620 is used to regulate the flow into the hydrogen inlet 114.

In one embodiment, the integrated energy utilization system 10 further includes a first temperature measuring device 630. The first temperature measuring device 630 is connected between the first heating device 610 and the eighth valve 620. The first temperature measuring device 630 is used to monitor the temperature of the hydrogen gas entering the hydrogen inlet 114.

In one embodiment, the integrated energy utilization system 10 further includes a second heating device 640. The second heating device 640 is configured to be connected between the sixth outlet 234 and the coolant inlet 113 of the fuel cell stack 110. The second heating device 640 is used for heating the cooling liquid.

In one embodiment, the integrated energy utilization system 10 further includes a power plant 650. The power plant 650 is configured to be connected between the second heating device 640 and the coolant inlet 113 of the fuel cell stack 110. The power plant 650 includes a pump for powering the cooling water circulation.

In one embodiment, the integrated energy utilization system 10 further includes a second temperature measuring device 660. The second temperature measuring device 660 is connected between the power plant 650 and the coolant inlet 113 of the fuel cell stack 110. The second temperature measuring device 660 is used for monitoring the temperature of the coolant entering the coolant inlet 113.

In one embodiment, the integrated energy utilization system 10 further includes a third temperature measuring device 102. The third temperature measuring device 102 is used for being disposed in the cab or the cabin 101, so as to monitor the temperature of the cab or the cabin 101 in real time.

The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.

The above-described examples merely represent several embodiments of the present application and are not to be construed as limiting the scope of the claims. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the concept of the present application, which falls within the scope of protection of the present application. Therefore, the protection scope of the present patent shall be subject to the appended claims.