INTEGRATED COMPRESSED GAS TRANSPORT REFRIGERATION UNIT FOR COMPRESSED GAS FUELED VEHICLES

Abstract

A transport refrigeration system comprises a vehicle having a refrigerated cargo space; a compressed gas tank configured to store gas; an engine configured to power the vehicle through combustion of the gas; and a pressure reducing mechanism fluidly connecting the compressed gas tank and the engine. The pressure reducing mechanism configured to reduce the pressure of the gas from the compressed gas tank. The transport refrigeration system also comprises an evaporator thermally coupled to the pressure reducing mechanism and the refrigerated cargo space. The evaporator is configured to cool the refrigerated cargo space. A temperature of the gas and a temperature of the evaporator are reduced as a result of the reduction in pressure of the gas by the pressure reducing mechanism.

Claims

1. A transport refrigeration system comprising: a vehicle having a refrigerated cargo space; a compressed gas tank configured to store gas; an engine configured to power the vehicle through combustion of the gas; a pressure reducing mechanism fluidly connecting the compressed gas tank and the engine, the pressure reducing mechanism configured to reduce the pressure of the gas from the compressed gas tank; an evaporator thermally coupled to the pressure reducing mechanism and the refrigerated cargo space; wherein the evaporator is configured to cool the refrigerated cargo space; and wherein a temperature of the gas and a temperature of the evaporator are reduced as a result of the reduction in pressure of the gas by the pressure reducing mechanism.

2. The transport refrigeration system of claim 1, wherein: the evaporator is fluidly connected to the pressure reducing mechanism and the engine, wherein the gas flows from pressure reducing mechanism through the evaporator and into the engine.

3. The transport refrigeration system of claim 2, wherein: the pressure reducing mechanism is composed of at least one expansion device.

4. The transport refrigeration system of claim 1, wherein: the pressure reducing mechanism is composed of an ejector system, the ejector system comprising an ejector fluidly connected to the compressed gas tank and a flash tank fluidly connected to the evaporator and the engine.

5. The transport refrigeration system of claim 4, wherein: the evaporator includes an evaporator inlet and an evaporator outlet, the flash tank being fluidly connected to the inlet of the evaporator; and the ejector includes an ejector inlet and an ejector outlet, the compressed gas tank and the evaporator outlet being fluidly connected to the ejector inlet, wherein the ejector outlet is fluidly connected to the flash tank.

6. The transport refrigeration system of claim 5, wherein: the flash tank provides liquid gas to the evaporator inlet and vapor gas to the engine.

7. The transport refrigeration system of claim 1, further comprising: a fan configured to operatively pass air across the evaporator and into the refrigerated cargo space.

8. The transport refrigeration system of claim 1, wherein: the gas is natural gas.

9. The transport refrigeration system of claim 1, wherein: the gas is propane.

10. A method of operating a transport refrigeration system, the method comprising: storing gas in a compressed gas tank; powering a vehicle using an engine fluidly connected to the compressed gas tank through a pressure reducing mechanism, the pressure reducing mechanism configured to reduce the pressure of the gas from the compressed gas tank; cooling a refrigerated cargo space using an evaporator thermally coupled to the pressure reducing mechanism and the refrigerated cargo space; and wherein a temperature of the gas and a temperature of the evaporator are reduced as a result of the reduction in pressure of the gas by the pressure reducing mechanism.

11. The method of claim 10, wherein: the evaporator is fluidly connected to the pressure reducing mechanism and the engine, wherein the gas flows from pressure reducing mechanism through the evaporator and into the engine.

12. The method of claim 11, wherein: the pressure reducing mechanism is composed of at least one expansion device.

13. The method of claim 10, wherein: the pressure reducing mechanism is composed of an ejector system, the ejector system comprising an ejector fluidly connected to the compressed gas tank and a flash tank fluidly connected to the evaporator and the engine.

14. The method of claim 13, wherein: the evaporator includes an evaporator inlet and an evaporator outlet, the flash tank being fluidly connected to the inlet of the evaporator; and the ejector includes an ejector inlet and an ejector outlet, the compressed gas tank and the evaporator outlet being fluidly connected to the ejector inlet, wherein the ejector outlet is fluidly connected to the flash tank.

15. The method of claim 14, wherein: the flash tank provides liquid gas to the evaporator inlet and vapor gas to the engine.

16. The method of claim 10, further comprising: operatively passing, using a fan, air across the evaporator and into the refrigerated cargo space.

17. The method of claim 10, wherein: the gas is natural gas.

18. The method of claim 10, wherein: the gas is propane.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0026] The subject matter which is regarded as the disclosure is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features and advantages of the disclosure are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:

[0027] FIG. 1 is a schematic illustration of a transport refrigeration system incorporated on an auto rickshaw or small truck, according to an embodiment of the present disclosure;

[0028] FIG. 2 is an enlarged schematic illustration of the transport refrigeration system of FIG. 1, according to an embodiment of the present disclosure;

[0029] FIG. 3 is a schematic illustration of a transport refrigeration system incorporated on an auto rickshaw or small truck, according to an embodiment of the present disclosure; and

[0030] FIG. 4 is an enlarged schematic illustration of the transport refrigeration system of FIG. 3, according to an embodiment of the present disclosure.

DETAILED DESCRIPTION OF THE DISCLOSURE

[0031] Referring to FIGS. 1-4. FIG. 1 shows a schematic illustration of a transport refrigeration system 200a incorporated on an auto rickshaw 102, according to an embodiment of the present disclosure. FIG. 2 shows an enlarged schematic illustration of the transport refrigeration system 200a of FIG. 1, according to an embodiment of the present disclosure. FIG. 3 shows a schematic illustration of a transport refrigeration system 200b incorporated on an auto rickshaw 102, according to an embodiment of the present disclosure. FIG. 4 shows an enlarged schematic illustration of the transport refrigeration system 200b of FIG. 3, according to an embodiment of the present disclosure.

[0032] The transport refrigeration system 200a of FIGS. 1-2 is being illustrated as a small vehicle refrigeration system 100, as seen in FIG. 1. The small vehicle refrigeration system 100 includes a vehicle 102 having a transport container 106. In an embodiment, the vehicle 102 may be a small truck or an auto rickshaw such as, for example a tuk-tuk. The vehicle 102 includes an operator's compartment or cab 104 and an engine 150 which acts as the drive system of the small vehicle refrigeration system 100. The transport container 106 is coupled to the vehicle 102. The transport container 106 is a refrigerated trailer and includes a top wall 108, a directly opposed bottom wall 110, opposed side walls 112, and a front wall 114, with the front wall 114 being closest to the vehicle 102. The transport container 106 further includes a door or doors 117 at a rear wall 116, opposite the front wall 114. The walls of the transport container 106 define a refrigerated cargo space 119, as shown in FIGS. 1 and 3.

[0033] The gas (i.e. fuel) that powers the engine 150 may be a pressurized gas, for example such as compressed natural gas, propane, or any other pressurized gas known to one of skill in the art. In an embodiment, the gas is compressed natural gas. In another embodiment, the gas is propane. In the illustrated embodiment, the compressed gas to power the engine 150 of the vehicle 102 is stored in a compressed gas tank 220. The engine 150 may be configured to power the vehicle 102 through combustion of the gas.

[0034] Transport refrigeration systems 200a and transport refrigeration systems 200b may be used to transport and distribute perishable goods and environmentally sensitive goods (herein referred to as perishable goods 118). The perishable goods 118 may include but are not limited to fruits, vegetables, grains, beans, nuts, eggs, dairy, seed, flowers, meat, poultry, fish, ice, blood, pharmaceuticals, or any other suitable cargo requiring refrigerated transport. The perishable goods 118 are stored in the refrigerated cargo space 119, as seen in FIGS. 1 and 3.

[0035] The transport refrigeration system 200a of FIGS. 1 and 2 comprises: a compressed gas tank 220; an expansion device 230 fluidly connected to the compressed gas tank 220, an evaporator 240 fluidly connected to the expansion device 230; and an engine 150 fluidly connected to the evaporator 240. The compressed gas tank 220 is configured to store compressed gas. The expansion device 230 is fluidly connected to the compressed gas tank 220 through a tank line 224. The evaporator 240 is fluidly connected to the expansion device 230 at the evaporator inlet 242 through an evaporator line 232. The engine 150 is fluidly connected to the evaporator 240 at the evaporator outlet 244 through engine line 154. In an embodiment, the evaporator 240 is thermally coupled to the expansion device 230 and the refrigerated cargo space 119.

[0036] The gas from the compressed gas tank 220 must then be decompressed to a low pressure to be consumable by the engine 150. For instance, commonly many tanks store compressed natural gas at around 3600 PSI and then the compressed natural gas must be decompressed to less than about 100 PSI for viable use in natural gas engines. The expansion device 230 is configured to depressurize the compressed gas from the compressed gas tank 220 to an operable pressure suitable for consumption by the engine 150. The expansion device 230 may be composed of a single expansion device or a series of multiple expansion devices. Heat is released during the compression process of the gas, while conversely heat is absorbed during the decompression process. So the decompression process through the expansion device 230 will lower the temperature of the gas and subsequently the evaporator 240 temperature as well. Thus, reduced temperature of the evaporator 240 provides cooling to the refrigerated cargo space 119. The cooling may be provided to the refrigerated cargo space 119 through thermal conduction or convection. The transport refrigeration system 200a may include a fan 250 to aid in the convection cooling process. The fan 250 is operative to pass air across the evaporator 240 and cool the refrigerated cargo space 119. The fan 250 may be powered by various methods including but not limited to a battery, a generator, and/or solar panels. The fan may also be spun by a turbine powered by the flow and/or decompression of the gas from the compressed gas tank 220.

[0037] The transport refrigeration system 200b of FIGS. 3-4 is similar to the transport refrigeration system 200a of FIGS. 1-2; however the expansion device 230 of FIGS. 1-2 is replaced by an ejector system 259 in FIGS. 3-4. The transport refrigeration system 200b of FIGS. 3 and 4 comprises: a compressed gas tank 220; an ejector 260 fluidly connected to the compressed gas tank 220, a flash tank 270 fluidly connected to the ejector 260, an evaporator 240 fluidly connected to the flash tank 270 and fluidly connected to the ejector 260; and an engine 150 fluidly connected to the flash tank 270. The compressed gas tank 220 is configured to store compressed gas. In an embodiment, the evaporator 240 is thermally coupled to the ejector system 259 and the refrigerated cargo space 119.

[0038] The ejector 260 includes an ejector inlet 264 and an ejector outlet 268. The ejector inlet 264 of the ejector 260 is fluidly connected to the compressed gas tank 220 through a tank line 222. The flash tank 270 is fluidly connected to the ejector outlet 268 of the ejector through an ejector line 262. The evaporator 240 includes an evaporator inlet 242 and an evaporator outlet 244. The evaporator inlet 242 of the evaporator 240 is fluidly connected to the flash tank 270 to the through a liquid line 272. The evaporator outlet 244 of the evaporator 240 is fluidly connected to the ejector inlet 264 of the ejector 260 through the ejector return line 248. The engine 150 is fluidly connected to the flash tank 270 through a vapor engine line 152.

[0039] The ejector system 259 is composed of the ejector 260 and the flash tank 270. Both the expansion device 230 and the ejector system 259 serve as a pressure reducing mechanism configured to reduce the pressure of the gas but accomplish the pressure reduction in different ways. The expansion device 230 of FIGS. 1-2 may be a valve or a series of valves that serve to reduce the pressure of the gas. Whereas the ejector 260 of FIGS. 3-4 reduces the pressure of the compressed gas and separates the gas into a liquid 276 and a vapor 274, both cooled from the decompression process in the ejector. The cooled liquid 276 will travel through the evaporator 240 to cool 240 and thus cool the refrigerated cargo space 119 as well. Once through the evaporator 240 and out the evaporator outlet 244, the liquid 276 will re-enter the ejector inlet 262 and travel through the ejector 260 again, as shown in FIGS. 3 and 4. The vapor 274 will travel to the engine 150 to be consumed.

[0040] The decompression process through the ejector 260 will lower the temperature of the gas and subsequently the evaporator 240 temperature as well. Thus, a reduced temperature of the evaporator 240 provides cooling to the refrigerated cargo space 119. The cooling may be provided to the refrigerated cargo space 119 through thermal conduction or convection. The transport refrigeration system 200b may include a fan 250 to aid in the convection cooling process. The fan 250 is operative to pass air across the evaporator 240 and cool the refrigerated cargo space 119. The fan 250 may be powered by various methods including but not limited to a battery, a generator, and/or solar panels. The fan may also be spun by a turbine powered by the flow and/or decompression of the gas from the compressed gas tank 220.

[0041] The transport refrigeration system 200a and the transport refrigeration system 200b may also include a controller (not shown) configured for controlling operation of the transport refrigeration system 200 including, but not limited to, operation of various components of the refrigerant unit 22 to provide and maintain a desired thermal environment within the refrigerated cargo space 119. The controller may also be able to selectively control the release of compressed gas from the compressed gas tank 220. The release of gas may be based on the requirements of the engine 150 and the transport refrigeration system (transport refrigeration system 200a or 200b). The controller may be an electronic controller including a processor and an associated memory comprising computer-executable instructions that, when executed by the processor, cause the processor to perform various operations. The a processor may be but is not limited to a single-processor or multi-processor system of any of a wide array of possible architectures, including field programmable gate array (FPGA), central processing unit (CPU), application specific integrated circuits (ASIC), digital signal processor (DSP) or graphics processing unit (GPU) hardware arranged homogenously or heterogeneously. The memory may be a storage device such as, for example, a random access memory (RAM), read only memory (ROM), or other electronic, optical, magnetic or any other computer readable medium.

[0042] Advantageously, using the decompression process of compressed gas provides cooling to a refrigerated cargo space, while avoiding the complexity and large volumetric requirements of a compressor based refrigeration system.

[0043] While the disclosure has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the disclosure is not limited to such disclosed embodiments. Rather, the disclosure can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the disclosure. Additionally, while various embodiments of the disclosure have been described, it is to be understood that aspects of the disclosure may include only some of the described embodiments. Accordingly, the disclosure is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.