Patent Application
20230278390
The embodiments herein generally relate to transport refrigeration units and more specifically, using the transport refrigeration units to provide cooling and/or electricity to auxiliary structures.
Refrigerated vehicles and trailers are commonly used to transport perishable goods. A transport refrigeration unit is commonly mounted to the vehicles or to the trailer in operative association with a cargo space defined within the vehicles or trailer for maintaining a controlled temperature environment within the cargo space.
Conventionally, transport refrigeration units used in connection with refrigerated vehicles and refrigerated trailers include a refrigerant compressor, a condenser with one or more associated condenser fans, an expansion device, and an evaporator with one or more associated evaporator fans, which are connected via appropriate refrigerant lines in a closed refrigerant flow circuit. Air or an air/gas mixture is drawn from the interior volume of the cargo space by means of the evaporator fan(s) associated with the evaporator, passed through the airside of the evaporator in heat exchange relationship with refrigerant whereby the refrigerant absorbs heat from the air, thereby cooling the air. The cooled air is then supplied back to the cargo space.
On many commercially available transport refrigeration units the compressor, and typically other components of the transport refrigeration unit, is powered during transit by a prime mover, either through a direct mechanical coupling or a belt drive. Alternatively, the transport refrigeration unit may be electrically powered (e.g., using an alternating (AC) synchronous generator that generates AC power). The generated AC power is typically used to power an electric motor for driving the refrigerant compressor, and other components of the transport refrigeration unit. In a different electrically powered transport refrigeration unit, the AC generator may be replaced with a battery pack and associated power electronics to provide power to the loads.
According to one embodiment, a transport refrigeration system is provided. The transport refrigeration system including: a transport refrigeration unit configured to provide conditioned air to a refrigerated cargo space of a transport container; a power source configured to provide electricity to the transport refrigeration unit, the power source including a fuel cell; an electrical connector electrically connecting the power source to an electrical system of an auxiliary structure; and a power management module configured to provide the electricity from the power source to at least one of the transport refrigeration unit or the electrical system through the electrical connector.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include that the power management module is configured to simultaneously provide the electricity from the power source to both the transport refrigeration unit and the electrical system through the electrical connector.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include that the power management module is configured to provide the electricity from the power source only to the transport refrigeration unit.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include that the power management module is configured to provide the electricity from the power source only to the electrical system through the electrical connector.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include an auxiliary fuel tank not located within the transport refrigeration unit or a trailer system of the transport refrigeration unit, the auxiliary fuel tank being configured to provide fuel to the fuel cell.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include that the auxiliary structure is a building, a vehicle, or another transport refrigeration unit.
According to another embodiment, a transport refrigeration system is provided. The transport refrigeration system including: a transport refrigeration unit configured to generate conditioned air, the transport refrigeration unit including an auxiliary outlet; a preconditioned air hose fluidly connecting the auxiliary outlet to at least one of an auxiliary structure or a climate control system of the auxiliary structure, wherein the transport refrigeration unit is configured to provide the conditioned air to at least one of a refrigerated cargo space of a transport container or the auxiliary outlet.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include an output damper configured to direct the conditioned air to at least one of the refrigerated cargo space or the auxiliary outlet, wherein the transport refrigeration unit is configured to simultaneously provide the conditioned air to both the refrigerated cargo space and the auxiliary outlet using the output damper.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include an output damper configured to direct the conditioned air to at least one of the refrigerated cargo space or the auxiliary outlet, wherein the transport refrigeration unit is configured to only provide the conditioned air to the refrigerated cargo space using the output damper.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include an output damper configured to direct the conditioned air to at least one of the refrigerated cargo space or the auxiliary outlet, wherein the transport refrigeration unit is configured to only provide the conditioned air to the auxiliary outlet using the output damper.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include a power source configured to provide electricity to the transport refrigeration unit, the power source including a fuel cell.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include an auxiliary fuel tank not located within the transport refrigeration unit, the auxiliary fuel tank being configured to provide fuel to the fuel cell.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include that the auxiliary structure is a building, a vehicle, or another transport refrigeration unit.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include that the transport refrigeration unit further includes an auxiliary return inlet, and wherein the transport refrigeration system further includes: a return hose fluidly connecting the auxiliary return inlet to at least one of the auxiliary structure or the climate control system of the auxiliary structure, wherein the transport refrigeration unit is configured to receive return air from at least one of the refrigerated cargo space or the auxiliary return inlet.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include a return damper configured to allow the transport refrigeration unit to receive the return air from at least one of the refrigerated cargo space or the auxiliary return inlet, wherein the transport refrigeration unit is configured to simultaneously receive the return air from the refrigerated cargo space and the auxiliary return inlet using the return damper.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include a return damper configured to allow the transport refrigeration unit to receive the return air from at least one of the refrigerated cargo space or the auxiliary return inlet, wherein the transport refrigeration unit is configured to only receive the return air from the refrigerated cargo space using the return damper.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include a return damper configured to allow the transport refrigeration unit to receive the return air from at least one of the refrigerated cargo space or the auxiliary return inlet, wherein the transport refrigeration unit is configured to only receive the return air from the auxiliary return inlet using the return damper.
According to another embodiment, a method of operating a transport refrigeration system is provided. The method including: generating conditioned air for a refrigerated cargo space of a transport container using a transport refrigeration unit; generating or storing electricity for the transport refrigeration unit using a power source, the power source including a fuel cell; and providing at least one of the electricity to an auxiliary structure or the conditioned air to the auxiliary structure.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include that providing at least one of the electricity to the auxiliary structure or the conditioned air to the auxiliary structure further includes: providing the electricity to the auxiliary structure.
In addition to one or more of the features described above, or as an alternative, further embodiments of may include that providing at least one of the electricity to the auxiliary structure or the conditioned air to the auxiliary structure further includes: providing the conditioned air to the auxiliary structure.
Technical effects of embodiments of the present disclosure include using a transport refrigeration unit to provide power to an auxiliary structure and/or provide conditioned air to the auxiliary structure.
The foregoing features and elements may be combined in various combinations without exclusivity, unless expressly indicated otherwise. These features and elements as well as the operation thereof will become more apparent in light of the following description and the accompanying drawings. It should be understood, however, that the following description and drawings are intended to be illustrative and explanatory in nature and non-limiting.
The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures.
Embodiments disclosed herein relate to using electricity and/or cooling from a transport refrigeration unit to provide power and/or cooling to an auxiliary structure.
Referring now to
Typically, transport refrigeration systems 200 are 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 temperature controlled transport. The transport refrigeration unit 22 is in operative association with the refrigerated cargo space 119 and is configured to provide conditioned air to the transport container 106. The transport refrigeration unit 22 functions, under the control of the controller 600, to establish and regulate a desired environmental parameters, such as, for example temperature, pressure, humidity, carbon dioxide, ethylene, ozone, light exposure, vibration exposure, and other conditions in the refrigerated cargo space 119, as known to one of ordinary skill in the art. In an embodiment, the transport refrigeration unit 22 is capable of providing a desired temperature, carbon dioxide, and humidity range. The refrigerated cargo space 119 may be subdivided into one or more sub-spaces and the transport refrigeration unit 22 may be able to maintain a different temperature in each sub-space.
The transport refrigeration unit 22 is powered by a fuel cell 400 and/or an energy storage device 510. The fuel cell 400, associated fuel tanks 410, and energy storage device 510 may be attached to the trailer system 100. The fuel cell 400, associated fuel tanks 410, and/or energy storage device 510 may be attached to a bottom of the trailer system 100 (or within a housing of the transport refrigeration unit 22).
Referring now to
The refrigerant heat rejection heat exchanger 34 may, for example, comprise one or more refrigerant conveying coiled tubes or one or more tube banks formed of a plurality of refrigerant conveying tubes across flow path to the heat outlet 142. The fan(s) 40 are operative to pass air, typically ambient air, across the tubes of the refrigerant heat rejection heat exchanger 34 to cool refrigerant vapor passing through the tubes. The refrigerant heat rejection heat exchanger 34 may operate either as a refrigerant condenser, such as if the transport refrigeration unit 22 is operating in a subcritical refrigerant cycle or as a refrigerant gas cooler, such as if the transport refrigeration unit 22 is operating in a transcritical cycle.
The refrigerant heat absorption heat exchanger 38 may, for example, also comprise one or more refrigerant conveying coiled tubes or one or more tube banks formed of a plurality of refrigerant conveying tubes extending across flow path from a return air intake 136. The fan(s) 44 are operative to pass air drawn from the refrigerated cargo space 119 across the tubes of the refrigerant heat absorption heat exchanger 38 to heat and evaporate refrigerant liquid passing through the tubes and cool the air. The air cooled in traversing the refrigerant heat absorption heat exchanger 38 is supplied back to the refrigerated cargo space 119 through a refrigeration unit outlet 140. It is to be understood that the term “air” when used herein with reference to the atmosphere within the cargo box includes mixtures of air with other gases, such as for example, but not limited to, nitrogen or carbon dioxide, sometimes introduced into a refrigerated cargo box for transport of perishable produce.
Airflow is circulated into and through the refrigerated cargo space 119 of the transport container 106 by means of the transport refrigeration unit 22. A return air 134 flows into the transport refrigeration unit 22 from the refrigerated cargo space 119 through the transport refrigeration unit return air intake 136, and across the refrigerant heat absorption heat exchanger 38 via the fan 44, thus conditioning the return air 134 to a selected or predetermined temperature. The return air 134, now referred to as conditioned air 138, is supplied into the refrigerated cargo space 119 of the transport container 106 through the transport refrigeration unit outlet 140. Heat 135 is removed from the refrigerant heat rejection heat exchanger 34 through the heat outlet 142. The transport refrigeration unit 22 may contain an external air inlet 144, as shown in
The transport refrigeration system 200 also includes a controller 600 configured for controlling the operation of the transport refrigeration system 200 including, but not limited to, the 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 600 may also be able to selectively operate the electric motor 26. The controller 600 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 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.
The fuel cell 400 may include an anode electrode and a cathode electrode separated by an electrolyte (not shown for simplicity). A reducing fluid such as hydrogen is supplied to the anode electrode, and an oxidant such as oxygen or air is supplied to the cathode electrode. In a cell utilizing a proton exchange membrane (“PEM”) as the electrolyte, the hydrogen electrochemically reacts at a catalyst surface of the anode electrode to produce hydrogen ions and electrons. The electrons are conducted to an external load circuit (e.g., the transport refrigeration unit 22 or energy storage device 510) and then returned to the cathode electrode, while the hydrogen ions transfer through the electrolyte to the cathode electrode, where they react with the oxidant and electrons to produce water and release thermal energy. A fuel tank 410 is configured to store and provide the reducing fluid to the fuel cell 400. In an embodiment, the reducing fluid is hydrogen.
There may be one or more fuel cells 400 and one or more fuel tanks 410. In one embodiment, the fuel cell 400 may be located inside the transport refrigeration unit 22, as shown in
In one embodiment, the energy storage device 510 may be located within the transport refrigeration unit 22, as shown in
The energy storage device 510 may include a battery system 512, a capacitor 514, and/or any other electricity storage system known to one of skill in the art. The battery system 512 may comprise, chemical batteries, lithium-ion batteries, solid state batteries, flow batteries, or any other type of battery known to one of skill in the art. The battery system 512 may employ multiple batteries organized into battery banks. The capacitor 514 may be an electrolytic capacitor, a mica capacitor, a paper capacitor a film capacitor, a non-polarized capacitor, a ceramic capacitor, or any type of capacitor known to one of skill in the art.
The energy storage device 510 may be charged by a stationary charging station 386 such as, for example a three-phase 460 Vac (60 Hz) or 400 Vac (50 Hz) power outlet. The charging station 386 may provide single phase (e.g., level 2 charging capability) or three phase AC power to the energy storage device 510. It is understood that the charging station 386 may have any phase charging and embodiments disclosed herein are not limited to single phase or three phase AC power. In an embodiment, the single phase AC power may be a high voltage DC power, such as, for example, 500 VDC. One function of the charging station 386 is to balance the cell voltage of individual cells of the battery system at some regular cadence.
The transport refrigeration unit 22 has a plurality of electrical power demand loads on the energy storage device 510, including, but not limited to, the electric motor 26 for the compression device 32, the fan motor 42 for the fan 40 associated with the refrigerant heat rejection heat exchanger 34, and the fan motor 46 for the fan 44 associated with the refrigerant heat absorption heat exchanger 38. As each of the fan motors 42, 46 and the electric motor 26 may be an AC motor or a DC motor, it is to be understood that various power converters 52, such as AC to DC rectifiers, DC to AC inverters, AC to AC voltage/frequency converters, DC to DC voltage converters, and filters may be employed in connection with the energy storage device 150 as appropriate. In the depicted embodiment, the heater 48 also constitutes an electrical power demand load. The electric resistance heater 48 may be selectively operated by the controller 600 whenever a control temperature within the temperature controlled cargo box drops below a preset lower temperature limit, which may occur in a cold ambient environment. In such an event the controller 600 would activate the heater 48 to heat air circulated over the heater 48 by the fan(s) 44 associated with the refrigerant heat absorption heat exchanger 38. The heater 48 may also be used to de-ice the return air intake 136. Additionally, the electric motor 26 being used to power the refrigerant compression device 32 constitutes a demand load. The refrigerant compression device 32 may comprise a single-stage or multiple-stage compressor such as, for example, a reciprocating compressor or a scroll compressor. The transport refrigeration system 200 may also include a voltage sensor 28 to sense the voltage coming into the transport refrigeration unit 22.
The power demand loads of the transport refrigeration unit 22 may be managed and fulfilled by an energy management system 300. The energy management system 300 may include the fuel cell 400 and/or the energy storage device 510. The energy management system 300 includes a power management module 310 that is in communication with transport refrigeration unit 22, the fuel cell 400 and/or the one or more supplemental power sources 500.
The power management module 310 is configured to control the electricity provided to transport refrigeration unit 22 from the fuel cell 400 and/or the energy storage device 510.
The power management module 310 may be an electronic controller including a processor 324 and an associated memory 322 comprising computer-executable instructions (i.e., computer program product) that, when executed by the processor 324, cause the processor 324 to perform various operations. The processor 324 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 322 may be but is not limited to a random access memory (RAM), read only memory (ROM), or other electronic, optical, magnetic or any other computer readable medium. While the power management module 310 is being illustrated and described herein as a separate electronic controller the embodiments described herein are applicable to the power management module 310 being incorporated as software within the controller 600 of the transport refrigeration unit 22 or a controller of the fuel cell 400.
In an embodiment, the power management module 310 may be configured to generate electricity using the fuel cell 400 and provide the electricity to an electrical system 710 of an auxiliary structure 700. The auxiliary structure 700 may be a building, a vehicle, a second transport refrigeration unit, or any other structure that may require electricity. In one example, the power management module 310 may be configured to provide electricity to the electrical system 710 of a building in the event of a power outage. In another example, the power management module 310 may be configured to provide electricity to the electrical system 710 of an electric vehicle in the event of the electric vehicle lost power. In yet another example, the power management module 310 may be configured to provide electricity to a second transport refrigeration unit in the event the second transport refrigeration unit lost power on the road and the perishable goods 118 of the second transport refrigeration unit may be in danger of spoilage.
In an embodiment, the power management module 310 may be configured to receive electricity from the electrical system 710 of the auxiliary structure 700. In one example, the power management module 310 may be configured to receive electricity from the electrical system 710 of the building in the event of a power outage of the transport refrigeration unit 22. In another example, the power management module 310 may be configured to receive electricity from the electrical system 710 of an electric vehicle in the event of the transport refrigeration unit lost power. In yet another example, the power management module 310 may be configured to receive electricity from a second transport refrigeration unit in the event the transport refrigeration unit 22 lost power on the road and the perishable goods 118 may be in danger of spoilage.
The power management module 310 may be configured to determine the power needs of the electrical system 710 of the auxiliary structure 700 and operate the fuel cell 400 to fulfil the power needs of the electrical system 710 of the auxiliary structure 700.
A communication system may exist between power management module 310 and an equivalent power management modules within the electrical system 710 of the auxiliary structure 700. When the systems are electrically couple, the loads in electrical system 710 may automatically withdraw power from the energy storage device 510 and/or from the fuel cell 400. There may be communications and power switches as safety mechanisms to ensure there are not ‘outages’ due to over-requirements of power.
The power management module 310 may include various power converters, such as AC to DC rectifiers, DC to AC inverters, AC to AC voltage/frequency converters, DC to DC voltage converters, and filters may be employed, as required, to provide electricity to the electrical system 710 of the auxiliary structure 700. The power management module 310 may be electrically connected to the electrical system 710 using an electrical connector 712. The electrical connector 712 may be an electrical hardwire, a wireless electrical transmission system, or any combination thereof. The power management module 310 may be configured to simultaneously provide electricity to both the transport refrigeration unit 22 and the electrical system 710.
In an embodiment, the transport refrigeration unit 22 may be configured to generate conditioned air 138 using electricity from the fuel cell 400 and provide the conditioned air 138 to an auxiliary structure 700. In one example, the transport refrigeration unit 22 may be configured to provide conditioned air to one or several buildings in the event of a power outage or a loss of cooling capability. In another example, the transport refrigeration unit 22 may be configured to provide conditioned air to one or several vehicles in the event of the vehicle lost power or cooling capability. In yet another example, the transport refrigeration unit 22 may be configured to provide conditioned air to a second transport container in the event a second transport refrigeration unit operably connected to the second transport container lost power or cooling capability on the road and the perishable goods 118 may be in danger of spoilage.
The power management module 310 of the transport refrigeration unit 22 may be configured to determine the cooling needs of the auxiliary structure 700 and instruct the controller 600 to operate the transport refrigeration unit 22 to fulfill the cooling needs of the auxiliary structure 700. The controller 600 may be in wired or wireless communication with a temperature sensor 610 within the auxiliary structure 700 in order to determine the cooling needs of the auxiliary structure 700. The temperature sensor 610 may be a standalone temperature sensor, a temperature sensor of a climate control system 720, or a thermostat of the HVAC system 720. The climate control system 720 may be a heating, ventilation, and air-conditioning (HVAC) system 720 or a refrigeration system.
The transport refrigeration unit 22 may be directly connected to the climate control system 720 of the auxiliary structure 700 or the transport refrigeration unit 22 may be fluidly connected to the auxiliary structure 700 through a window, door, or any other opening of the auxiliary structure 700. The transport refrigeration unit 22 may include an auxiliary outlet 620 configured to receive the conditioned air 138 from the refrigerant heat absorption heat exchanger 38. A preconditioned air hose 622 may operably connect to the auxiliary outlet 620. The preconditioned air hose 622 may fluidly connect the auxiliary outlet 620 to the climate control system 720 and/or the auxiliary structure 700. The preconditioned air hose 622 is configured to deliver the conditioned air 138 from the auxiliary outlet 620 to the climate control system 720 and/or the auxiliary structure 700.
The transport refrigeration unit 22 may include an auxiliary return inlet 640 configured to receive the return air 634 from the climate control system 720 and/or auxiliary structure 700. A return hose 642 may operably connect to the auxiliary return inlet 640. The return hose 642 may fluidly connect the auxiliary return inlet 640 to the climate control system 720 and/or the auxiliary structure 700. The return hose 642 is configured to deliver the return air 634 to the auxiliary outlet 620 from the climate control system 720 and/or the auxiliary structure 700. Alternatively or additionally, the return hose 642 may also be configured to dump the return air 634 from the climate control system 720 and/or the auxiliary structure 700 outside.
The transport refrigeration unit 22 may be configured to simultaneously provide conditioned air 138 to both the transport container 106 and the auxiliary structures or the transport refrigeration unit 22 may be configured to provide conditioned air 138 to only the transport container 106 or the auxiliary structure 700 at any one time.
The transport refrigeration unit 22 may include an output damper 650 to direct the conditioned air 138 to the auxiliary outlet 620 and/or the refrigeration unit outlet 140. The output damper 650 may include a swinging gate 652. The output damper 650 may move the swinging gate 652 to a first position 654 to direct the conditioned air 138 only to the refrigeration unit outlet 140 and block the flow of the conditioned air 138 to the auxiliary outlet 620. The output damper 650 may move the swinging gate 652 to a second position 656 to direct the conditioned air 138 only to the auxiliary outlet 620 and block the flow of the conditioned air 138 to the refrigeration unit outlet 140. The output damper 650 may move the swinging gate 652 to a third position 658 to direct the conditioned air 138 to the auxiliary outlet 620 and the refrigeration unit outlet 140.
The transport refrigeration unit 22 may include a return damper 670 configured to allow the transport refrigeration unit 22 to receive the return air 634 from the auxiliary return inlet 640 and/or the transport refrigeration unit return air intake 136. The return damper 670 may include a swinging gate 672. The return damper 670 may move the swinging gate 672 to a first position 674 to receive the return air 134 from the refrigeration unit outlet 140 and block the return air 634 from the auxiliary return inlet 640. The return damper 670 may move the swinging gate 672 to a second position 676 to receive the return air 634 from the auxiliary return inlet 640 and block the return air 134 from the refrigeration unit outlet 140. The return damper 670 may move the swinging gate 672 to a third position 678 to receive the return air 634 from the auxiliary return inlet 640 and the return air 134 from the refrigeration unit outlet 140.
The fuel cell 400 may also be removably connected to an auxiliary fuel tank 420. The auxiliary fuel tank 420 may be configured to a store and provide a fuel for the fuel cell 400, such as, for example, hydrogen. The auxiliary fuel tank 420 may be separate from the transport refrigeration unit 22, transport refrigeration system 200, and the trailer system 100. The auxiliary fuel tank may not be located within the transport refrigeration unit 22 or the trailer system 100. The auxiliary fuel tank 420 can be exchanged with new auxiliary fuel tanks 420 and/or refilled, once empty or low. The auxiliary fuel tank 420 is essentially a refill fuel tank that may provide the fuel cell 400 with a near endless supply of fuel as it can be continuously switched out. In one example, the auxiliary fuel tank 420 may be a large hydrogen fuel tanker truck that may be parked next to the trailer system 100 and provide the fuel cell 400 with a long lasting source of hydrogen, which advantageously would be beneficial during natural disasters as the transport refrigeration unit 22 may be used as a generator to provide electricity and/or as mobile air-conditioning unit to provide cooling air.
Referring now to
At block 804, electricity for the transport refrigeration unit is generated and/or stored using a power source. At block 806 conditioned air 138 is generated for a refrigerated cargo space 119 of a transport container 106 using a transport refrigeration unit 22.
The power source may be the fuel cell 400 or 420. It is understood that while a fuel cell 400 is mainly described herein, the embodiments disclosed herein may be utilized with other power sources, such as electric batteries, internal combustion engines, hybrid engines, or any combination thereof.
At block 808, at least one of the electricity is provided to an auxiliary structure 700 or the conditioned air 138 is provided to the auxiliary structure 700. In an embodiment, the electricity is provided to the auxiliary structure 700. In another embodiment, the conditioned air 138 is provided to the auxiliary structure 700. In yet another embodiment, both the electricity and the conditioner air 138 are provided to the auxiliary structure 700. In an embodiment, the electricity is provided to the electrical system 710 of the auxiliary structure 700. In another embodiment, the conditioned air 138 is provided to the climate control system 720 of the auxiliary structure 700. In yet another embodiment, both the electricity is provided to the electrical system 710 of the auxiliary structure 700 and the conditioned air 138 is provided to the climate control system 720 of the auxiliary structure 700.
While the above description has described the flow process of
As described above, embodiments can be in the form of processor-implemented processes and devices for practicing those processes, such as processor. Embodiments can also be in the form of computer program code (e.g., computer program product) containing instructions embodied in tangible media (e.g., non-transitory computer readable medium), such as floppy diskettes, CD ROMs, hard drives, or any other non-transitory computer readable medium, wherein, when the computer program code is loaded into and executed by a computer, the computer becomes a device for practicing the embodiments. Embodiments can also be in the form of computer program code, for example, whether stored in a storage medium, loaded into and/or executed by a computer, or transmitted over some transmission medium, such as over electrical wiring or cabling, through fiber optics, or via electromagnetic radiation, wherein, when the computer program code is loaded into and executed by a computer, the computer becomes a device for practicing the exemplary embodiments. When implemented on a general-purpose microprocessor, the computer program code segments configure the microprocessor to create specific logic circuits.
The term “about” is intended to include the degree of error associated with measurement of the particular quantity based upon the equipment available at the time of filing the application. For example, “about” can include a range of ±8% or 5%, or 2% of a given value.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, element components, and/or groups thereof.
While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.
This applications claims the benefit of U.S. Provisional Application No. 63/315,239, filed Mar. 1, 2022, all of which are incorporated herein by reference in their entirety.
| Number | Date | Country | |
|---|---|---|---|
| 63315239 | Mar 2022 | US |
