HYBRID REFUELING STATION AND METHOD FOR REFUELING
20220090739 · 2022-03-24
Inventors
- Jerad Allen Stager (Richmond, CA, US)
- Xianming Li (Orefield, PA, US)
- Anthony Ku (Fremont, CA, US)
- Edward Youn (Pacific Grove, CA, US)
Cpc classification
F17C2225/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C7/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/054
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C5/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E60/32
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F17C2270/0139
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/0157
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/0341
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/0393
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2265/065
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2225/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/015
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2265/032
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/043
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0184
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0161
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0178
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F17C5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Provided is a hybrid refueling station, including: a liquefied fuel unit, a gaseous fuel unit, a temperature management system and a dispensing unit. By combining the liquefied fuel unit with the gaseous fuel unit, boil-off fuel from the liquefied fuel unit is recovered into the gaseous fuel unit, which avoids boil-off loss of liquefied fuel. Provided also is a method for refueling in a hybrid refueling station. By using the gaseous fuel unit to perform a refueling operation during start-up of the liquefied fuel unit, the problem in the prior art of a delay during start-up when the liquefied fuel unit is used is overcome.
Claims
1. A hybrid refueling station, comprising: a liquefied fuel unit, which comprises at least one liquefied fuel storage device, a vaporization device and a first gas storage subunit, wherein the liquefied fuel storage device is connected with the first gas storage subunit via the vaporization device, and the first gas storage subunit is used for storing vaporized fuel; a gaseous fuel unit, which comprises at least one gaseous fuel storage device, a pressurization device and a second gas storage subunit, wherein the gaseous fuel storage device is connected with the second gas storage subunit via the pressurization device, and the second gas storage subunit is used for storing pressurized gaseous fuel; a temperature management system, which comprises a gas inlet and a gas outlet, wherein the gas inlet is connected to the liquefied fuel unit and the gaseous fuel unit respectively for adjusting a temperature of gas discharged from the liquefied fuel unit and the gaseous fuel unit; and a dispensing unit, which is connected to the gas outlet of the temperature management system for dispensing gas from the temperature management system, wherein boil-off fuel from the liquefied fuel unit is recovered to the gaseous fuel unit.
2. The hybrid refueling station according to claim 1, wherein boil-off fuel from the liquefied fuel unit is recovered to the gaseous fuel storage device.
3. The hybrid refueling station according to claim 1, wherein the boil-off fuel comprises boil-off fuel from the liquefied fuel storage device and boil-off fuel during a cryopump precooling.
4. The hybrid refueling station according to claim 1, wherein the temperature management system further comprises a heat exchanger inlet and a heat exchanger outlet, wherein the heat exchanger inlet is connected to the liquefied fuel unit, and the heat exchanger outlet is connected to the gaseous fuel unit.
5. The hybrid refueling station according to claim 4, wherein the heat exchanger outlet is connected to the gaseous fuel storage device or the second gas storage subunit.
6. The hybrid refueling station according to claim 1, wherein the liquefied fuel unit further comprises a low-temperature pressurization device, wherein a feeding end of the low-temperature pressurization device is connected to an outlet of the liquefied fuel storage device, and a discharging end of the low-temperature pressurization device is connected to an inlet of the vaporization device.
7. The hybrid refueling station according to claim 6, wherein the low-temperature pressurization device is a cryopump.
8. The hybrid refueling station according to claim 1, wherein the first gas storage subunit and the second gas storage subunit each are independently selected from the group consisting of a cascade storage tubes or a buffer storage tank.
9. The hybrid refueling station according to claim 1, wherein the temperature management system is a refrigeration device; and/or the dispensing unit comprises a refueling nozzle; and/or the pressurization device is a gas compressor or a cryopump; and/or the vaporization device is a vaporizer.
10. The hybrid refueling station according to claim 9, wherein the temperature management system is selected from the group consisting of a tubular heat exchanger, a coil heat exchanger and a plate heat exchanger.
11. A method for refueling by using the hybrid refueling station according to claim 1, comprising the steps of: refueling, during start-up of the liquefied fuel unit, by the gaseous fuel unit and recovering boil-off fuel from the liquefied fuel unit to the gaseous fuel unit, wherein the boil-off fuel from the liquefied fuel unit comprises boil-off fuel from the liquefied fuel storage device and boil-off fuel during a cryopump precooling.
12. The method for refueling according to claim 11, wherein recovering boil-off fuel from the liquefied fuel unit to the gaseous fuel storage device.
13. The method for refueling according to claim 11, wherein the step of refueling by the gaseous fuel unit comprises: performing refueling after subjecting gaseous fuel in the gaseous fuel storage device to pressurization and refrigeration.
14. The method for refueling according to claim 11, wherein the method for refueling further comprises: performing refueling by the gaseous fuel unit or the liquefied fuel unit after start-up of the liquefied fuel unit is finished.
15. The method for refueling according to claim 11, wherein liquefied fuel from the liquefied fuel unit is used to perform refrigeration to the temperature management system.
16. The method for refueling according to claim 11, wherein the fuel is selected from the group consisting of hydrogen, natural gas and propane.
17. The method for refueling according to claim 16, wherein the fuel is hydrogen.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0040] The scope of the present disclosure will be better understood by reading the detailed description of the illustrative embodiments below with reference to the accompanying drawings, in which:
[0041]
[0042]
[0043] and
[0044]
[0045]
[0046]
[0047]
LIST OF REFERENCE NUMBERS
[0048] In
[0049] In
[0050] In
DETAILED DESCRIPTION OF THE EMBODIMENTS
[0051] Technical solutions in embodiments of the present disclosure will be illustrated clearly and completely hereinafter in combination with the accompanying drawings of the embodiments to make the purpose and advantages of the present disclosure more clear. Obviously, embodiments to be described are only some embodiments of the present disclosure, rather than all embodiments of the present disclosure.
[0052] Hence, the detailed description of the embodiments of the present disclosure with reference to the accompanying drawings is not intended for limiting the claimed scope of the present disclosure, but only provides preferred embodiments of the present disclosure. All other embodiments obtained by those ordinary skilled in the art without making any creative effort based on the embodiments of the present disclosure fall into the protection scope of the present disclosure.
[0053] Referring to
[0054] a liquefied fuel unit, which includes a liquefied fuel storage device 9, a low-temperature pressurization device 10, a vaporization device 11 and a first gas storage subunit 12, wherein an outlet of the liquefied fuel storage device 9 is connected to a feeding end of the low-temperature pressurization device 10 and a gaseous fuel storage device 3 respectively, a discharging end of the low-temperature pressurization device 10 being connected to an inlet of the vaporization device 11, an outlet of the vaporization device 11 being connected to a feeding end of the first gas storage subunit 12, and a discharging end of the first gas storage subunit 12 being connected to a gas inlet of a temperature management system 6, wherein the low-temperature pressurization device 10 is a cryopump;
[0055] a gaseous fuel unit, which includes the gaseous fuel storage device 3, a pressurization device 4 and a second gas storage subunit 5, wherein an outlet of the gaseous fuel storage device 3 is connected to a feeding end of the pressurization device 4, a discharging end of the pressurization device 4 being connected to an inlet of the second gas storage subunit 5, and a discharging end of the second gas storage subunit 5 being connected to the gas inlet of the temperature management system 6, wherein the pressurization device 4 is a gas compressor;
[0056] the temperature management system 6, which includes a heat exchanger inlet, a heat exchanger outlet, a gas inlet and a gas outlet, wherein the gas inlet is connected to the first gas storage subunit 12 of the liquefied fuel unit and the second gas storage subunit 5 of the gaseous fuel unit respectively, for adjusting a temperature of gas from the liquefied fuel unit and the gaseous fuel unit; and
[0057] a dispensing unit 7, wherein a gas outlet of the temperature management system 6 is connected to an inlet of the dispensing unit, an outlet of the dispensing unit is connected to a vehicle to be refueled.
[0058] A process for using the hybrid refueling station for refueling is specifically as follows:
[0059] When a vehicle enters the refueling station, the liquefied fuel unit and the gaseous fuel unit in the refueling station start up at the same time; the low-temperature pressurization device 10 starts a refrigeration cycle; the pressurization device 4 pressurizes gas from the gaseous fuel storage device 3; pressurized gas goes through the second gas storage subunit 5 and enters the temperature management system 6 for cooling; cooled gaseous fuel is dispensed to a vehicle by the dispensing unit 7. After precooling of the low-temperature pressurization device 10 is finished, liquefied fuel from the liquefied fuel storage device 9 is pressurized by the low-temperature pressurization device 10 and is vaporized into gaseous fuel by the vaporization device 11, and the gaseous fuel is stored in the first gas storage subunit 12 for use; and meanwhile, boil-off fuel in the refrigeration cycle is recovered to the gaseous fuel storage device 3 as a supplement. After start-up of the liquefied fuel unit is finished, when a vehicle enters the refueling station, dispensing may be carried out by subjecting the gaseous fuel in the second gas storage subunit 5 to heat-exchanging and delivering obtained gaseous fuel to the dispensing unit 7, by subjecting the gaseous fuel in the first gas storage subunit 12 to heat-exchanging and delivering obtained gaseous fuel to the dispensing unit 7, by subjecting the liquefied fuel in the liquefied fuel storage device 9 to low-pressure pressurization, vaporization and heat-exchanging and delivering obtained gaseous fuel to the dispensing unit 7, or by subjecting the gaseous fuel in gaseous fuel storage device 3 to pressurization and heat-exchanging and delivering obtained gaseous fuel to the dispensing unit 7, so as to accomplish back-to-back refueling operations for vehicles. When there is a shortage of fuel storage in the gaseous fuel storage device 3, the fuel may be supplemented by delivery with a tube trailer 1 and on-site electrolysis with an electrolysis+compression device 2, or by vaporization of the liquefied fuel in the liquefied fuel storage device 9.
[0060] The present disclosure will be described in detail through embodiments.
Embodiment 1
[0061] The hybrid refueling station is arranged as above. The discharging end of the low-temperature pressurization device 10 is in communication with the inlet of the vaporization device 11 and the heat exchanger inlet of the temperature management system 6 respectively, and the heat exchanger outlet of the temperature management system 6 is connected to the inlet of the gaseous fuel storage device 3 so as to use low-temperature liquefied fuel to heat-exchange the gaseous fuel. Hydrogen fuel is used in the refueling station, and a total amount of gas refueling is 3000 kg/d, which includes a liquefied fuel supply amount of 2700 kg/d and a gaseous fuel supply amount of 300 kg/d. Data on dispensing cost, capital requirement, boil-off loss of liquefied fuel can be seen in Table 1.
[0062] Design benefits of the hybrid refueling station can be illustrated with detailed techno-economic analysis. The US Department of Energy (DOE) Argonne National Laboratory (ANL) has developed such models that have been accepted as the standard. In particular, the Hydrogen Refueling Station Analysis Model (HRSAM) takes such factors as hydrogen refueling station size, refueling profile, rate of return on capital and manufacturing maturity into consideration and produces equipment layout, capital investment requirement and unit dispensing cost.
[0063]
[0064] Similarly,
Embodiment 2
[0065] The hybrid refueling station is arranged as above. The discharging end of the low-temperature pressurization device 10 is in communication with the inlet of the vaporization device 11 and the heat exchanger inlet of the temperature management system 6 respectively, and the heat exchanger outlet of the temperature management system 6 is connected to the inlet of the second gas storage subunit 5 so as to use low-temperature liquefied fuel to heat-exchange the gaseous fuel.
Comparative Example 1
[0066] A liquefied hydrogen fuel refueling station in the prior art as shown in
Comparative Example 2
[0067] A gaseous hydrogen refueling station in the prior art as shown in
TABLE-US-00001 TABLE 1 Liquefied Gaseous hydrogen fuel hydrogen fuel Hybrid refueling refueling station refueling station station Liquefied 3000 0 2700 hydrogen fuel use, kg/d Gaseous 0 3000 300 hydrogen fuel use, kg/d Total station 3000 3000 3000 capacity, kg/d Dispensing 1.26 2.27 1.61 (2700 kg @ cost, $/kg 1.41 and 300 kg @ 3.36) Capital 3.3 6.9 4.3 (3.3 + 0.97) requirement, $m Boil-off loss 30 + boil-off 0 0 from storage loss from tank, kg/d cryopump precooling
[0068] Industry experience suggests that boil-off loss from the liquefied hydrogen fuel storage tank itself is approx. 1% per day, in addition to any boil-off loss associated with cryopump precooling. Therefore the boil-off loss is at least 30 kg/d for a purely liquefied hydrogen fuel station without boil-off loss mitigation. Additional liquefied hydrogen fuel boil-off loss is generated during start-up of the refueling station, and the exact amount varies depending on the refueling schedule for the refueling station; a refueling station with longer gaps between consecutive refueling events will generate larger quantities of liquefied hydrogen fuel boil-off loss. For LDV applications or refueling stations where vehicles arrive in an unscheduled manner, the refueling station will need to be designed to handle the “worst case” scenario to ensure reliability of service. For a purely gaseous hydrogen fuel refueling station, the unit dispensing cost and the capital investment are both much higher, although there is no boil-off loss of fuel. For a purely liquefied hydrogen fuel refueling station, although the benefit of low capital and operating costs is kept, there is boil-off loss of the liquefied hydrogen fuel.
[0069] According to the present disclosure, by combining the gaseous hydrogen fuel refueling station with the liquefied hydrogen fuel refueling station, any boil-off fuel from a liquefied hydrogen fuel unit, including natural boil-off loss from the storage tank and boil-off loss caused by cryopump precooling, is recovered into the gaseous fuel storage device, which avoids boil-off loss of the liquefied hydrogen fuel. Besides, during start-up of the liquefied hydrogen fuel unit, a gaseous hydrogen unit is instantly used for hydrogen refueling, which avoids a delay during start-up of the liquefied hydrogen fuel unit. In addition, compared with a purely gaseous hydrogen fuel refueling station, the hybrid refueling station according to the present disclosure has a smaller footprint and a lower cost. The result in the table shows that the hybrid refueling station has no boil-off loss with quick startup, back-to-back refueling, and reasonable capital and dispensing costs.
[0070] It should be noted that, the above embodiments are only for explaining the present disclosure, and does not constitute any limitation to the present disclosure. The present disclosure is described with reference to exemplary embodiments, but it should be understood that words used herein are descriptive and explanatory, rather than restrictive. Changes can be made to the present disclosure within the scope of the claims of the present disclosure, and modifications can be made to the present disclosure without departing from the scope and the spirit of the present disclosure. Although specific methods, materials and embodiments of the present disclosure are described herein, it does not mean that the present disclosure is limited to specific embodiments disclosed herein; on the contrary, the present disclosure can be extended to all other methods and applications for the same function.