The present disclosure relates generally to cryogenic fluid transfer systems and, more specifically, to a lossless or nearly lossless, closed-loop cryogenic fluid transfer system and method that incorporates a compressor.
Typically, cryogenic fluids are stored in pressure vessels so that, as the vessels are heated, the warmed and partly vaporized cryogenic fluids therein pressurize the containers without loss of product. There are situations and applications, however, where one would desire to transfer all or a portion of the cryogenic fluid from one pressure vessel to another. Examples include filling portable cryogenic cylinders from a bulk cryogenic tank, filling a vehicle-mounted liquefied natural gas (LNG) fuel tank from a fuel station bulk tank, or transferring fluid from a first cylinder to a second cylinder to effect repairs on the first cylinder.
A variety of prior art methods are commonly used for transferring cryogenic fluid from one vessel to another. If the fluid being transferred is relatively inexpensive (such as liquid nitrogen), transfer is usually effected by a “vent fill” method wherein a single hose connects the liquid phase of the dispensing tank to the receiving tank. When the receiving tank's vent is opened to the atmosphere, liquid can then transfer from the dispensing tank to the receiving tank, as the vapor pressure in the headspace of the dispensing tank “pushes” the liquid phase out of the dispensing tank. There is inherent loss in this transfer, however, since the receiving tank must vent vapor to remain at a pressure that is lower than the pressure of the dispensing tank. Automated systems have been designed to minimize these transfer losses by automatically venting the least amount of vapor possible to achieve a fill. An example of such a system is the Lo-Loss Liquid Cylinder Filling System available from Chart Industries, Inc. of Ball Ground, Ga. Systems and methods such as this, however, can only minimize the losses to the minimum allowed by the laws of physics, and usually still incur losses or around 5%.
More expensive fluids (such as liquid argon or LNG) require more sophisticated (and expensive) solutions to effect low- or no-loss transfers. The simplest solution is for the dispensing tank to build and maintain a sufficient head pressure to fill the receiving tank without venting. This can be done with standard pressure building circuits well-known to those in the art including, but not limited to, those that vaporize liquid from the liquid side of the tank using one or more heat exchanger(s) and direct the resulting vapor to the headspace of the tank.
In the case where the dispensing tank is a bulk storage tank, however, it may be cost-prohibitive to construct a large volume high-pressure tank. Furthermore, it is commonly found that the receiving tank (often a portable cylinder) is of a higher working pressure than the bulk storage tank. Cryogenic liquid pumps can be used to transfer liquid from the dispensing tank to the receiving tank in such situations, though the pumps may be quite expensive.
There are several aspects of the present subject matter which may be embodied separately or together in the devices and systems described and claimed below. These aspects may be employed alone or in combination with other aspects of the subject matter described herein, and the description of these aspects together is not intended to preclude the use of these aspects separately or the claiming of such aspects separately or in different combinations as set forth in the claims appended hereto.
In one aspect, a cryogenic fluid transfer system includes a dispensing tank having a dispensing tank headspace, where the dispensing tank is configured to store a supply of cryogenic liquid with the dispensing tank headspace above the supply of cryogenic liquid. A receiving tank has a receiving tank headspace. A compressor has an inlet and an outlet. A compressor inlet line is in fluid communication with the receiving tank headspace and the compressor inlet. A compressor outlet line is in fluid communication with the compressor outlet and the headspace of the dispensing tank. A liquid transfer line is in fluid communication with the dispensing tank and the receiving tank and is configured to transfer cryogenic liquid from the dispensing tank to the receiving tank when the compressor is activated so as to transfer vapor from the headspace of the receiving tank to the headspace of the dispensing tank to create a pressure differential between the dispensing and receiving tanks.
In another aspect, a cryogenic fluid transfer system includes a dispensing tank having a dispensing tank headspace and is configured to store a supply of cryogenic liquid with the dispensing tank headspace above the supply of cryogenic liquid. A receiving tank has a receiving tank headspace. A compressor has an inlet and an outlet. A compressor inlet line is in fluid communication with the receiving tank headspace and the compressor inlet. A compressor outlet line is in fluid communication with the compressor outlet and the headspace of the dispensing tank so that when the compressor is activated, vapor from the headspace of the receiving tank flows to the headspace of the dispensing tank so as to create a pressure differential between the dispensing and receiving tanks. A liquid transfer line is in fluid communication with the dispensing tank and the receiving tank and configured to transfer cryogenic liquid from the dispensing tank to the receiving tank due to the pressure differential between the dispensing and receiving tanks.
In another aspect, a method for transferring a cryogenic liquid from a dispensing tank to a receiving tank includes the steps of withdrawing vapor from a headspace of the receiving tank and delivering it to a headspace of the dispensing tank so that a differential pressure is created between the dispensing and receiving tanks. The liquid side of the dispensing tank is placed in fluid communication with the receiving tank so that cryogenic liquid is driven from the dispensing tank to the receiving tank by the differential pressure.
Embodiments of the disclosure provide a fluid transfer system and method that utilizes a compressor to move vapor from the receiving tank to the dispensing tank, thereby simultaneously decreasing the receiving tank's pressure and increasing the dispensing tank's pressure so that cryogenic liquid may flow freely though a separate connecting line.
A liquid transfer line 13 connects the liquid side or liquid space of the dispensing tank 10 to the liquid side or liquid space of receiving tank 12. It is to be understood that portions of the dispensing and receiving tank interiors may be either vapor or liquid spaces, depending on the liquid levels in the tanks.
A heat exchanger inlet line 14 connects the headspace of receiving tank 12 to the inlet of a heat exchanger 17. A compressor inlet line 15b extends between the outlet of the heat exchanger 17 and the inlet of a compressor 16, while a compressor outlet line 15a extends between the outlet of the compressor 16 and the headspace of dispensing tank 10.
An explanation of how the transfer system of
With tanks 10 and 12 starting at equal pressures, and at least dispensing tank 10 containing a supply of cryogenic liquid 6, compressor 16 is powered on. Compressor 16 creates a differential pressure between the two tanks 10 and 12 by drawing vapor from the headspace 8 of receiving tank 12 through line 14 and warming it in heat exchanger 17. The compressor 16 receives the warmed vapor via line 15b and pushes it via line 15a to the headspace 7 of dispensing tank 10, as indicated by arrow 18. The resulting differential pressure between tanks 10 and 12 causes the cryogenic liquid 6 to flow from dispensing tank 10 to receiving tank 12 through liquid line 13, as indicated by arrow 19. The transfer occurs until the compressor 16 is is turned off or all of the liquid has been removed from dispensing tank 10.
The system of
It should be noted that heat exchanger 17 of
A liquid transfer line 23 connects the liquid side or liquid space of the dispensing tank 20 to the liquid side or liquid space of receiving tank 22. It is to be understood that portions of the dispensing and receiving tank interiors may be either vapor or liquid spaces, depending on the liquid levels in the tanks.
A heat exchanger inlet line 24b connects the headspace of receiving tank 22 to the inlet of a heat exchanger passage 30b. A compressor inlet line 25b extends between the outlet of the passage 30b of the heat exchanger 28 and the inlet of the compressor 26. A compressor outlet line 25a leads from the outlet of the compressor to the inlet of passage 30a of the heat exchanger 28. A heat exchanger outlet line 24a leads from the outlet of heat exchanger passage 30a to the headspace 27 of dispensing tank 20.
The system of
With the exception of the heat exchanger 28, the transfer system of
As with the system of
Additional embodiments of the transfer system of the disclosure may include additional plumbing lines or valving to allow additional user benefits.
One example is a bypass line that is equipped with a valve, indicated at 40 and 42, respectively, in
As another example, with reference to
Valves 42 (
These and other modifications are possible, but do not detract or alter the general concept of this disclosure, which is the closed-loop transfer system utilizing a compressor acting on the vapor flowing between a dispensing and receiving tank.
As an example only, the systems of the disclosure may be used to fill a bulk cryogenic tank from a cryogenic transport trailer. An example of a cryogen in such an application includes, but is not limited to, liquid hydrogen. As another example, the systems of the disclosure may be used to fill liquid hydrogen fuel tanks on vehicles at a liquid hydrogen refueling station.
While the preferred embodiments of the disclosure have been shown and described, it will be apparent to those skilled in the art that changes and modifications may be made therein without departing from the spirit of the disclosure, the scope of which is defined by the following claims.
The present application claims the benefit of and priority to U.S. Provisional Patent Application No. 62/639,311, filed Mar. 6, 2018, the contents of which are hereby incorporated by reference.
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International Search Report and Written Opinion of the European Patent Office for International Application No. PCT/US2019/020908, dated Jun. 18, 2019, 13 pages. |
Number | Date | Country | |
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20190277450 A1 | Sep 2019 | US |
Number | Date | Country | |
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62639311 | Mar 2018 | US |