CRYOGENIC FLUID DELIVERY SYSTEM

CLAIM OF PRIORITY

[0001] This application claims the benefit of U.S. Provisional Application No.

62/489,575, filed April 25, 2017, the contents of which are hereby incorporated by reference.

FIELD OF THE INVENTION

[0002] The present disclosure relates generally to cryogenic fluid delivery systems and, more specifically, to a pressure building cryogenic fluid delivery system.

BACKGROUND

[0003] Cryogenic fluid delivery systems are often used to provide the fluids to use devices as fuel or for other uses. For example, one type of cryogenic fluid delivery system provides liquid natural gas (LNG) as fuel to the engine of an LNG-powered vehicle and must be mounted on the chassis of the vehicle, along with the LNG storage tank.

[0004] Many natural gas fuel systems require high fuel delivery pressures to satisfy the engine's flow requirements. Optimally saturated LNG is not always available at fueling stations. Also, desaturation is caused in high use applications where the fuel is being withdrawn continuously from the vessel and at a high rate. Both of these can lead to low pressure problems resulting in inadequate flow to natural gas engines.

[0005] A need exists for a cryogenic fluid delivery system that addresses the above low pressure issues. SUMMARY

[0006] 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.

[0007] In one aspect, an integrated cryogenic fluid delivery system includes a tank configured to store a supply of cryogenic liquid and a heat exchanger having a main line and a reheat line. A liquid pickup line has an inlet configured to receive cryogenic liquid from the tank and an outlet in fluid communication with an inlet of the main line of the heat exchanger. A trim heater exit tee has an inlet in fluid communication with an outlet of the main line of the heat exchanger, a trim heater outlet and an engine outlet. A trim heater return tee has a primary inlet, a trim heater inlet and a combined stream outlet. A flow restriction device has an inlet in fluid communication with the engine outlet of the trim heater exit tee and an outlet in fluid communication with the primary inlet of the trim heater return tee. A trim heater line has an inlet in fluid communication with the trim heater outlet of the trim heater exit tee and an outlet in fluid communication with an inlet of the reheat line of the heat exchanger. A portion of the trim heater line is positioned within the tank. An outlet of the reheat line of the heat exchanger is in fluid

communication with the trim heater inlet of the trim heater return tee. [0008] In another aspect, a system for delivering cryogenic fluid from a tank includes a heat exchanger having a main line and a reheat line. A liquid pickup line has an inlet configured to receive cryogenic liquid from the tank and an outlet in fluid communication with an inlet of the main line of the heat exchanger. A trim heater exit tee has an inlet in fluid communication with an outlet of the main line of the heat exchanger, a trim heater outlet and an engine outlet. A trim heater return tee has a primary inlet, a trim heater inlet and a combined stream outlet. A flow restriction device has an inlet in fluid communication with the engine outlet of the trim heater exit tee and an outlet in fluid communication with the primary inlet of the trim heater return tee. A trim heater line has an inlet in fluid communication with the trim heater outlet of the trim heater exit tee and an outlet in fluid communication with an inlet of the reheat line of the heat exchanger. A portion of the trim heater line is positioned within the tank. An outlet of the reheat line of the heat exchanger is in fluid communication with the trim heater inlet of the trim heater return tee.

[0009] In another aspect, a method of delivering a cryogenic fluid to a use device includes the steps of storing a cryogenic liquid in a tank, vaporizing cryogenic liquid from the tank in a heat exchanger to provide a cryogenic vapor, directing a first portion of the cryogenic vapor to the use device, directing a second portion of the cryogenic vapor to the tank to warm the stored cryogenic liquid whereby a cooled cryogenic vapor is produced, warming the cooled cryogenic vapor in the heat exchanger to produce a trim heated cryogenic vapor and combining the trim heated cryogenic vapor with the first portion of the cryogenic vapor for delivery to the use device. BRIEF DESCRIPTION OF THE DRAWINGS

[0010] Fig. 1 is a schematic view of an embodiment of the pressure building cryogenic fluid delivery system of the disclosure;

[0011] Fig. 2 is a rear elevational view of the system of Fig. 1 .

DETAILED DESCRIPTION OF EMBODIMENTS

[0012] The embodiments of the system of the disclosure described below provide an integrated delivery system of liquefied natural gas (LNG) from a storage tank to a use device, such as a natural gas powered vehicle engine. It is to be understood that the invention may alternatively be used to deliver or dispense other types of cryogenic fluids.

[0013] Embodiments of the disclosure include a circuit for building tank pressure while product is being withdrawn in order to effectively add enough heat and pressure into the tank to build pressure and solve low pressure issues.

[0014] With reference to Figs. 1 and 2, fuel stored in tank 15 enters the Liquid Pickup Line 1 and passes through the Check Valve 2, Manual Valve 3, Excess Flow Valve 4, and enters the main passage or Main Line 5a of the Heat Exchanger 5 via line 12. The heat exchanger adds heat (Q1 ) to and vaporizes the natural gas via hot engine coolant flowing through its shell and making contact with the tubes carrying the LNG.

[0015] As examples only, the heat exchanger 5 may be configured as described U.S. Patent No. 9,829,156 or U.S. Patent Application No. 15/924,779, both to Chart Inc., the contents of both of which are hereby incorporated by reference, a shell and tube heat exchanger or other heat exchanger known in the art. [0016] The flow of natural gas vapor exiting the Heat Exchanger splits with a portion continuing to the engine (indicated in phantom at 13 in Fig. 1 ) and the remainder diverted back so as to travel through the tank via the Tank Heater Line 7. As a result, the Tank Heater Line 7 delivers Heat (Q2) into the tank 15, causing an increase in internal tank pressure.

[0017] The flow back into the Tank Heater Line is made possible by a flow

restriction device, such as Orifice 6, which causes a differential pressure between the Exit Tee 10 and Return Tee 1 1 of the Tank Heater Line 7. The pressure build rate can be manipulated by increasing or decreasing the size of the orifice, that is, reducing the size of the orifice will cause more flow to be directed into the Tank Heater Line thus causing a higher pressure build rate. Alternatively, using a larger orifice will allow more flow to be directed to the engine, thus reducing amount of flow into the Tank Heater Line and, in turn, decrease pressure build rate. An orifice is used herein to control the pressure build rate, however ones skilled in the art know that the flow can also be manipulated via a needle valve, regulator, check valve or any other flow restriction device known in the art, all of which the invention encompasses. As another alternative, which the invention encompasses, the piping or lines downstream of the Exit Tee 10 may include diameters, bends and/or lengths that create a pressure building system to serve as the flow restriction device so that an orifice, needle valve, regulator, check valve or other dedicated component is not required.

[0018] The gas within Tank Heater Line 7 will typically be cold upon exiting from inside the tank, and thus the cooled gas can be routed back, via line 14, into a second pass Reheat Line 5b of the Heat Exchanger 5 in order to warm it back up for engine delivery. After exiting the Reheat Line 5b, the gas will mix back in with the fuel delivery gas at the Return Tee 1 1 , and go through the Automatic Valve 8 and then to the engine 13.

[0019] The Liquid Pickup Line 1 may be provided with an economizer circuit, as disclosed in Chart Inc. U.S. Patent No. 9,829,156. When so equipped, the system of Figs. 1 and 2 is prevented from over-pressurizing the tank 15 by an "Economizer" or "Auto-Refrigeration" valve of the economizer circuit opening once the pressure within the tank gets to the valve set-point. When the economizer circuit valve is open, heat- laden vapor is removed from the tank, via the economizer circuit and the liquid pickup line 1 , and is delivered from the system to the engine, thus keeping a steady internal tank pressure. The present system may also have the same pressure relief, fill, level control, vent, and cold fuel detection devices of Chart Inc. U.S. Patent No. 9,829,156.

[0020] Although a coolant-warmed heat exchanger is described here, ambient vaporizers, electric heaters, or other suitable heat exchangers could be used.

Furthermore, whilst the system is described using LNG, the invention could be used for any other cryogenic system as well that has to have pressure being built during product delivery in order to solve the low pressure issues described above.

[0021] Cryogenic fluid delivery systems must often be installed in environments that have considerable space limitations. For example, the components of a system for providing liquid natural gas (LNG) to the engine of an LNG-powered vehicle must be mounted on the chassis of the vehicle, along with the LNG storage tank. As a result, as illustrated in Fig. 2, it is desirable to integrate all of the components of the system into one assembly. The assembly of components may be positioned within in a shroud 16 which may be attached to an end wall or head of the tank containing the LNG, as taught in Chart Inc. U.S. Patent No. 9,829,156.

[0022] 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.