Method and system for delivering a gaseous fuel into the air intake system of an internal combustion engine

Abstract

A method and system delivers a cryogenically stored fuel in a gaseous state into the air intake system of a gaseous fuelled internal combustion engine. The method involves measuring the pressure in the vapor space of the cryogenic storage vessel, comparing the measured pressure to a required fuel supply pressure and supplying fuel in gaseous state directly from the vapor space of the cryogenic storage vessel to the fuel delivery line that supplies fuel to the engine, when the pressure measured in the vapor space of the cryogenic storage vessel is equal to or higher than the required fuel supply pressure. The method further involves activating a cryogenic pump to deliver fuel to the internal combustion engine from the liquid space of the cryogenic storage vessel when the measured pressure in the vapor space is lower than the required fuel supply pressure.

Claims

1. A method for delivering a fuel in a gaseous state into an air intake system of a gaseous fuelled internal combustion engine, said method comprising: determining a required fuel supply pressure for delivering said fuel into said air intake system according to a required engine intake pressure as a function of an operating condition of said engine; measuring pressure in a vapor space of a storage vessel which stores said fuel; comparing said measured pressure to said required fuel supply pressure, and supplying said fuel in said gaseous state from said vapor space in said storage vessel when said measured pressure is equal to or higher than said required fuel supply pressure, or activating a fuel pump and delivering fuel from a liquid space in said storage vessel when said measured pressure is lower than said required fuel supply pressure.

2. The method of claim 1 wherein determining said required fuel supply pressure further comprises adding a predetermined pressure threshold to said required engine intake pressure.

3. The method of claim 2 further comprising determining said predetermined pressure threshold as a function of said engine operating condition.

4. The method of claim 1 wherein the step of activating said fuel pump comprises supplying hydraulic fluid from a hydraulic pump to a hydraulic drive unit that drives said fuel pump.

5. The method of claim 4 wherein said hydraulic pump is driven by an electric motor operating independently from operation of said internal combustion engine.

6. The method of claim 4 wherein said hydraulic pump is a first one of at least two hydraulic pumps, the method further comprising electrically activating at least one additional hydraulic pump to deliver hydraulic fluid to said hydraulic drive unit when a commanded hydraulic fluid flow rate is higher than that which can be supplied by said first one of at least two hydraulic pumps.

7. The method of claim 1 further comprising increasing the temperature of said fuel by flowing it through a heat exchanger.

8. The method of claim 7 further comprising increasing heat exchange rate in said heat exchanger when said fuel is supplied from said liquid space, compared to when said fuel is supplied from said vapor space.

9. The method of claim 1 wherein said storage vessel is a first one of a plurality of storage vessels each having a respective vapor space and a liquid space, said method further comprising: measuring pressure in said vapor space of each one of said plurality of storage vessels; comparing measured pressure in said vapor space of each one of said plurality of storage vessels with said required fuel supply pressure; supplying said fuel from said vapor space of any one of said plurality of storage vessels in which vapor pressure is higher than said required system fuel supply pressure; or activating said fuel pump and supplying said fuel from one of said plurality of storage vessels when none of said plurality of storage vessels has a vapor pressure higher than said required system fuel supply pressure.

10. The method of claim 9, said method further comprising measuring the amount of fuel in each of said plurality of storage vessels and, when activating said fuel pump, supplying said fuel from one of said plurality of storage vessels that has the most of said fuel.

11. The method of claim 1 wherein said storage vessel is a first one of a plurality of storage vessels each having a respective vapor space and liquid space, and each having a respective fuel pump, said method further comprising: measuring pressure in said vapor space of each one of said plurality of storage vessels; comparing measured pressure in said vapor space of each one of said plurality of storage vessels with said required fuel supply pressure; supplying said fuel from said vapor space of any one of said plurality of storage vessels in which vapor pressure is higher than said required system fuel supply pressure; or selecting and activating one of said fuel pumps and supplying said fuel from an associated one of said plurality of storage vessels when none of said plurality of storage vessels has a vapor pressure higher than said required system fuel supply pressure.

12. The method of claim 11 wherein selecting one of said fuel pumps that is to be activated is determined by operating each one of said fuel pumps in sequential order.

13. The method of claim 11 wherein selecting one of said fuel pumps that is to be activated is determined by measuring the amount of fuel in each one of said plurality of storage vessels and selecting the one of said plurality of fuel pumps that is associated with the storage vessel that has the most of said fuel.

14. The method of claim 11 further comprising increasing the temperature of said fuel by flowing it through a heat exchanger associated with a respective storage vessel from which fuel is supplied to said engine.

15. A system for delivering a fuel in a gaseous state into an air intake system of a gaseous fuelled internal combustion engine, said system comprising: a. a storage vessel for holding said fuel; b. a fuel pump fluidly connected to receive fuel from a liquid space of said storage vessel; c. a liquid supply line in fluid communication with a discharge outlet of said fuel pump for delivering fuel from said discharge outlet of said fuel pump to a delivery line which delivers fuel to said air intake system of said engine; d. a vapor supply line in fluid communication with a vapor space of said storage vessel for delivering fuel in a gaseous state from said vapor space to said delivery line; e. a pressure sensor for measuring vapor pressure in said vapor space of said storage vessel; and f. a controller which receives pressure measurements from said pressure sensor, determines a required fuel supply pressure for delivering said fuel into said air intake system according to a required engine intake pressure as a function of an operating condition of said engine and compares said measured pressure to said required fuel supply pressure, wherein said controller commands said fuel pump to operate when said measured pressure is lower than said required fuel supply pressure.

16. The system of claim 15 further comprising a heat exchanger placed in said delivery line for increasing the temperature of said fuel being supplied to said engine.

17. The system of claim 15 further comprising a hydraulic pump which supplies hydraulic fluid to a hydraulic drive unit that drives said fuel pump.

18. The system of claim 17 wherein said hydraulic pump is driven by an electric motor operating independently from operation of said engine.

19. The system of claim 17 wherein said hydraulic pump is a first one of at least two hydraulic pumps which can be electrically activated to deliver hydraulic fluid to said hydraulic drive unit that drives said fuel pump.

20. The system of claim 17 wherein said fuel pump is disposed within a cryogenic space of said storage vessel.

21. The system of claim 17 wherein said engine is the prime mover for a vehicle.

22. The system of claim 17 wherein said storage vessel is a first one of a plurality of storage vessels each having a respective vapor space and a liquid space, and being fluidly connected to said fuel pump, and wherein said controller is programmed to activate said fuel pump to supply fuel from said liquid space of one of said plurality of storage vessels when none of said plurality of storage vessels has a vapor pressure higher than said required fuel supply pressure.

23. The system of claim 17 wherein said storage vessel is a first one of a plurality of storage vessels each having a respective vapor space and a liquid space, and each being fluidly connected to a respective fuel pump, and wherein said controller is programmed to select and activate one of said fuel pumps and supply fuel from one of said plurality of storage vessels which is associated with said activated fuel pump when none of said plurality of storage vessels has a vapor pressure higher than said required fuel supply pressure.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is schematic diagram of a system for delivering fuel in gaseous state into the air intake system of an internal combustion engine.

(2) FIG. 2 is a schematic diagram illustrating the basic steps of a method for delivering fuel from a cryogenic storage vessel to the air intake system of a gaseous fuelled internal combustion engine.

(3) FIG. 3 is a representation of a map correlating the engine speed with the throttle position which is used by the system's controller to determine the engine operating condition.

(4) FIG. 4 is schematic diagram of another embodiment of a fuel delivery system comprising two hydraulic pumps for supplying hydraulic fluid to the hydraulic drive unit of the system's fuel pump.

(5) FIG. 5 is a schematic diagram of another embodiment of a fuel delivery system comprising two fuel storage vessels, each storage vessel being associated with a fuel pump, and a controller which activates each of the fuel pumps according to the method described in the present disclosure.

(6) FIG. 6 is a schematic diagram of another embodiment of a fuel delivery system comprising two fuel storage vessels which are both fluidly connected to one external fuel pump and a controller which activates the fuel pump according to the method described in the present disclosure.

DETAILED DESCRIPTION OF ILLUSTRATIVE EMBODIMENT(S)

(7) FIG. 1, schematically illustrates fuel delivery system 100 which is employed to supply a fuel in gaseous state into the air intake system of an internal combustion engine. Engine 110 is an internal combustion engine which is operated by injecting fuel into the engine's air intake manifold or into the air intake port, which is a different method than injecting fuel directly into the engine's combustion chamber. Gaseous fuel is injected into air intake manifold 111 of engine 110 or into air intake ports 113 at pressures that are generally around 70 to 100 psig (pounds per square inch gauge) and can reach around 500 psig. Such pressures are much lower than the operating pressure of a direct injection internal combustion engine where gaseous fuel is injected directly into the combustion chamber at around 4000 psig.

(8) Fuel delivery system 100 comprises fuel storage vessel 112 which stores gaseous fuel in liquefied form at cryogenic temperatures in liquid space 114 within the cryogenic space of the storage vessel. Since heat is transmitted from the surrounding environment to the walls of the storage vessel, liquid fuel stored in the vessel can vaporize and the generated vapor occupies the headspace of the storage vessel, creating vapor space 116.

(9) Liquid space 114 is fluidly connected to fuel pump 118 which can be placed inside the cryogenic space of the storage vessel, as illustrated in FIG. 1, or can be an external pump that communicates through a supply line with the liquid space in the storage vessel. Fuel pump 118 can be activated by starting hydraulic pump 120 which supplies hydraulic fluid from storage vessel 121 through flow switching device 124 to the hydraulic drive unit of fuel pump 118. Hydraulic pump 120 is driven by an electric motor and therefore can operate independently of the operating condition of the engine. In current fuel delivery systems, the hydraulic pump that activates the fuel pump is mechanically actuated by the engine accessory drive and therefore depends on the engine rotation (rpm).

(10) Liquid fuel from liquid space 114 of fuel storage vessel 112 can be pumped by fuel pump 118 through liquid fuel supply line 123 to delivery line 122 which supplies fuel to engine 110. Liquid fuel supply line 123 comprises check valve 125 which prevents, or at least reduces, fuel backflow to storage vessel 112.

(11) Fuel in vapor form can be supplied from vapor space 116 to delivery line 122 through vapor supply line 126 whose one end fluidly communicates with vapor space 116 of storage vessel 112. Vapor supply line 126 is provided with check valve 128 to prevent, or at least reduce, fuel backflow to storage vessel 112.

(12) Liquid fuel line 123 and vapor supply line 126 are each connected to delivery line 122 downstream of their respective check valve. Delivery line 122 further comprises heat exchanger 130 which transmits heat from a heat exchange fluid to the fuel. In some embodiments the heat exchange fluid in heat exchanger 130 is the engine coolant. Delivery line 122 further comprises module 132 for dampening the pressure fluctuations in the stream of fuel being supplied to the engine and pressure regulator 134 for adjusting the pressure of the fuel supplied to the engine to the required engine intake pressure. Automatic fuel shut-off valve 136 is provided on delivery line 122 between pressure regulator 134 and engine 110. Fuel shut-off valve 136 is used as a safety measure for stopping any, or at least substantially any, fuel flow to the engine when the engine is not operating.

(13) The system further comprises controller 140 which commands the operation of fuel pump 118 and hydraulic pump 120 and receives measurement signals from pressure sensors 150 and 152 and from temperature sensor 154. Pressure sensor 150 measures the pressure in vapor space 116 of fuel storage vessel 112 and pressure sensor 152 measures the fuel supply pressure which is the pressure in fuel delivery line 122 downstream of module 132 and upstream of pressure regulator 134. Temperature sensor 154 measures the temperature of the fuel flowing through delivery line 122 downstream of heat exchanger 130 and controller 140 can control the operation of heat exchanger 130 so that the temperature of the fuel supplied to engine 110 is higher than a predetermined limit.

(14) Controller 140 also receives input from the engine regarding the engine speed and another parameters indicative of the engine operating condition. One of the parameters indicative of the fuel demand is the throttle position. The controller can determine the required fuel supply pressure based on the information from a map, which correlates the engine speed data with the other parameters indicative of the engine operating condition.

(15) The method of delivering fuel in a gaseous state into the air intake system of a gaseous fuelled internal combustion engine will now be described in relation to the embodiment of the fuel delivery system illustrated in FIG. 1. The steps of the method are illustrated in FIG. 2. In step 210 of method 200, controller 140 determines the required fuel supply pressure which is the pressure of the fuel flowing through delivery line 122 upstream of pressure regulator 134. At this step, controller 140 receives information from the engine regarding its operating condition and uses the map illustrated in FIG. 3 to determine a point on the map which indicates the current engine operating condition. Map 300 stored in the controller's memory is divided into two regions low flow region 310 and high flow region 320. Low flow region 310 is delimited by boundary line 330 set by a low speed S.sub.L and by boundary line 340 set by a low throttle position T.sub.L. High flow region 320 is delimited by boundary line 350 set by a high engine speed S.sub.H and a high throttle position T.sub.H. If the engine operates for example at a point A, which is characterized by coordinates (S.sub.1, T.sub.1) corresponding to a value S.sub.1 for the engine speed and a value T.sub.1 for the throttle position, it is determined that the engine operates in low flow region 310. Once the point on the map where the engine operates is identified, controller 140 can determine based on predetermined algorithms, the engine intake pressure P.sub.engine A required for operating the engine efficiently. The required fuel supply pressure P.sub.supply A is then determined by the formula P.sub.supply A=P.sub.engine A+P.sub.threshold A, where P.sub.threshold A is the pressure value that is added to the engine intake pressure to obtain the fuel supply pressure. The fuel supply pressure, which is the pressure in fuel delivery line 122 upstream of pressure regulator 134 is higher than the engine intake pressure which is the pressure in fuel delivery line 122 downstream of pressure regulator 134 such that dynamic engine demands can be easily met. Similarly, if the engine operates at point B characterized by coordinates (S.sub.2, T.sub.2), corresponding to a different engine speed S.sub.2 and a different throttle position T.sub.2, located in high flow region 320 on map 300, the controller determines that a different engine intake pressure P.sub.engine B is required for operating the engine efficiently. The required fuel supply pressure is then determined by the same formula: P.sub.supply B=P.sub.engine B+P.sub.threshold B. The value of the pressure threshold that is added to the required engine intake pressure when the engine operates in low flow region 310 is different than the pressure threshold that is added to the required engine intake pressure when the engine operates in high flow region 320. Both the engine intake pressure P.sub.engine and the threshold pressure P.sub.threshold are determined by the controller through control algorithms based on the region on map 300 where the engine operates.

(16) In step 220, pressure P.sub.v within vapor space 116 of fuel storage vessel 112 is measured by pressure sensor 150 and the measured value is communicated to controller 140.

(17) In step 230, the measured pressure P.sub.v in vapor space 116 is compared to the required fuel supply pressure P.sub.supply, which was determined in step 210. If the measured pressure in the vapor space is equal to or higher than the predetermined required fuel supply pressure, fuel is supplied in gaseous state from vapor space 116 in storage vessel 112 through vapor supply line 126 to fuel delivery line 122, which is step 240. If the measured pressure in the vapor space is lower than the predetermined required fuel supply pressure, the controller executes step 250 and activates fuel pump 118 whereby fuel is supplied from liquid space 114 through liquid fuel supply line 123 to fuel delivery line 122.

(18) The temperature of the fuel supplied to fuel delivery line 122 is increased by flowing the fuel through heat exchanger 130. If fuel is supplied from liquid space 114 the heat exchange rate in heat exchanger 130 is increased compared to when the fuel is supplied from vapor space 116 because the temperature of the fuel supplied from the liquid space is slightly lower than the temperature of the fuel supplied in vapor state from the vapor space.

(19) One advantage of the present method over the known methods for delivering fuel in gaseous state to the air intake system of a gaseous fuelled engine is that fuel can be delivered to the engine without relying on the fuel saturation pressure to push the fuel out of the storage vessel.

(20) Other embodiments of fuel delivery system are illustrated in FIGS. 4 to 6. These embodiments have many components that are equivalent to like components of the embodiment presented in FIG. 1 and like components are identified by like reference numbers. In this disclosure like-numbered components function in substantially the same way in each embodiment. Accordingly, if like components have already been described with respect to one embodiment, while identified in the figures for other embodiments, the purpose and function of like components may not be repeated for each of the illustrated embodiments.

(21) FIG. 4 illustrates another embodiment of a fuel delivery system. Fuel delivery system 400 is delivering fuel in gaseous state from cryogenic storage vessel 412 to air intake manifold 411 or to air intake ports 413 of gaseous fuelled internal combustion engine 410. Fuel can be delivered to fuel delivery line 422 either from vapor space 416 through vapor supply line 426 or it is supplied by fuel pump 418 from liquid space 414 through liquid fuel supply line 423. Liquid supply line 423 and vapor supply line 426 are each provided with check valve 425 and respectively 428 for preventing, or at least reducing, fuel backflow. Fuel passing through fuel delivery line 422 is heated in heat exchanger 430 and the pressure fluctuations in the fuel stream are dampened in module 432. Pressure regulator 434 regulates the fuel pressure to the engine intake pressure. Automatic shut-off valve 436 is provided as a safety measure during the times when the engine is not operating. The pressure in fuel delivery line 422 is measured by pressure sensor 452.

(22) System 400 illustrated in FIG. 4 is different than the system illustrated in FIG. 1 in that it uses two hydraulic pumps 420 and 460 for activating fuel pump 418. Hydraulic pumps 420 and 460 supply hydraulic fluid from storage vessel 421 through flow switching unit 424 to the hydraulic drive unit that drives fuel pump 418. In this arrangement, both hydraulic fluid pumps can be used at the same time when the hydraulic fluid flow rate commanded by controller 440 is higher than that which can be supplied by only one hydraulic pump.

(23) In this embodiment heat exchanger 430 is not commanded by controller 440 and provides the same amount of heat to the fuel flowing through delivery line 422 independently of where the fuel is supplied from. The temperature of the fuel flowing through fuel delivery line 422 is measured by temperature sensor 454 and communicated to controller 440.

(24) The method of delivering fuel from storage vessel 412 to engine 410 is the same as the method described in relation to FIG. 2 and therefore it will not be described here in great detail. The pressure in vapor space 416 is measured by pressure sensor 450 and it is compared to the required fuel supply pressure. If the pressure measured in vapor space 416 is equal to or higher than the required fuel supply pressure fuel is supplied in gaseous state from vapor space 416 to the engine, and if the pressure measured in vapor space 416 is lower than the required fuel supply pressure, fuel pump 418 is activated and fuel is delivered by the pump from liquid space 414 to the engine. The required fuel supply pressure is determined following the same algorithm as the one applied for the system illustrated in FIG. 1.

(25) FIG. 5 illustrates another embodiment of the present fuel delivery system. Fuel delivery system 500 is delivering fuel in gaseous state to air intake manifold 511 or to air intake ports 513 of gaseous fuelled internal combustion engine 510. Fuel system 500 is different than the previous embodiments because it comprises two cryogenic storage vessels 512A and 512B, each storage vessel having respective vapor space 516A and 516B, and respective liquid space 514A and 514B, and being fluidly connected to respective fuel pump 518A and 518B.

(26) Each of the two fuel pumps 518A or 518B is activated by supplying hydraulic fluid from hydraulic storage vessel 521 through one of two hydraulic pumps 520 or 560 or through both of them, through flow switching units 562, and further through one of flow switching units 524A or 524B, to the hydraulic drive unit of the respective fuel pump to be activated. Hydraulic fluid pumps 520 and 560 are driven by an electric motor and therefore can be operated independently from the operation of the internal combustion engine.

(27) Similar to the other embodiments described here, pressure in fuel delivery line 522 is measured by pressure sensor 552 upstream of pressure regulator 534 and downstream of module 532. Pressure fluctuations in fuel delivery line 522 are dampened in module 532. Temperature in fuel delivery line 522 is measured by temperature sensor 554. Automatic shut-off valve 536 is provided as a safety measure on fuel delivery line 522 during the times when the engine is not operating.

(28) A similar method of delivering fuel to the engine as described in relation to FIGS. 1 and 4 is applied here. The pressure in the vapor space of each tank 512A and 512B is measured by respective pressure sensor 550A and 550B and communicated to controller 540. Controller 540 compares the pressure measured in each vapor space with the required fuel supply pressure which is determined in a similar way as in the methods described in relation to FIGS. 1 and 4 and fuel is supplied from a vapor space of one of storage vessels 512A or 512B in which vapor pressure is higher than the required fuel supply pressure. Fuel is supplied from the respective vapor space through vapor liquid line 526A or 526B and through heat exchanger 530A or 530B to delivery line 522. When none of two storage vessels has a vapor pressure higher than the required fuel supply pressure, controller 540 selects and activates one of two fuel pumps 518A and 518B to supply fuel from the liquid space of the storage vessel associated with the activated pump. Liquid fuel is supplied through respective liquid supply line 523A or 523B and through heat exchanger 530A or respectively 530B to delivery line 522. Liquid fuel supply lines 523A and 523B and vapor supply lines 526A and 526B are each provided with check valve 525A, 525B and respectively 528A, 528B to prevent, or at least reduce backflow.

(29) In FIG. 5 controller 540 selects which one of the two fuel pumps should be activated such that the two fuel pumps are operated in sequential order. Alternatively, the amount of fuel remaining in each storage vessel 512A and 512B is measured and controller 540 selects one of fuel pumps 518A or 518B based on which storage vessel has the most fuel.

(30) Even though only two storage vessels are shown in the embodiment illustrated in FIG. 5, the system can comprise more than two cryogenic storage vessels and the method of selecting and activating one fuel pump for supplying fuel from a liquid space of one storage vessel will be similar to the method described above.

(31) FIG. 6 illustrates another fuel delivery system 600 for delivering fuel in gaseous state to air intake manifold 611 or to air intake ports 613 of gaseous fuelled internal combustion engine 610. Fuel system 600 is different than the previous embodiments because it comprises one external fuel pump 618 and two cryogenic storage vessels 612A and 612B whereby fuel pump 618 can supply fuel from liquid space 614A or 614B of the respective storage vessels 612A and 612B. Fuel pump 618 is activated when hydraulic pump 620 supplies hydraulic fluid from storage vessel 621 to the hydraulic drive unit of fuel pump 618 through flow switching unit 624.

(32) Similar to the other embodiments described here, pressure in fuel delivery line 622 is measured by pressure sensor 652 upstream of pressure regulator 634 and downstream of module 632. Pressure fluctuations in fuel delivery line 622 are dampened in module 632. Automatic shut-off valve 636 is provided as a safety measure on fuel delivery line 622 during the times when the engine is not operating. Vapor supply lines 626A and 626B are each provided with check valve 628A and 628B respectively and check valve 625 is provided on delivery line 622 downstream of fuel pump 618 to prevent, or at least reduce, fluid backflow.

(33) A similar method of delivering fuel to the engine as described in relation to FIGS. 1, 4 and 5 is applied in FIG. 6. Pressure in vapor spaces 616A and 616B of each storage vessel 612A and respectively 612B is measured by respective pressure sensor 650A and 650B and communicated to controller 640. Controller 640 compares the pressure measured in each vapor space with the required fuel supply pressure which is calculated in a similar way as in the methods described in relation to FIGS. 1, 4 and 5 and fuel is supplied from a vapor space of one of storage vessels 612A or 612B in which vapor pressure is higher than the required fuel supply pressure. Fuel is supplied from the respective vapor space through vapor liquid line 626A or 626B and through heat exchanger 630 to delivery line 622. When none of the two storage vessels has a vapor pressure higher than the required fuel supply pressure, controller 640 activates fuel pump 618 to supply fuel from the liquid space of one of the two storage vessels 612A or 612B. Fuel is supplied from liquid space 614A or 614B through respective liquid supply line 623A or 623B to delivery line 622.

(34) In this embodiment each liquid supply line 623A and 623B is provided with shut-off valve 670A and 670B respectively which can be commanded by controller 640. When none of the two storage vessels has a vapor pressure higher than the required fuel supply pressure, the amount of fuel in each storage vessel is measured and fuel is supplied from the storage vessel which has the most fuel. For example, when it is determined that storage vessel 612A has the most fuel, controller 640 commands shut-off valve 670B to close and fuel pump 618 supplies fuel from liquid space 614A to delivery line 622. Alternatively if it is determined that storage vessel 612B has the most fuel controller 640 commands shut-off valve 670A to close and fuel pump 618 supplies fuel from liquid space 614B to delivery line 622.

(35) The pressure measurements in this embodiment are communicated by pressure sensors 652, 650A and 650B to controller 640 and the temperature of the fuel flowing through delivery line 622 is measured by temperature sensor 654.

(36) In this embodiment, the required fuel supply pressure is determined following the same logic as the one applied for the systems illustrated in FIGS. 1, 4 and 5.

(37) Even though two storage vessels are shown in FIG. 6, the system can comprise more than two cryogenic storage vessels and the method of selecting the liquid space from which fuel is supplied when none of the storage vessels has a vapor space higher than the required fuel supply system is similar to the one described above.

(38) While particular elements, embodiments and applications of the present invention have been shown and described, it will be understood, that the invention is not limited thereto since modifications can be made by those skilled in the art without departing from the scope of the present disclosure, particularly in light of the foregoing teachings.