Compression device and method
12553423 ยท 2026-02-17
Assignee
Inventors
Cpc classification
F04B7/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B15/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B53/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04B15/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B53/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The invention relates to a fluid compression device comprising a compression chamber accommodating a piston that is able to move between first and second ends of the compression chamber, the device comprising a regeneration circuit connecting the first and second ends of the compression chamber and having a regenerator, the supply pipe comprising a set of one or more valves, the device comprising at least one compressed-fluid discharge pipe comprising an upstream end connected to the compression chamber and a downstream end intended to be connected to a receiver of the compressed fluid, the device comprising a bypass pipe comprising an upstream end connected to the regeneration circuit and a downstream end connected to a recovery member, the bypass pipe being configured to draw a fluid fraction during a regeneration phase during which the piston is moved from the second end towards the first end of the compression chamber.
Claims
1. A fluid compression device having a compression chamber accommodating a piston, the fluid compression device comprising: a first end accommodating a first end of the compression chamber; a second end accommodating a second end of the compression chamber, wherein the piston is configured to move in translation between the first and second ends of the compression chamber; a regeneration circuit connecting the first and second ends of the compression chamber and having a regenerator; a supply pipe comprising an upstream end intended to be connected to a source of fluid to be compressed and a downstream end opening into the first end of the compression chamber, the supply pipe comprising a set of one or more valves; at least one compressed-fluid discharge pipe comprising an upstream end connected to the compression chamber and a downstream end intended to be connected to a receiver of the compressed fluid; and a bypass pipe comprising an upstream end connected to the regeneration circuit and a downstream end connected to a recovery member, the bypass pipe being configured to draw a fluid fraction during a regeneration phase during which the piston is moved from the second end towards the first end of the compression chamber.
2. The fluid compression device according to claim 1, wherein the upstream end of the bypass pipe is connected to the regeneration circuit at the second end of the compression chamber and/or at the first end of the compression chamber and/or at the regenerator.
3. The fluid compression device according to claim 1, wherein the bypass pipe comprises a set of one or more valves.
4. The fluid compression device according to claim 3, wherein the set of one or more valves of the bypass pipe is selected from the group consisting of pressure regulation valve, flow rate regulation valve, and combinations thereof.
5. The fluid compression device according to claim 4, the set of one or more valves are controlled as a function of the pressure inside the fluid tank and/or the pressure inside the compression chamber.
6. The fluid compression device according to claim 1, further comprising a liquefied-fluid tank constituting a fluid source connected to the upstream end of the supply pipe, and in that the recovery member comprises said tank.
7. The fluid compression device according to claim 6, wherein the bypass pipe comprises a pressure and/or flow rate regulation valve controlled as a function of the pressure inside the fluid tank and/or the pressure inside the compression chamber.
8. The fluid compression device according to claim 7, wherein the pressure and/or flow rate regulation valve are controlled as a function of the pressure at the second end of the compression chamber.
9. The fluid compression device according to claim 7, wherein the pressure and/or flow rate regulation valve is configured to provide controlled regulation as a function of the pressure differential between the pressure inside the fluid tank and the pressure inside the compression chamber.
10. The fluid compression device according to claim 1, wherein the set of one or more valves of the supply pipe comprises a non-return member, wherein the non-return member is a non-return valve.
11. The fluid compression device according to claim 1, wherein the second end of the device comprises a heating system.
12. The fluid compression device according to claim 1, wherein the first end of the device comprises a cooling or heating system.
13. The fluid compression device according to claim 1, wherein the regenerator comprises a heat exchanger tube, in particular a cylindrical tube, filled with a material configured to store and release the heat and to allow the fluid in the liquid and/or gaseous state to pass.
14. A method for compressing fluid by means of a device according to claim 1, the method comprising the following successive steps: a) admitting a fluid in the liquid state at an initial pressure into the first end of the compression chamber via the supply pipe, b) compressing by movement of the piston towards the first end of the compression chamber and transfer of the fluid from the first end of the compression chamber towards the second end of the compression chamber via the regeneration pipe, the second end of the device being kept at a temperature higher than the temperature of the first end, c) regenerating by movement of the piston towards the second end of the compression chamber and transfer of the fluid from the second end of the compression chamber towards the first end of the compression chamber, wherein the method further includes, during the regeneration step c), a step of bypassing a fluid fraction outside the compression chamber from the second end of the compression chamber towards the first end of the compression chamber.
15. The method according to claim 14, wherein the fluid in the liquid state is admitted into the first end of the compression chamber at an initial pressure from a liquefied-fluid tank constituting the fluid source, and wherein the recovery member is said liquefied-fluid tank such that the fluid fraction is sent towards the liquefied-fluid tank during the bypass step.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Further features and advantages of the invention will become apparent from the description hereinafter of embodiments, which are given by way of illustration but without any limitation, the description being given in relation with the following attached FIGURES:
(2)
DETAILED DESCRIPTION OF THE INVENTION
(3) Throughout the FIGURES, the same references relate to the same elements.
(4) In this detailed description, the following embodiments are examples. Although the description refers to one or more embodiments, this does not mean that the features apply only to a single embodiment. Individual features of different embodiments can also be combined and/or interchanged in order to provide other embodiments.
(5) The fluid compression device 1 illustrated in [
(6) The piston 5 is able to move in translation between the first 3 and second 6 ends of the compression chamber (via any suitable drive system, which is not described for the sake of simplicity).
(7) The device 1 comprises a regeneration pipe 7 connecting the first 3 and second 6 ends of the compression chamber and having a regenerator 17.
(8) The device 1 also comprises a supply pipe 8 having an upstream end intended to be connected to a source 13 of fluid to be compressed and a downstream end opening into the first end 3 of the compression chamber. The source 13 is preferably a cryogenic fluid tank, for example liquefied hydrogen.
(9) The tank 13 preferably contains a cryogenic fluid in a two-phase form and supplies the thermal compression device with liquid, preferably in a state close to saturation, and potentially subcooled. The diagram does not show pressure control members for the tank 13 (pressurization and/or depressurization system), which may be provided in a conventional manner.
(10) The supply pipe 8 comprises a set of one or more valves, in particular a non-return valve 9. The device 1 comprises at least one compressed-fluid discharge pipe 10 comprising an upstream end connected to the compression chamber and a downstream end intended to be connected to a receiver of the compressed fluid. This discharge pipe 10 also comprises a set of one or more valves, for example a non-return valve 11.
(11) For example, the upstream end of the compressed-fluid discharge pipe 10 is connected to the first and/or the second end of the compression chamber.
(12) For example and as illustrated, the device 1 may comprise two discharge outlets (from the hot chamber and from the cold chamber). It is also possible to envisage a discharge at an intermediate temperature between these two ends.
(13) For example, the upstream end of the compressed-fluid discharge pipe 10 is connected to the first end 3 of the compression chamber. This means that the compressed fluid is discharged from the relatively cold end 3 of the device 1. This enables relatively cold compressed fluid to be produced.
(14) The regeneration pipe 7 is preferably separate from the discharge pipe 10. This means that this regeneration pipe 7 connects the two ends 3, 6 of the compression chamber by passing through the regenerator 17 and thus allows only direct transit between these ends during the movements of the piston 5.
(15) The downstream end of the supply pipe 8 is preferably connected directly to the first end 3 of the compression chamber, i.e. without passing through a pre-compression chamber. This means that the fluid to be compressed is injected directly into the compression chamber 3.
(16) Conventionally, the regenerator 17 can comprise a heat exchanger tube, in particular a cylindrical tube, filled with a material configured to store and release the heat and to allow the fluid in the liquid and/or gaseous state to pass. Of course, any other suitable heat exchanger structure can be envisaged.
(17) Operation may be as follows: In a first compression step, the first (cold) end 3 is filled with cold fluid supplied by the tank 13. The second (hot) end 6 is at its minimal volume. The piston 3 is moved from the second end 6 towards the first end 3, forcing the fluid into the regenerator 17. The fluid is heated in the regenerator and optionally in an additional exchanger.
(18) The fluid thus heated enables the ends 3, 6 of the compression chamber to be pressurized (iso-pressure). Once the delivery pressure has been reached, the outlet valve 11 opens. In a subsequent regeneration and injection phase, the piston 5 is moved from the first 3 towards the second 6 end, then forcing the fluid back into the regenerator 17. The fluid cools and enables the pressure inside the compressor to be reduced. Once this pressure is lower than the pressure of the tank 13, the supply valve 9 is opened. Thus, the incoming fluid (coming from the tank 13) and the fluid returning from the regenerator 17 mix together in the cold chamber (first end 3). The liquid level in the supply tank drops, which lowers the pressure inside the tank 13. An internal or external pressurization system can be used to maintain a pressure therein.
(19) According to an advantageous feature, the device 1 further comprises a bypass pipe 12 comprising an upstream end connected to the regeneration circuit 7 and a downstream end connected to a recovery member 13 outside the compression chamber.
(20) This bypass pipe 12 is configured to draw a fluid fraction during the regeneration phase during which the piston 5 is moved from the second 6 towards the first 3 end of the compression chamber to cool and lower the pressure of fluid that had been heated in the preceding phase.
(21) This means that fluid is extracted from the thermal compressor during the regeneration phase. Extracting fluid in this phase means that less fluid is mixed with the supply liquid admitted into the first end 3 of the compression chamber.
(22) Furthermore, since the return fluid flow rate from the second hot end 6 is reduced, the temperature pinch at the cold point of the regenerative exchanger 17 is improved.
(23) This fluid bypass also reduces the quantity of heat returned to the first end 3 of the compression chamber as a result of compression inefficiency.
(24) These two effects result in an increase of the liquid content at the end of the injection phase and therefore an increase in the efficiency of the device 1.
(25) This helps to improve the operating efficiency of the device and can in particular be adapted to the fluid and the operating conditions.
(26) This fluid fraction drawn by the bypass pipe 12 is preferably and optimally extracted at the second end 6 of the compression chamber (hot end). However, this bypass can withdraw the fluid at any point of the return between the second end 6 and the first end 3 (see the three withdrawal points shown by way of example).
(27) The fluid withdrawn by the bypass pipe 12 is therefore relatively hot and at high pressure, close to the delivery pressure of the thermal compressor at the beginning of the regeneration phase. The pressure inside the compressor then drops as the fluid is extracted and a part of the fluid traverses the regenerator 17.
(28) As illustrated, some or all of this fluid extracted from the thermal compressor may be returned to the tank 13, for example to pressurize the latter. This is because the pressure inside the tank tends to drop as a result of the flow rate of the thermal compressor. This both increases the efficiency of the thermal compressor and helps to limit the need to use a storage pressurization system. The reinjection point in the tank 13 may be positioned at any height of the tank 13, for example in the top in the expansion space.
(29) The quantity of fluid withdrawn by the bypass pipe 12 towards the tank 13 to pressurize same may be an optimization and regulation variable of the device 1. For example, if the quantity of fluid bypassed is not enough to pressurize the tank 13, the pressure maintenance system for the tank 13 may be activated. Conversely, if the quantity of fluid bypassed is too high, it is possible to bypass only the quantity of fluid required for pressurization.
(30) The bypass pipe 12 preferably comprises a pressure and/or flow rate regulation valve 14, which is for example controlled. For example, the valve 14 is controlled as a function of the pressure inside the fluid tank 13 and/or the pressure inside the compression chamber, and for example at the second end 6 of the compression chamber.
(31) An active control system for the injection of this extracted fluid can be implemented to control the pressure differences between the thermal compressor (compression chamber) and the tank 13. During the injection phase, the pressure of the tank 13 is greater than the pressure inside the thermal compressor. During the compression and regeneration phases, the pressure of the compressor is greater than the pressure of the tank 13 up to a given point of the regeneration phase. The bypass valve 14 must therefore preferably be opened as a function of the pressure differential between the tank and the thermal compressor.
(32) This enables inefficient energy from the thermal compressor to be used as efficient energy for the tank 13.
(33) A buffer volume may be used on the bypass pipe 12 to smooth the quantity of gas returning into the tank 13.
(34) The compression device 1 may be supplied with gas or liquid. Better compression performance is achieved in the latter case.
(35) The invention is advantageously used to compress liquid hydrogen, but may also relate to a fluid that is chosen from the list comprising He, H2, Ne, CO, Ar, N2, O2, CH4, CO2, NO, Kr, Xe or any mixture of two or more of these chemical species.
(36) While the invention has been described in conjunction with specific embodiments thereof, it is evident that many alternatives, modifications, and variations will be apparent to those skilled in the art in light of the foregoing description. Accordingly, it is intended to embrace all such alternatives, modifications, and variations as fall within the spirit and broad scope of the appended claims. The present invention may suitably comprise, consist or consist essentially of the elements disclosed and may be practiced in the absence of an element not disclosed. Furthermore, if there is language referring to order, such as first and second, it should be understood in an exemplary sense and not in a limiting sense. For example, it can be recognized by those skilled in the art that certain steps can be combined into a single step.
(37) The singular forms a, an and the include plural referents, unless the context clearly dictates otherwise.
(38) Comprising in a claim is an open transitional term which means the subsequently identified claim elements are a nonexclusive listing (i.e., anything else may be additionally included and remain within the scope of comprising). Comprising as used herein may be replaced by the more limited transitional terms consisting essentially of and consisting of unless otherwise indicated herein.
(39) Providing in a claim is defined to mean furnishing, supplying, making available, or preparing something. The step may be performed by any actor in the absence of express language in the claim to the contrary.
(40) Optional or optionally means that the subsequently described event or circumstances may or may not occur. The description includes instances where the event or circumstance occurs and instances where it does not occur.
(41) Ranges may be expressed herein as from about one particular value, and/or to about another particular value. When such a range is expressed, it is to be understood that another embodiment is from the one particular value and/or to the other particular value, along with all combinations within said range.