Heat exchanger
12359875 ยท 2025-07-15
Assignee
Inventors
Cpc classification
Y02P20/133
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
F28D9/0075
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D2021/0033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F2275/205
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C25B1/044
CHEMISTRY; METALLURGY
Y02E60/36
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
F28F2275/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F2265/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2290/44
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J5/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J3/0252
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D9/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F21/083
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F28D9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C25B1/044
CHEMISTRY; METALLURGY
Abstract
A heat exchanger comprises a plurality of cells formed by a stack of alternate planar flow-guide plates (1) and heat transfer plates (2), each heat transfer plate having at least three apertures (3, 4, 6) therethrough, each aperture defining a part of a respective one of at least three fluid flow paths in the heat exchanger. Each flow-guide plate has apertures therethrough corresponding to at least two of the flow paths and a larger aperture (5, 7, 8) therethrough configured to guide fluid in the remaining flow path across the face of the heat transfer plates between which the flow-guide plate is located, each successive flow-guide plate in the stack forming part of a different flow path from the preceding one in the stack.
Claims
1. A cryogenic system for the separation of electrolytically produced oxygen and hydrogen comprising a heat exchanger, the heat exchanger being configured for use in the cryogenic system for the separation of electrolytically produced oxygen and hydrogen, the heat exchanger being configured to exchange heat between a mixed gas stream, hydrogen, and oxygen, the heat exchanger comprising a plurality of cells formed by a stack of alternate planar flow-guide plates and heat transfer plates, each heat transfer plate having at least three apertures therethrough, each aperture defining a part of a respective one of at least three fluid flow paths in the heat exchanger, each flow-guide plate having apertures therethrough corresponding to at least two of the flow paths and a larger aperture therethrough configured to guide fluid in a remaining flow path across a face of the heat transfer plates between which the flow-guide plate is located, each successive flow-guide plate in the stack forming part of a different flow path from a preceding one in the stack.
2. The cryogenic system according to claim 1, wherein the cells in the stack are not equally divided between the three flow paths.
3. The cryogenic system according to claim 1, wherein a direction of flow across the face of the heat transfer plates in each of the flow paths changes along the length of the stack.
4. The cryogenic system according to claim 1, wherein the heat exchanger further comprises a pair of end plates between which the stack of alternate planar flow guide plates and heat transfer plates are clamped by means of tie rods.
5. The cryogenic system according to claim 4, wherein the tie rods are threaded tie rods, and the stack of alternate planar flow-guide plates and heat transfer plates are clamped by means of the threaded tie rods and nuts.
6. The cryogenic system according to claim 4, wherein the heat exchanger further comprises alignment pins extending between the end plates to hold the plates in alignment.
7. The cryogenic system according to claim 4, wherein the end plates have flow connections therethrough.
8. The cryogenic system according to claim 7, wherein the heat exchanger comprises connecting spigots, provided on each end plate for connecting the three flow paths within the heat exchanger to external gas flow pipes.
9. The cryogenic system according to claim 1, wherein the three flow paths comprise one mixed gas stream flow path, one hydrogen flow path, and one oxygen flow path, the mixed gas flow path and the oxygen flow path being longer than the hydrogen flow path.
10. The cryogenic system according to claim 1, comprising a liquid oxygen reservoir connected to the oxygen flow path.
11. The cryogenic system according to claim 1, comprising an electrolyser connected to the mixed gas flow path.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In the drawings, which illustrate embodiments of the invention:
(2)
(3)
(4)
(5)
(6)
DETAILED DESCRIPTION OF THE ILLUSTRATED EMBODIMENT
(7) Referring first to
(8) The next plate 2a in the stack is a heat-transfer plate, provided with three apertures 3, 4 and 6 therethrough adjacent to one edge of the plate apertures 3 and 4 aligning with apertures 3 and 4 in the flow guide plate 1a, when the plates are stacked, and the other aperture 6 opening on one side into the area 5 of the first flow guide plate 1a and thus forming part of the first flow path through the heat exchanger.
(9) Flow guide plate 1b is the third plate in the stack and takes the form of a frame with an edge portion widened to accommodate apertures 3 and 6 aligning with the apertures 3 and 6 in the preceding heat transfer plate 2a. The open area 7 encompassed by the frame communicates with the aperture 4 in the heat transfer plate 2a, allowing gas to flow across the face of the plate to an aperture 4 in the next heat transfer plate 2b, located adjacent the opposite corner of the square shape from the aperture 4 in the preceding heat transfer plate.
(10) The third flow guide plate 1c is in the form of a frame having an aperture 6 located centrally of one side of the frame within an intrusion into the frame, and an aperture 4 at a corner of the opposite side of the frame, which is widened accordingly to accommodate it. The open area 8 of the frame communicates with the aperture 3 of the preceding heat transfer plate 2b and with an aperture 3 in the opposite corner of the third heat transfer plate 2c, which has an aperture 6 corresponding to that in the third flow guide plate 1c and apertures 3 and 4 in the two corners opposite to it.
(11) The same sequence of flow guide and heat transfer plates 1 and 2 is then repeated in the next six plates, but the plates are flipped so that the flow directions across the faces of the heat transfer plates are reversed with respect to the first six plates. The next six plates revert to the pattern of the first six and this pattern is repeated throughout the stack. It will be seen, therefore, that in this particular configuration only three different designs of flow guide plates and three different designs of heat transfer plates need to be manufactured.
(12) Dependent upon the flow-rates of the gases, the number of cells in a heat exchanger stack could vary substantially.
(13)
(14) The heat exchanger of this design makes use of materials which have very similar coefficients of linear thermal expansion in order to avoid stresses which would otherwise build up during thermal cycling and gradients through the length of the heat exchanger. In order to achieve this, the heat exchanger is constructed with 316L stainless steel components throughout, with a high-temperature copper-brazed bond between each component in the construction. Both 316L stainless steel and copper have a coefficient of linear thermal expansion of around 1610.sup.6 mm/ C., rendering them ideal for cooperative use in these applications.
(15) In order for the unit to operate at the pressures which may be required of the hydrogen production system, the heat exchanger must be constructed of a suitable wall-thickness. This requirement is made even greater by the need to withstand an explosion at any point within the gas-transportation system in order to resist the associated radially outward forces.
(16) Similarly, the unit must be designed to withstand the linear cell-to-cell separation forces under such conditions. This requires a substantial area of high-integrity braze interface at each joint in the unit, aided by end-plates of substantial thickness and tie-rods. Placed between each flow-guide plate and each heat transfer plate are pre-formed copper foils which form high-strength joints between the stainless steel plates in the high-temperature vacuum brazing operation in which the unit is finally bonded.
(17) Connectors at each end of each gas pathway are required to withstand the above described pressures and pressure spikes without failure. This, in turn, requires a joint between the heat exchanger end-plate and each connector to be of similarly high integrity. Such connectors may be threaded or tubular in construction, dependent upon mating technologies.
(18) For improved heat transfer, cells may have a matrix of metal past which the gas can freely flow, while giving rise to greater turbulence. This could be in welded or woven mesh form or directly imposed on the profile of the cell plate. As illustrated in
(19) The function of these inserts is three-fold: a. They create turbulent flow of the gases passing across their profile, thereby increasing the potential for transfer of thermal energy b. They provide additional surface area to the gases in order to improve heat transfer, and c. They offer resistance to the deformation of heat transfer plates in the event of a significant differential pressure between cells.
(20) Orientation of flow manifolds in the stack can be varied to accommodate assembly in specific environments, should this be a requirement. An additional benefit of this arrangement is that the number of cells in a given gas stream can be varied to accommodate differential thermal transfer rates from fluid-to-fluid, whether or not the fluid is gaseous or liquid.
(21) Referring now to
(22) By housing a unit of this design in a vacuum chamber, efficient exchange of thermal energy can be achieved, with one end of the unit being at close to ambient temperature, while the other end is at cryogenic temperatures of around 70K to 90K (203.15 C. to 183.15 C.). One example of a system in which there is a heat exchanger according to the invention is shown in
(23) The heat exchanger as described above sits in a vacuum chamber above the Dewar, taking the hydrogen and oxygen streams In at the base, and the mixed-gas stream in at the top. As the streams pass from cell-to-cell, the thermal energy is transferred, with the incoming stream cooled to around 70K to 90K and the outgoing streams warmed to around ambient temperature, thereby reducing to an absolute minimum the power required to maintain the temperature of the LN in the Dewar. This helps optimise the efficiency of the end-to-end process of hydrogen and oxygen production by electrolytic water decomposition.
(24) Other designs and arrangements for a three-stream heat exchanger may be derived from the unit described above. Critically, this application covers the use in combination with a cryogenics system of a heat exchanger which performs to the aforementioned criteria.
(25) In the graphic below, the mixed gas stream enters the heat exchanger from the top and travels down through it, cooling as it passes from cell-to-cell. A condensing coil which sits in the LN finally cools the gas stream, ensuring distillation of 99%+ of the oxygen which collects in the oxygen reservoir near the bottom of the Dewar.
(26) From the O.sub.2 reservoir, the liquid oxygen is forced back out by differential pressure between the incoming and outgoing gas streams to pass through the liquid O.sub.2 flow control valve after which it enters the bottom of the heat exchanger.
(27) Similarly, the hydrogen stream leaves the top of the O.sub.2 reservoir to pass through the heat exchanger. Other designs of cryogenics system may be used for the liquefaction process which will require a 3-stream heat exchanger in order to optimise efficiency.
(28) In the arrangement of cells shown in