HEAT EXCHANGER CORE LAYER
20230408213 ยท 2023-12-21
Inventors
Cpc classification
F28F3/048
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
F28F3/044
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D9/0037
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D9/0081
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
F28F2255/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F3/022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F28F3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A pin for a core layer of a heat exchanger, the pin being an additively manufactured pin having a sinusoidal shape between an upper and a lower sheet.
Claims
1. A pin for a core layer of a heat exchanger, the pin being an additively manufactured pin having a sinusoidal shape between a first end of the pin and a second end of the pin.
2. The pin of claim 1, wherein the pin defines at least one further curve between the first end of the pin and the second end of the pin.
3. The pin of claim 2, wherein the pin has a cross-section that tapers from an inlet side of the pin to an outlet side of the pin.
4. The pin of claim 3, wherein the cross-section is a rounded triangular shape.
5. A layer for a heat exchanger, the layer comprising: an inlet; an outlet; an upper sheet; a lower sheet; a fluid flowpath defined between the upper sheet and lower sheet and from the inlet to the outlet; and at least one pin disposed in the flowpath and connecting the upper sheet to the lower sheet; wherein the at least one pin is an additively manufactured pin that defines a substantially sinusoidal shape by extruded cross-section along a sine wave path between the upper sheet and the lower sheet.
6. The layer of claim 5 having a plurality of said at least one pin.
7. The layer of claim 6, the layer defining an inflow path from the inlet, and an outflow path to the outlet, the inflow path and the outflow path being separated in the layer by a separation bar, the inflow path and the outflow path each having a plurality of said pins, the layer further comprising a plurality of turning vanes to turn the direction of flow from the inflow path by substantially 180 degrees to the outflow path.
8. The layer of claim 7, wherein the plurality of turning vanes includes a first plurality of vanes to turn the direction of flow from the inflow path by substantially 90 degrees and a second plurality of turning vanes to turn the direction of flow by a further 90 degrees to the outflow path.
9. A heat exchanger comprising: a first layer and second layers both formed according to claim 5; and wherein the upper sheet of the second layer is also the lower sheet of the first layer.
10. The heat exchanger according to claim 9, wherein the number of pins disposed in the flowpath of the first layer is different from the number of pins disposed in the flowpath of the second layer.
11. A method of additively manufacturing a pin for layer for a heat exchanger, the method comprising: additively manufacturing a pin having a sinusoidal shape wherein the cross-section of the pin is extruded along a sine wave path between the lower sheet and the upper sheet.
12. A method of manufacturing a layer for a heat exchanger comprising: providing a first sheet and a second sheet: additively manufacturing at least one pin according to the method of claim 11; and locating the at least one pin between the first and the second sheet such that the first end is located at the first sheet and the second end is located at the second sheet.
13. A method of manufacturing a heat exchanger, the method comprising: manufacturing a first plurality of layers interleaved with a second plurality of layers, wherein each layer of the first and second pluralities of layers is manufactured according to the method of claim 12; manufacturing a first header fluidly connected to each of the first plurality of layers; and manufacturing a second header fluidly connected to each of the second plurality of layers.
14. The method according to claim 11, wherein each step of additive manufacturing is performed using a metal powder bed SLM process or other additive manufacturing process, wherein a powder of the metal is one of an aluminium alloy, a titanium alloy, an austenitic nickel-chromium-based superalloy, stainless steel or copper.
15. The method according to claim 12, wherein each step of additive manufacturing is performed using a metal powder bed SLM process or other additive manufacturing process, wherein a powder of the metal is one of an aluminium alloy, a titanium alloy, an austenitic nickel-chromium-based superalloy, stainless steel or copper.
16. The method according to claim 13, wherein each step of additive manufacturing is performed using a metal powder bed SLM process or other additive manufacturing process, wherein a powder of the metal is one of an aluminium alloy, a titanium alloy, an austenitic nickel-chromium-based superalloy, stainless steel or copper.
Description
BRIEF DESCRIPTION
[0022] Certain embodiments of the present disclosure will now be described in greater detail by way of example only and with reference to the accompanying drawings in which:
[0023]
[0024]
[0025]
[0026]
[0027]
[0028]
DETAILED DESCRIPTION
[0029]
[0030] The first header 12 connects to a first plurality of layers 30 of the heat exchanger core 11. The second header 14 connects to a second plurality of layers 31 of the heat exchanger core 11. The first plurality of layers 30 is interleaved with the second plurality of layers 31 so that the first fluid flows through every second layer and the second fluid flows through the layers in-between the first fluid layers, providing alternate layers of first fluid flow and second fluid flow. Alternate layers are typically rotated by 180 degrees relative to each other. At least within the heat exchanger 10, the first fluid flowing in the first plurality of layers 30 is fluidly isolated from the second fluid flowing in the second plurality of layers by the sheets separating the layers.
[0031] As shown in
[0032] With reference to
[0033] Similarly, a first portion of the second header 14 connects to the inlet side 32 of each layer 31 and, in use, fluid is pumped into the first portion and flows into the inlet side 32 of every layer connected to the second header 14. The fluid flows through each of the layers 3 land out through the outlet 34 of each layer. The outlets 34 are all connected to the second portion of the second header 14, the second portion being fluidly isolated from the first portion. Fluid flows into the second portion and then out of the second header 14.
[0034] Within each layer 30, as shown in
[0035] Additionally, there may be provided within each layer 30 a first set of turning vanes 200a that may turn the flow through 90 degrees, and a second set of turning vanes 200b that may turn the flow through a further 90 degrees, to create the overall U-shaped flow path. A plurality of pins 100b may be disposed between the first and second sets of turning vanes 200a, b. The pins 100 shown in
[0036]
[0037]
[0038] The sinusoidal shape of the pin creates turbulence in the fluid flow thus leading to improved thermal exchange. This can be seen by the arrows in
[0039] In a heat exchanger core, as described above, several such layers will be provided, separated by the sheets.
[0040] Whilst a simple sinusoidal shape pin has been described, it is also conceivable that the pins are formed by extruded cross-section (see
[0041] Any or all parts of the heat exchanger 10 other than the pins may be made from metal. In some embodiments, some or all parts are made from an austenitic nickel-chromium-based superalloy, such as the Inconel family of metals manufactured by the Special Metals Corporation of New York state, USA. In other embodiments, some or all parts may be made from an aluminium alloy, a titanium alloy, stainless steel or copper.
[0042] The first and second fluids may be oil, such that the heat exchanger 10 is an oil-oil heat exchanger. However, in other embodiments, the first fluid may be different from the second fluid. Other fluids, including air, water, fuel(s), or carbon dioxide are also envisaged for either or both of the first and second fluids.
[0043] While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.