LOW WEIGHT TUBE FIN HEAT SINK
20170248379 · 2017-08-31
Inventors
Cpc classification
F21V29/81
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21V29/80
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
The invention provides a lighting device comprising a light source and a heat sink (200). The heat sink (200) is configured to dissipate thermal energy from the light source when in operation. The heat sink comprises a plurality of pin-shaped fins (210) and a support (220), wherein each fin (210) has a fin height (h) relative to the support (220), a bottom part (213) associated with the support (220) and a top part (214), a cross-section having a first width (d1) and a second width (d2) having a ratio d1/d2 selected from the range of 1.2-10, and a first width axis, wherein the first width axes of the pin-shaped fins (210) are arranged parallel, and wherein the pin-shaped fins (210) are hollow over at least part of their fin height (h).
Claims
1-12. (canceled)
13. A heat sink comprising a plurality of pin-shaped fins and a support, wherein each fin has a fin height relative to the support, a bottom part associated with the support and a top part, a cross-section having a first width and a second width having a ratio d1/d2 selected from the range of 1.2-10, and a first width axis, wherein the first width axes of the pin-shaped fins are arranged parallel, and wherein the pin-shaped fins are hollow over at least part of their fin height, wherein each pin-shaped fin comprises a fin wall with the fin wall defining a cavity within the pin-shaped fin having a cavity height, wherein the cavity has a cavity cross-section with a cavity cross-sectional area, wherein over at least part of the cavity height the cavity cross-sectional area reduces in a direction from the top part to the bottom part.
14. A lighting device comprising a light source and a heat sink according to claim 1, wherein the heat sink is configured to dissipate thermal energy from the light source when in operation.
15. The lighting device according to claim 14, wherein the plurality of pin-shaped fins are arranged in an array having one or more pitches selected from the range of 1.2*d1-6*d1.
16. The lighting device according to claim 14, wherein the top parts of the pin-shaped fins are closed.
17. The lighting device according to claim 14, wherein pin-shaped fins have a height in the range of 0.5-100 cm.
18. The lighting device according to claim 14, wherein the heat sink comprises a support structure associated with the top parts of the plurality of pin-shaped fins.
19. The lighting device according to claim 14, wherein the pin-shaped fins are over at least part of their fin height filled with a thermally conductive material.
20. The lighting device according to claim 14, wherein the pin-shaped fins are arranged in a hexagonal array.
21. The lighting device according to claim 14, wherein the lighting device comprises a floodlight.
22. The lighting device according to claim 14, wherein the heat sink is configured to allow during operation of the lighting device an air flow between the pin-shaped fins in a direction parallel to the first width axes.
23. The lighting device according to claim 14, wherein the pin-shaped fins comprise a material selected from the group consisting of aluminum, magnesium, copper, gold, silver, and an alloy comprising one or more of the aforementioned materials.
24. The lighting device according to claim 14, wherein the pin-shaped fins have a cross-sectional shape selected from the group consisting of an oval, a rectangle, and a rhombus.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0039] Embodiments of the invention will now be described, by way of example only, with reference to the accompanying schematic drawings in which corresponding reference symbols indicate corresponding parts, and in which:
[0040]
[0041]
[0042]
[0043] The drawings are not necessarily on scale.
DETAILED DESCRIPTION OF THE EMBODIMENTS
[0044]
[0045] Each fin 210 has a fin height h relative to the support 220, such as in the range of 1-100 cm. Further, each fin has a bottom part 213 associated with the support 220 and a top part 214. As is visible for the fins shown in cross-section, the pin-shaped fins 210 are hollow over 100% of their fin height h. Hence, the total height of the heat sink is the thickness or height of the support 220 and the height h of the fins 210.
[0046] Here, a regular array or pattern 1210 is shown. The fins 210 have thus a pitch p. In the schematically depicted embodiment, the arrangement 1210 is hexagonal. Hence, nearest neighbors may differ in distance or pitch depending upon the direction. In a non-hexagonal arrangement, there may be two different pitches between nearest neighbors (see also
[0047]
[0048]
[0049] As shown in
[0050]
[0051] To prevent pollution of the tubes they are either (partially) filled with a low density material like foamed poly styrene or a thermal conductive material, but alternatively or additionally the top may especially be closed. A preferred way to realize a closed top is by forging a tube with a closed bottom and placing it upside down on the base plate. The tubes can be press-fit on a die-cast base plate that has features on it to press-fit the tube on to, in order to get a good thermal and mechanical interconnection. Further robustness of the heat sink can be obtained interconnecting the tubes with a kind of network, or wires, bands or rims (embodiments of the herein indicated support structure, see also
[0052]
[0053]
[0054]
[0055]
[0056] As boundary conditions, the following conditions were chosen: [0057] Ambient temperature: 25° C. (298 K); [0058] Aluminum thermal conductivity: 237 W/mK (default value); [0059] Radiation included (Heat sink emissivity=0.9); [0060] Gravity effect included; [0061] Opening for air at 0 Pa relative pressure; [0062] Heat flux attached to the bottom surface of fin base (constant for all cases); [0063] Total heat flux=500 W/85800 mm.sup.2=5827.5 W/m.sup.2.
The Shear Stress Transport (SST) turbulence model was used.
[0064] The results (with reference to
TABLE-US-00001 3a 3b 3c 3d Total Exposed area (m.sup.2) 0.026 0.031 0.029 0.027 Base Area 0.0028 0.0025 0.0025 0.0028 Max Temperature rise (° C.) 68 70 76 77 Power (W) (heat flux*Area) 16.3 14.4 14.4 16.3 Average heat transfer coefficient: 12.8 10.7 8.7 10.9 pins (W/m.sup.2K) Average heat transfer coefficient: 3.8 2.7 2.5 3 Base (W/m.sup.2K) Ave base temperature (° C.) 90 87 96 98 Thermal resistance (K/W) 0.13 0.12 0.14 0.15 Mass flow at inlet (kg/s) 4.8 × 4.1 × 3.3 × 4.1 × 10.sup.−4 10.sup.−4 10.sup.−4 10.sup.−4 Temperature rise of air from 34 35 44 35 ambient (° C.) Width ratio (total model width/ 520/17 520/15 520/15 520/17 section width)
[0065] Then, the thermal resistance of the entire heat sink was evaluated, see below table:
TABLE-US-00002 3a 3b 3c 3d No. of fins 330 408 408 330 One fin area (m2) 2.21E−03 2.41E−03 2.24E−03 2.21E−03 Total fin area (m2) 7.29E−01 9.83E−01 9.12E−01 7.28E−01 Base area (m2) 0.0858 0.0858 0.0858 0.0858 Fin efficiency 0.75 0.82 0.75 0.75 Ave HTC fins (W/m2K) 12.8 10.7 8.7 10.9 Ave HTC base (W/m2K) 3.8 2.7 2.5 3 Thermal resistance 0.14 0.11 0.16 0.16 (K/W)
[0066] The result clearly shows that elliptical pin fins provides better results in terms of maximum temperature and thermal resistance. Further, the flow resistance of the elliptical fins is lower compared to the circular fins. The average heat transfer in the system that may even be further optimized is very high. A higher value could be achieved by optimizing the design more.
[0067] Further, thermal calculations have been done on the straight fins of a heat sink of the size that is required for the floodlight example given above. With some assumptions on the material characteristics and the heat transfer coefficient, the total fin weight is around 11 kg and the thermal resistance from fins to ambient is 0.04 K/W. Similar calculations were done with the tube-fin heat sink, in which the pitch between the tubes was set to a preliminary value of 15 mm, and the tube is elliptical in cross section, with 9 mm maximum diameter and 4.5 mm minimum diameter. The tubes are placed in a hexagonal array. Typically 1320 tubes are needed on the 0.52m×0.495 m base. The thermal resistance (Rth) of the fins to the ambient is expected to be comparable to the straight fin heat sink, about 0.04 K/W, but the fin weight is considerably lower, about 3.6 kg, which is even much lower than 6 kg that is expected for 1 mm fin thickness of the straight fin heat sink.
[0068] With the invention, disadvantages of the prior art that are overcome are amongst others: [0069] the high weight of the finned heat sink; [0070] the low bending and buckling stiffness of general thin walled elements; [0071] the high hydraulic resistance of round or hybrid tubular structures placed in an air flow field.
[0072] Hence, the invention may include a heat sink base (“support”) with rulers, supports, bumps, or holes (“connectors”) to attach arrays of tubes to. The base plate may be flat or curved in 1 direction or curved in 2 directions. The tubes have a low wall thickness that are connected to the base plate by e.g. press fit, screwing, soldering, welding or other connection technologies that guarantee a good thermal connection. Further, the tubes are hollow, and have a non-axisymmetric cross-section. Ovals are the first preference, but other hollow rectangular, hexagonal or other multi-angular profiles that are aligned with the expected air flow direction are also possible. Any longitudinal structure with a non-axisymmetric cross section that offer a high bending stiffness and strength while also offering cooling area which can have addition holes or slits, and that are aligned with the expected air flow direction. For instance, forged (oval) tubes that have a (flat) bottom can be are placed upside down on the heat sink base. Optionally, a low density material to fill the hollow tubular structures preventing pollution and giving additional stiffness to the tubes. Optionally a structure to mechanically interconnect the tubes for robustness, which can be combined with the lids mentioned above.