The present disclosure relates to a heat transfer tube which is especially suitable for a heating furnace. The present disclosure further relates to a cracking furnace using the heat transfer tube.
Cracking furnaces, the primary equipment in the petrochemical industry, are mainly used for heating hydrocarbon material so as to achieve cracking reaction which requires a large amount of heat. Fourier's theorem says,
wherein q is the heat transferred, A represents the heat transfer area, k stands for the heat transfer coefficient, and dt/dy is the temperature gradient. Taking a cracking furnace used in the petrochemical industry as an example, when the heat transfer area A (which is determined by the capacity of the cracking furnace) and the temperature gradient dt/dy (which is determined by the furnace coil material and burner capacity) are determined, the only way to improve the heat transferred per unit area q/A is to improve the value of the heat transfer coefficient k, which is subject to influences from thermal resistance of the main fluid, thermal resistance of the boundary layer, etc.
In accordance with Prandtl's boundary layer theory, when an actual fluid flows along a solid wall, an extremely thin layer of fluid close to the wall surface would be attached to the wall without slippage. That is to say, the speed of the fluid attached to the wall surface, which forms a boundary layer, is zero. Although this boundary layer is very thin, the heat resistance thereof is unusually large. When heat passes through the boundary layer, it can be rapidly transferred to the main fluid. Therefore, if the boundary layer can be somehow thinned, the heat transferred would be effectively increased.
In the prior art, the furnace pipe of a commonly used cracking furnace in the petrochemical industry is usually structured as follows. On the one hand, a rib is provided on the inner surface of one or more or all of the regions from the inlet end to the outlet end along the axial direction of the furnace coil in the cracking furnace, and extends spirally on the inner surface of the furnace coil along an axial direction thereof. Although the rib can achieve the purpose of agitating the fluid so as to minimize the thickness of the boundary layer, the coke formed on the inner surface thereof would continuously weaken the role of the rib as time lapses, so that the function of reducing the boundary layer thereof will become smaller. On the other hand, a plurality of fins spaced from one another are provided on the inner surface of the furnace pipe. These fins can also reduce the thickness of the boundary layer. However, as the coke on the inner surface of the furnace pipe is increased, these fins will similarly get less effective.
Therefore, it is important in this technical field to enhance heat transfer elements so as to further improve heat transfer effect of the furnace coil.
To solve the above technical problem in the prior at, the present disclosure provides a heat transfer tube, which possesses good transfer effects. The present disclosure further relates to a cracking furnace using the heat transfer tube.
According to a first aspect of the present disclosure, it discloses a heat transfer tube comprising a twisted baffle arranged on an inner wall of the tube, said twisted baffle extending spirally along an axial direction of the heat transfer tube and being provided with a non-through gap extending from one end to the other end of the twisted baffle along an axial direction of the heat transfer tube.
In the heat transfer tube according to the present disclosure, with the arrangement of the twisted baffle, fluid can flow along the twisted baffle and turns into a rotating flow. A tangential speed of the fluid destroys the boundary layer so as to achieve the purpose of enhancing heat transfer. Besides, the arrangement of the gap reduces the resistance of fluid in the heat transfer tube, which further reduces the pressure loss of the fluid. Moreover, the gap is non-through, i.e., the twisted baffle is still an integral piece with both of the two side edges thereof connecting to the heat transfer tube, thus increasing the stability of the twisted baffle under the impact of the fluid.
In one embodiment, the twisted baffle has a twist angle of between 90° to 1080°. When the twist angle is relatively small, the pressure drop of the fluid and the tangential speed of the rotating fluid are both small. Therefore, the heat transfer tube is of poor effect. As the twist angle turns larger, the tangential speed of the rotating flow would increase, so that the effect of the heat transfer tube would be improved, but the pressure drop of the fluid will be increased. When the twist angle ranges from 120° to 360°, the capacity of the heat transfer tube and the pressure drop of the fluid both fall within proper ranges. The ratio of the axial length of the twisted baffle to the inner diameter of the heat transfer tube is in a range from 1:1 to 10:1. When this ratio is relatively small, the tangential speed of the rotating flow is relatively great, so that the heat transfer tube is of high capacity but the pressure drop of the fluid is relatively great. As the value of the ratio gradually increases, the tangential speed of the rotating flow would turn smaller, and thus the capacity of the heat transfer tube would be decreased, but the pressure drop of the fluid would turn smaller. When this ratio ranges from 2:1 to 4:1, both the capacity of the heat transfer tube and the pressure drop of the fluid would fall within respective proper scopes. The twisted baffle of such size further enables the fluid in the heat transfer tube with a tangential speed sufficient enough to destroy the boundary layer, so that a better heat transfer effect can be achieved and there would be a smaller tendency for coke to be formed on the heat transfer wall.
In one embodiment, the area ratio of the gap to the twisted baffle falls within a range from 0.05:1 to 0.95:1. When this ratio is relatively small, the twisted baffle has a great diversion effect to the fluid, so that the heat transfer effect of the tube is good, but the pressure drop of the fluid is also great. As this ratio turns larger, the diversion effect of the twisted baffle to the fluid and the pressure drop of the fluid would grow smaller, but the heat transfer effect would also accordingly turn poorer. When this ratio stays within the range from 0.6:1 to 0.8:1, both the capacity of the heat transfer tube and the pressure drop of the fluid achieve proper ranges. In addition, with the area ratio within the above range, the fluid has a small pressure loss and the twisted baffle has a high resistance to impact. In one embodiment, the gap has a contour line of a smooth curve, which facilitates flow of the fluids, reduces resistance thereof and further reduces pressure loss of the fluid. In a specific embodiment, the smooth curve comprises two identical curve segments, which are centrosymmetric with respect to a centerline of the heat transfer tube. In one embodiment, the ratio of the width of a starting end of the gap to an inner diameter of the heat transfer tube is in a range from 0.05:1 to 0.95:1, preferably from 0.6:1 to 0.8:1, with either of the curve segments extending from the starting end towards a tail end of the gap. The ratio of the x-axis component of the curvature radius change rate of the curve segment to the inner diameter of the heat transfer tube ranges from 0.05:1 to 0.95:1; the ratio of the y-axis component of the curvature radius change rate of the curve segment to the inner diameter of the heat transfer tube ranges from 0.05:1 to 0.95:1; and the ratio of the z-axis component of the curvature radius change rate of the curve segment to the inner diameter of the heat transfer tube ranges from 1:1 to 10:1. When the ratio of the z-axis component of the curvature radius change rate of the curve segment to the inner diameter of the heat transfer tube is relatively small, the tangential speed of the rotating fluid is great, so that the heat transfer effect is good, but the pressure drop of the fluid is also great. As this ratio turns greater, both the tangential speed of the rotating fluid and the pressure drop of the fluid would grow smaller, but the heat transfer effect would also accordingly turn poorer. When this ratio stays within the range from 2:1 to 4:1, both the capacity of the heat transfer tube and the pressure drop of the fluid achieve proper ranges. The gap contour line formed in this way possesses the best hydrodynamic effects, i.e., a minimum of the hydraulic pressure is generated and a maximum of the impact resistance of the twisted baffle is achieved.
In one embodiment, there are two gaps, which extend from different ends of the twisted baffle towards each other along the axial direction of the heat transfer tube without intersection. The area ratio of the upstream gap to the downstream gap is in a range from 20:1 to 0.05:1. When the ratio is relatively large, both the pressure drop of the fluid and the tangential speed of the rotating fluid are small, so that the heat transfer effect is poor. As this ratio turns smaller, the tangential speed of the rotating fluid would grow larger, and the capacity of the heat transfer tube would be improved, but the pressure drop of the fluid would be increased. When this ratio stays within the range from 2:1 to 0.5:1, both the capacity of the heat transfer tube and the pressure drop of the fluid achieve proper ranges. In addition, the downstream gap is beneficial for further lowering resistance of the fluid so as to lower the pressure drop. Furthermore, the arrangement of an upstream gap and a downstream gap is advantageous for decreasing the weight of the twisted baffle, thus facilitating arrangement and use thereof.
In one embodiment, the twisted baffle is provided with a plurality of holes. Both axial and radial flowing fluids can flow through the holes, i.e., these holes can alter the flow directions of the fluids, so as to enhance turbulence in the heat transfer tube, thus destroying the boundary layer and achieving the purpose of enhancing heat transfer. In addition, fluids from different directions can all conveniently pass through these holes and flow downstream, thereby further reducing resistance to flow of the fluids and reducing pressure loss. Coke pieces carried in the fluids can also pass through these holes to move downstream, which facilitates the discharge of the coke pieces. In a preferred embodiment, the ratio of an axial distance between the centerlines of two adjacent holes to an axial length of the twisted baffle ranges from 0.2:1 to 0.8:1.
According to a second aspect of the present disclosure, it discloses a cracking furnace, comprising at least one, preferably 2 to 10 of heat transfer tubes according to the first aspect of the present disclosure.
In one embodiment, a plurality of the heat transfer tubes are arranged in the radiant coil along an axial direction thereof in a manner of being spaced from each other, with the ratio of a spacing distance to the diameter of the heat transfer tube in a range from 15:1 to 75:1, preferably from 25:1 to 50:1. The plurality of heat transfer tubes spaced from one another continuously alter the fluid in the radiant coil from piston flow into rotating flow, thus improving the heat transfer efficiency.
In the context of the present disclosure, the term “piston flow” ideally means that fluids mix with each other in the flow direction but by no means in the radial direction. Practically however, only approximate piston flow rather than absolute piston flow can be achieved.
Compared with the prior art, the present disclosure excels in the following aspects. To begin with, the arrangement of the twisted baffle in the heat transfer tube turns the fluid flowing along the twisted baffle into a rotating fluid, thus improving the tangential speed of the fluid, destroying the boundary layer and achieving the purpose of enhancing heat transfer. Next, the twisted baffle is provided with a non-through gap extending along the axial direction of heat transfer tube from one end towards the other end of the twisted baffle. The gap decreases resistance of the fluids in the heat transfer tube, thus decreasing pressure loss of the fluid. Besides, the gap is non-through, i.e., the twisted baffle is actually an integral piece with two side edges thereof both connecting to the heat transfer tube, which improves stability of the twisted baffle under the impact of the fluid. In addition, the plurality of holes provided on the twisted baffle can change the flow direction of the fluid so as to strengthen the turbulence in the heat transfer tube and achieve the object of enhancing heat transfer. Moreover, these holes further reduce the resistance in the flow of the fluid, so that pressure loss is further decreased. In addition, coke pieces carried in the fluid can also move downstream through these holes, which promotes the discharge of the coke pieces.
In the following, the present disclosure will be described in detail in view of specific embodiments and with reference to the drawings, wherein,
In the drawings, the same component is referred to with the same reference sign. The drawings are not drawn in accordance with an actual scale.
The present disclosure will be further illustrated in the following in view of the drawings.
The axial length of the twisted baffle 11 can be called as a “pitch”, and the ratio of the “pitch” to the inner diameter of the heat transfer tube can be called a “twist ratio”. The twist angle and twist ratio would both influence the rotation degree of the fluid in the heat transfer tube 10. When the twist ratio is determined, the larger the twist angle is, the higher the tangential speed of the fluid will be, but the pressure drop of the fluid would also be correspondingly higher. The twisted baffle 11 is selected as with a twist ratio and twist angle which can enable the fluid in the heat transfer tube 10 to possess a sufficiently high tangential speed to destroy the boundary layer, so that a good heat transfer effect can be achieved. In this case, a smaller tendency for coke to be formed on the inner wall of the heat transfer tube can be resulted and the pressure drop of the fluid can be controlled as within an acceptable scope. By arranging the gap 12 on the twisted baffle 11, the contact area of the fluid with the twisted baffle 11 is significantly reduced, thus reducing the resistance of the fluid in the heat transfer tube 10 and the pressure drop of the fluid. In addition, the gap 12 is non-through, i.e., the twisted baffle is actually an integral piece with two side edges thereof both connecting to the heat transfer tube 10, which improves stability of the twisted baffle 11 in the heat transfer tube 10.
As a matter of fact, the twisted baffle 11 indicated in
Although
The present disclosure further relates to a cracking furnace (not shown in the drawings) using the heat transfer tube 10 as mentioned above. A cracking furnace is well known to one skilled in the art and therefore will not be discussed here. A radiant coil 50 of the cracking furnace is provided with at least one heat transfer tube 10 as described above.
In the following, specific example will be used to explain the heat transfer efficiency and pressure drop of the radiant coil 50 of the cracking furnace when the heat transfer tube 10 according to the present disclosure is used.
The radiant coil of the cracking furnace is arranged with 6 heat transfer tubes 10 with twisted baffles as indicated in
The radiant coil of the cracking furnace is mounted with 6 prior art heat transfer tubes 50′. The heat transfer tube 50′ is structured as being provided with a twisted baffle 51′ in a casing of the heat transfer tube 50′, the twisted baffle 51′ dividing the heat transfer tube 50′ into two material passages non-communicating with each other as indicated in
In view of the above example and comparative example, it can be derived that compared with the heat transfer efficiency of the radiant coil in the cracking furnace using the prior art heat transfer tube, the heat transfer efficiency of the radiant coil in the cracking furnace using the heat transfer tube according to the present disclosure is significantly improved, and the pressure drop is also decreased. The above features are very beneficial for hydrocarbon cracking reaction.
Although this disclosure has been discussed with reference to preferable examples, it extends beyond the specifically disclosed examples to other alternative examples and/or use of the disclosure and obvious modifications and equivalents thereof. Particularly, as long as there are no structural conflicts, the technical features disclosed in each and every example of the present disclosure can be combined with one another in any way. The scope of the present disclosure herein disclosed should not be limited by the particular disclosed examples as described above, but encompasses any and all technical solutions following within the scope of the following claims.
Number | Date | Country | Kind |
---|---|---|---|
201310512687.2 | Oct 2013 | CN | national |
This application is a divisional application of U.S. application Ser. No. 14/068,543, filed on Oct. 31, 2013, which claims benefit of priority under 35 U.S.C. § 119 to Chinese Patent Application No. CN 201310512687.2, filed Oct. 25, 2013, the contents of each are also incorporated herein by reference in their entireties.
Number | Name | Date | Kind |
---|---|---|---|
1056373 | Segelken | Mar 1913 | A |
4727907 | Duncan | Mar 1988 | A |
5492408 | Alfare | Feb 1996 | A |
5605400 | Kojima | Feb 1997 | A |
5813762 | Fleischli | Sep 1998 | A |
Number | Date | Country | |
---|---|---|---|
20190128622 A1 | May 2019 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 14068543 | Oct 2013 | US |
Child | 16232759 | US |