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Numerical Simulation of Temperature Field in the Cyclone

Pingyang Xiao a and Zhenwei Zhang b

School of Mechanical Engineering and Automation, Northeastern University, Shenyang, Liaoning, 110004, China

a xpypaper@https://www.sodocs.net/doc/ad778406.html,,

b zzw1658@https://www.sodocs.net/doc/ad778406.html,

Keywords: Separator, Numerical Simulation, Temperature Field.

Abstract. This paper mainly focuses on the numerical simulation of temperature field in the cyclone separation. The authors took advantage of RSM turbulence model of software FLUENT to imitate the temperature field. This thesis puts forward the temperature distribution of the cyclone, and figures out that the overall temperature is 373°C. Temperature difference in different region is less than one centigrade degree with the maximum temperature in the cone part and the minimum temperature in inlet tube and cylinder part of the cyclone, what’s more, the temperature is relatively higher near the wall. The air compression can lead the higher temperature in the lower part, so the cone part has the highest temperature. The higher temperature near the wall is caused by the friction between the wall and flow.

Introduction

This paper mainly focuses on the flow field phenomenon of gas-solid separation process in CLT/A type cyclone separator about the potato granules drying system. The simulation is established based on the discrete coupling model, the assumption of which is that the model needs the constant temperature. It is really necessary to simulate the temperature field of CLT/A type cyclone as the temperature of hot air is relatively high in the drying system and the internal temperature conditions can not be determined.

Physical model

The cylindrical volume is relatively large in the cyclone group of CLT/A 8.4×4 type shown in Fig.

1. The cyclone separator is divided into four sub-cylinders, which show symmetrical layout and the structure is identical. Therefore the simulation only focuses on the single cylinder.

Fig. 1 Structure group graph of Fig. 2 Three-dimensional solid model

CLT / A 8.0 × 4-type cyclone of the CLT / A-type cyclone

The three-dimensional model can be obtained by taking advantage of powerful modeling capabilities of solid surface of UG about CLT/A type cyclone shown in Fig. 2.

Finite element model

The three-dimensional solid model established by UG can be imported into GAMBIT so as to be meshed. Multiple Boolean operations should be carried out on the solid model in order to be facilitated to mesh in GAMBIT, which can lead to the establishment of two entities form. The overall body of Volom1 is consisted of exhaust volute and exhaust pipe. The overall body of Volom2 is consisted of entrance pipe and cone below the cylinder. Then the model is exported in the .step format, and then the model will be imported into GAMBIT. The total model is shown in Fig. 3. Meshing should be conducted in the several parts of model in order to generate the better structured grid. The operations in GAMBIT can be shown as flowing.

(1) Establish the auxiliary plane and split the intake pipe with the Split command.

(2) The cylinder can be divided into two parts with a plane parallel to Y-axis at Y=2260mm, the

upper of which is ring cylinder and the lower part is cylinder.

Fig. 3 Physical model of cyclone in GAMBIT Fig. 4 Mesh diagram of CLT / A-type cyclone

The entire cyclone is divided into four parts: intake pipe, outtake pipe, lower half part of the cylinder and the upper half part of the cylinder. The meshing can be imposed on them separately. Meshing is the premise process of numerical simulation and also the discrete process of calculating region. The number of the grid has nothing to do with the final result according to the theory of CFD, and when the intensity of the grid reaches a certain value, it has little effect on the simulation result by continuing encryption [1]. However, in practice, if the mesh is too sparse, it is difficult to describe some detail in the flow field. What’s more, the computing speed can be greatly affected if the number of the meshing is too large. Therefore the number select of the grids can both guarantee the accuracy requirements and avoid excessive consumption of the system resources [2]. This paper adopts the complex grids according to the complexity of the flow field and variability of local feature. The hexahedral grid can be generated, which is the main structure, by taking advantage of Hex/Wedge-type structured grid and Cooper barrel pattern. This kind of grid matches well with the flow field, and is conductive to process of coupling conditions in the numerical simulation region. The meshing can be drawn as Fig. 4.

Boundary conditions

The gas phase can be simplified in order to facilitate solving the multiphase flow inside the cyclone

[3].

(1) Gas flow is steady-state in cyclone;

(2) The gas flow rate is low( generally less than 30m/s), and the gas can be seen as incompressible

fluid;

(3) The inlet air flows evenly, and in a fully developed turbulent state;

(4) No gas exhausts from the dust exhaust at the bottom of the cyclone.

Set the boundary conditions as following:

(1) Inlet boundary: the inlet air temperature is 373.15K, and the density is 1.225 kg/m3. The viscosity

is 18.1×10-6 . The entrance speed is known, so the inlet boundary is set as the velocity inlet boundary condition. Assuming that the inlet turbulent is developed fully, and the gas inlet velocity is set as 15 m/s evenly distribution throughout the inlet section. The turbulence intensity is set as I and the hydraulic diameter is set as D. Flow Reynolds number is shown as Eq. 1.

4e 61.225150.252R 2.5725101810

UD ρμ?××===××. (1) Hydraulic diameter is set as Eq. 2. 220.460.2070.2940.460.207HD ab D a b ××===++. (2)

Turbulence Intensity is set as Eq. 3. 1/851/8e 0.16(R )100%0.16(2.5710)7.34%I ??=×=××=.

(3) (2) Outlet boundary: outlet boundary is set as outflow boundary. Assuming that the flow condition is

in fully developed condition, namely the flow situation can be obtained by the pulling of flow field. The air exhaust can be set as the outflow, and the weight of the flow is set as one. The dust exhaust is set as outflow, and the weight of the flow is set as zero.

(3) Wall conditions: take the standard wall function, namely the wall has no-slip boundary [4]. The

roughness parameter of wall is set as 0.5.

(4) The overlapping circle is set as interface surface, which connects the exhaust pipe and cylinder.

Fig. 5 Total temperature field

Numerical simulation analysis

Temperature distribution at various locations in CLT/A type cyclone can be intuitively obtained through numerical simulation shown in the Fig. 5. The entrance temperature is relatively low, and temperature can increase with moving downward along the cone. The value can reach the highest at the bottom of cone. The exhaust temperature can decrease along the exhaust pipe, but is still higher than inlet air temperature. The temperature change reason is shown as following: the air enters the air intake with the number of 100, and the flow can be compressed by centrifugal force caused by the rotation. In addition, the temperature can be increased due to the friction between the flow and wall. The temperature continues to rise owing to the further impact of compression and friction when reaches the cone wall. The final flow will be excluded through the exhaust pipe with some pressure decrease lower than the cone and bigger than the cylinder and inlet, namely the temperature is center. However the temperature change is small, and the left table stays at 3.73e+2 from start to finish shown from the color column. The temperature is about 100℃ in the cyclone with only less than one temperature change. Therefore temperature change is small.

Fig. 6 and Fig. 7 respectively show the temperature distribution in Y=0 section about static and total temperature in CLT/A type cyclone separator. The static temperature distribution has the same situation with the total temperature distribution in the Y=0 cross section in the cyclone, and specific temperature change region inside the cyclone can be clear obtained. The temperature of air intake and cylinder is the lowest with the maximum temperature in the cone part, and the temperature of exhaust pipe stays centre. The exhaust pipe temperature can decrease further. Temperature distribution shows a symmetrical situation in both sides of the exhaust pipe or inside the exhaust pipe in cyclone with only little difference near the wall, which shows the vortex shape. The small difference is caused by the local turbulence accompanied by the rotation flow inside cyclone.

Fig. 6 Y=0 Static temperature Fig. 7 Y=0 Total temperature

Fig. 8 and Fig. 9 respectively show the temperature distribution in X=0 section about static and total temperature in CLT/A type cyclone separator. Temperature distribution of each parts of the X=0 cross section can be seen clearly in the picture. Internal temperature distribution of X=0 section has the same situation with the total temperature distribution in cyclone. The cylinder part below the exhaust pipe has almost the same temperature distribution with the lower cone compared with the section Y=0 with only obvious difference in the position above the air exhaust, the reason for which is that the asymmetry caused the flow’s entrance from the unilateral line.

Fig. 8 X=0 Static temperature Fig. 9 X=0 Total temperature

Temperature distribution can be respectively obtained in the section Z=0.5, Z=0.75, Z=1, Z=1.25, Z=1.5, Z=1.75 and Z=2 in the cyclone shown in Fig. 10, which also shows that temperature near the wall is relatively high, the reason for which is that friction between the flow and wall and compression effect of centrifugal force can lead the enhancement of temperature. Temperature gradient of each cross-section shows circular ring, better symmetry and a certain degree irregularity that can be caused by the different local turbulence.

Fig. 10 The temperature distribution on Z = 0.5, 0.75, 1, 1.25, 1.5, 1.75, 2 cross section

Conclusion

This thesis puts forward the temperature distribution of the cyclone with type of CLT/A, and figures out that the overall temperature is about 373°C. Temperature difference in different region is less than one centigrade degree with the maximum temperature in the cone part and the minimum temperature in inlet tube and cylinder part of the cyclone, what’s more, the temperature is relatively higher near the wall. The air compression can lead the higher temperature in the lower part, so the cone part has the maximum temperature which is caused by the strengthen impact of air compression. The higher temperature near the wall is caused by the friction between the wall and flow. The total temperature in the cyclone stays a constant value with almost no change and local difference can be obtained.

References

[1] F. Boysan, B. Ewan and J. Swithenbank: Experimental and Theoretical Studies of Cyclone Separator Aerodynamics: (Chem E Symp Series, P. 305-320, 1983).

[2] W. Q. Tao. Modern Process of Heat Transfer Calculation: (Science Press, 2002).

[3] G. L. Gao. Thermal Engineering and Fluid Mechanics: (China Electric Power Press, P. 130-131,

China 1997).

[4] Y. Mao, L. Pang, X. W. Wang et al. Numerical Simulation of Three-dimensional Turbulence in

Cyclone: (Petroleum Refining and Chemical Industry, V. 33(2), P. 1-6, China 2002).

Advanced Mechanical Design

10.4028/https://www.sodocs.net/doc/ad778406.html,/AMR.479-481

Numerical Simulation of Temperature Field in the Cyclone 10.4028/https://www.sodocs.net/doc/ad778406.html,/AMR.479-481.462

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1GENERAL INSTRUCTIONS 1.1Type area The text should fit exactly into the type area of 187 ?272 mm (7.36" ?10.71"). For correct settings of margins in the Page Setup dialog box (File menu) see Table 1. Table 1. Margin settings for A4 size paper and letter size paper. * Column dialog box in Format menu. 1.2Typefont, typesize and spacing Use Times New Roman 12 point size and 14 point line spacing (Standard; text tag). Use roman type except for the headings (Heading tags), parameters in mathematics (not for log, sin, cos, ln, max., d (in d x), etc), Latin names of species and genera in botany and zoology and the titles of journals and books which should all be in italics. Never use bold, except to denote vectors in mathematics. Never underline any text. Use the small font (10 points on 11 points) for tables (Table tags), figure captions (Figure caption tag) and the references (Reference text tag). Never use letterspacing and never use more than one space after each other. 2GETTING STARTED 2.1Preparing the new file with the correct template Copy the template file B2ProcA4.dot (if you print on A4 size paper) or B2ProcLe.dot (for Letter size paper) to the template directory. This directory can be found by selecting the Tools menu, Options and then by tabbing the File Locations. When the Word programme has been started open the File menu and choose New. Now select the template B2ProcA4.dot or B2ProcLe.dot (see above). Start by renaming the document by clicking Save As in the menu Files. Name your file as follows: First three letters of the file name should be the first three letters of the last name of the first author, the second three letters should be the first letter of the first three words of the title of the paper (e.g. this paper: balpcc.doc). Now you can type your paper, or copy the old version of your paper onto this new formated file. 2.2Copying old text onto new file Open your old file and the new file. Switch between these two with the Window menu. Select all text of the old file (excluding title, authors, affiliations and Preparing a Two Column Paper with MS Word for Windows W.J. ZHOU & J.Tang A.A. Balkema Publishers, Rotterdam, Netherlands C.T.Zhao New Institute, Gouda, Netherlands ABSTRACT: Authors of papers to proceedings have to type these in a form suitable for direct photographic reproduction by the publisher. In order to ensure uniform style throughout the volume, all the papers have to be prepared strictly according to the instructions set below. A laser printer should be used to print the text. The publisher will reduce the camera-ready copy to 75% and print it in black only. For the convenience of the authors template files for MS Word 6.0 (and higher) are provided. KEYWORD: In order to; MS Word

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ei会议论文怎么检索.doc ei 会议论文怎么检索 ei 会议论文怎么检索(共 3 篇) 篇一:EI 检索的国际会议论文标准格 式 The Structure Optimization of the Siphonic Bedpan’s Floerical
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Simulation Technology
Ge Zhenghao, ENSIONAL STEADY
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NUMERIC SIMULATION FOR FLOENT America The preferred spelling is ent” in after the “g”. Avoid the stilted expression, DXDiTa9E3d “One of us (R.B.G.) thanks . . .” Instead, try “R.B.G. thanks”. Put applicable sponsor acknoents here; DO NOT place them on the first page of your paper or as a footnote. REFERENCES [1] Yue bangguo, “Talking about bedpan?s flushing filth function and saving ents of puting hydromechanics. Beijing: the Science Press. 2001. 1-8. (in Chinese) [3] Hong fangulation and experimentation research,” Doctor Degree thesis. ethod for the dynamics of free boundaries. Journal of Computational Physics, 1981, 39:201-225. [5] Lin huzong, Phantasmagoric floultiphase hydromechanics. Beijing: the book concern of Qinghua University, Guangzhou: the book concern of Jinan University. (in Chinese) [6] in, The theory and numeric method on finite element analysis. Beijing: the book concern of Qinghua University, 1997. (in Chinese) 篇二:EI 学术论文检索、EI 会议论
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文核心检索入口 EI 论文检索入口
华译网论文翻译专业机构汇集
EI 检索地址如下,本文后附有华译网 EI 论文翻译价格和英文论文外 籍校对价格,欢迎大家惠顾.chinatranslation.。 EI 论文检索入口 常用网址如下: 英特网 EI 官方网址: /Kns55/brief/Result_CPFD.htm 清华大学图书馆: /service/SCIcenter/eiall. 《工程索引》(The Engineering Index,
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简称 EI)是美国工程信息公司(Engineering information Inc.)出版 的著名工程技术类综合性检索工具。收录文献几乎涉及工程技术各 个领域。例如:动力、电工、电子、自动控制、矿冶、金属工艺、 机械制造、管理、土建、水利、教育工程等。它具有综合性强、资

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