COMPARATIVE THERMAL ANALYSIS OF CONVENTIONAL TUBULAR HEAT EXCHANGER WITH HELIXCHANGER USING BELL-DELAWARE METHOD

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COMPARATIVE THERMAL ANALYSIS OF CONVENTIONAL TUBULAR HEAT EXCHANGER WITH HELIXCHANGER USING BELL-DELAWARE METHOD Prof.S.S.SHINDE 1*, P.V.HADGEKAR 2, Dr.S.PAVITRAN 3 1 Department of Mechanical Engineering Vishwakarma Institute of Technology, Pune. 2 Department of Mechanical Engineering Vishwakarma Institute of Technology, Pune. 3 Department of Mechanical Engineering Vishwakarma Institute of Technology, Pune. *Corresponding author email: sunilkumarshinde@gmail.com, +91-9890602638 Abstract Heat exchangers are important heat & mass transfer apparatus in oil refining, chemical engineering, environmental protection, electric power generation etc. Among different types of heat exchanger, shell-andtube heat exchangers (STHXs) have been commonly used in Industries. Thermal analysis of helixchanger-a heat exchanger with helical baffles hasn t been done using Bell-Delaware method. Bell-Delaware method is proven & has been verified by other researchers. The present work modifies the existing Bell-Delaware method used for conventional heat exchanger, taking into consideration the helical geometry of helixchanger. The thermal analysis of Helixchanger using Bell-Delaware method which gives clear idea that the ratio of heat transfer coefficient per unit pressure drop is maximum in helixchanger as compared to segmental baffle heat exchanger. The Helixchanger eliminates principle shortcomings caused by shell side zigzag flow induced by conventional baffle arrangement. The flow pattern in the shell side of the heat exchanger with continuous helical baffle was forced to rotational & helical due to geometry of continuous helical baffles, which results in significance increase in heat transfer coefficient per unit pressure drop in the heat exchanger. Keywords: Bell-Delaware method, helical baffles, helix angle, heat transfer coefficient per unit pressure drop, shell & tube heat exchanger. 1) Introduction: 1.1) Introduction Conventional heat exchangers with segmental baffles in shell side have some shortcomings resulting in the relatively low conversion of pressure drop into a useful heat transfer. Both hydrodynamic studies and testing of heat transfer and the pressure drop on research facilities and industrial equipment showed much better performance of helically baffled heat exchanger when compared with conventional ones. These results in relatively high value of shell side heat transfer coefficient, low pressure drop, and low shell side fouling 1. ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 27

Figure - 1.1.1: Helixchanger 1.2) Desirable Features of Heat Exchangers: In order to obtain maximum heat exchanger performance at the lowest possible operating and capital costs without comprising the reliability, the following features are required of an exchange. 1.2.1) Higher heat transfer coefficient and larger heat transfer area: A high heat transfer coefficient can be obtained by using heat transfer surfaces, which promote local turbulence for single phase flow or have some special features for two phase flow. Heat transfer area can be increased by using larger exchangers, but the more cost effective way is to use a heat exchanger having a large area density per unit exchanger volume. 1.2.2) Lower pressure drop: Pumping costs are dependent on pressure drop within an exchanger. Therefore the lower pressure drop means lower operating costs. 1.3) Developments in shell and tube exchanger: The developments for shell and tube exchangers centre on better conversion of pressure drop into heat transfer by improving the conventional baffle designs. With single segmental baffles, a significant proportion of the overall pressure drop is wasted in changing the direction of flow, this baffle arrangement also leads to other undesirable effects such as dead spots or zones of recirculation which can cause increased fouling, high leakage flow, which bypass the heat transfer surface, and large cross flow. The cross flow not only reduces the mean temperature difference but can also cause potentially damaging tube vibration 2. 1.3.1) Helical baffle Heat Exchanger or Helixchanger: Figure 1.3.1: Helical baffle heat exchanger The baffles are of primary importance in improving mixing levels and consequently enhancing heat transfer of shell-and-tube heat exchangers. However, the segmental baffles have some adverse effects such as large back mixing, fouling, high leakage flow, and large cross flow, but the main shortcomings of segmental baffle design remain 3. ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 28

Compared to the conventional segmental baffled shell and tube exchanger Helixchanger offers the following general advantages 4. Increased het transfer rate/ pressure drop ratio. Reduced bypass effects. Reduced shell side fouling. Prevention of flow induced vibration. Reduced maintenance. 1.3.2) Research aspects Research on the helixchanger has forced on two principle areas. Hydrodynamic studies on the shell side and Heat transfer and pressure drop studies on small scale and full industrial scale equipment. 1.3.3) Design aspects: An optimally designed helical baffle arrangement depends largely on the heat exchanger operating conditions and can be accomplished by appropriate design of helix angle, baffle overlapping, and tube layout. In the original method an ideal shell-side heat transfer coefficient is multiplied by various correction factors for flow distribution and the non-idealities such as leakage streams, bypass stream etc. for helical baffle geometry it is suggested that some correction factor are not required; at the same time new are introduced by 4. Figure 1.3.2 Helixchanger pitch 1.3.4) Important Parameters: Pressure Drop( P S ) Baffles pitch(helix angle) angle (α) Baffle space (B) Surface area (A) Heat transfer coefficient (h o ) In designing of helixchanger s, pitch angle, baffle s arrangement, and the space between two baffles with the same position are important parameters. Baffles pitch angle (α) is the angle between flow and perpendicular surface on exchanger axis and B is space between two following baffles with the same situation. Optimum design of helical baffle heat exchangers is depended on operating condition of heat exchanger, and it can be followed and completed by consideration of proper design of pitch angle, overlapping of baffles and tube s layout. Changing the pitch angle in helical baffle system can create wide range of flow velocities as the baffle space and baffle cut in traditional heat exchangers. Moreover, overlapping of helical baffles is a parameter that can affect significantly on shell side flow pattern. ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 29

2) Heat transfer coefficients and pressure drop calculations Heat transfer coefficients and pressure drop calculations are the main part of design of heat exchangers with a given duty. In traditional approaches such as Kern and Bell Delaware methods are used to calculate the overall heat transfer coefficient, heat transfer coefficient & pressure drop. The Kern (1950) method, which was an attempt to correlate data for standard exchangers by a simple equation analogous to equations for flow in tubes. However, this method is restricted to a fixed baffle cut (25%) and cannot adequately account for baffle-to-shell leakages. Nevertheless, although the Kern equation is not particularly accurate, it does allow a simple & rapid calculation of shell side coefficients and pressure drop to be carried out and has been successfully used since its inception. The next stage of development of shell side calculation methods was that commonly described as Bell-Delaware method (Bell-1963). In this method, correction factors for baffle leakage effects, etc., are introduced based on experimental data.this method is widely used and is the basis of the approach recommended, in the Heat exchanger design handbook [5,6,7] 2.1) Thermal analysis of Segmental baffle heat exchanger & Helixchanger In the present work, Bell Delaware method has been used for comparing the thermal performance of Segmental baffle heat exchanger & Helixchanger.Firstly,thermal parameters have been calculated for Segmental baffle heat exchanger using various steps mentioned by Bell-Delaware. Then, suitable modifications have been carried out in different steps for calculating the thermal parameters of Helixchanger.Then comparative analysis has been done between the two heat exchangers. Following data has been assumed and the geometrical parameters are kept constant for both types of heat exchangers. ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 30

Table2.1 Input Data. Sr.no Parameter Shell side Tube side 1 Fluid Water Water 2 Volume flow rate ( 60(lpm) 10(lpm) 3 Mass flow rate ( ) 1Kg/s 0.17Kg/s 4 Shell ID ( 0.153 m 5 Shell length 1.123m 6 Tube pitch 0.0225 m 7 No of passes 1 8 Baffle cut 25% =0.25 9 Baffle pitch 0.060 m 10 Nozzle ID 0.023 m 0.023 m 11 No of baffles 17 12 Mean Bulk Temperature C C 13 Tube OD 0.012 m 14 Tube thickness 0.0014 m 15 No of tube 24 16 Helix angle 25 0 17 No of baffles for Helixchanger 5 Fluid property: Table2.2:Fluid properties Property Unit Cold Water (Shell Side) Hot Water (Tube Side) Cp kj/kg. K 4.178 4.178 K W/m. K 0.6150 0.6150 µ Kg.s/m 2 0.001 0.001 Sp Gr. 0.996 0.996 Pr 5.42 5.42 1 kg/m3 996 996 ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 31

Leakage and bypass clearances: i) Tube to baffle clearance ( ) = 0.0004 m. ii) Baffle to shell clearance ( ) = 0.001 m iii) Shell to bundle clearance = 0.01428 m. iv) Shell outer tube limit = 0.1387 m v) Shell central tube limit =. 1) Cross flow area: Area between central baffle spaces = 0.1267 m 2.1.1 = 0.004405m 2 2) Reynolds number 2.1.2 Re = 3) Heat transfer coefficient: h o = h ideal (J c J L J B ) 2.1.3 4) Window flow area: Area between the baffle cut & shell wall. S w = 2.1.4 5) Shell side pressure drop 2.1.5 ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 32

2.2) Thermal analysis of Helixchanger 1) Cross flow area: 2.2.1 In helixchanger baffles covers half of the shell diameter so cross flow area reduces to half. 2) Reynolds number: Re = 2.2.2 3) Heat transfer coefficient: h o = h ideal (J c J L J B ) 2.2.3 4) Window flow area: As the helical baffle runs over the diameter window area does not exists. From geometry Window flow area, 2.2.4 5) Shell side pressure drop: 2.2.5 ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 33

3)Summary SheetTable 2.3 Sr.No. Parameter Segmental baffle Heat Exchanger Helixchanger (25 deg) 1 S m (m 2 ) 0.004405 0.008224 2 S sb (m 2 ) 0.00032 0.00016 3 S tb (m 2 ) 0.0003012 0.00027143 4 F bp (m 2 ) 0.195 0.1947 5 R e 2725 1459 6 h O (W/m 2.k) 2570.82 1639.65 7 P C (Pa) 112.22 95.83 8 P W (Pa) 102.24 0.1719 9 P S (Pa) 2209.6 420.5 10 h O / P s 1.16 3.90 Table 2.4 m Kg/s Ps (Seg.) Ps( Helix.) 0.333 171.04 50.21 0.667 642.59 82.32 1 2209.59 420 1.33 3395.37 500.25 1.667 4951.12 600.01 ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 34

Table 2.5 m Kg/s ho(seg.) ho(helix.) 0.333 1256.313654 848.0710607 0.667 1974.66215 1332.990228 1 2570.318155 1735.086168 1.33 3094.669695 2089.048227 1.667 3584.816743 2419.920637 Table 2.6 m Kg/s ho/ Ps(Seg.) ho/ Ps(Helix.) 0.333 7.345017281 98.19264199 0.667 3.072939033 55.21283866 1 1.163255249 4.131157544 1.33 0.911435811 4.85825169 1.667 0.724041466 5.287808639 ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 35

4) Conclusion The pressure drop in window flow region for helical baffle STHX reduces drastically as compared to conventional due to negligible window flow area. The pressure drop in cross flow region for helical baffle STHX decreases appreciably as compared to conventional due to baffle geometry. Helical baffle heat exchanger has better heat transfer coefficient per unit pressure drop as compared to segmental baffle heat exchanger. Bell Delaware method available in the literature is only for the segmental baffle heat exchanger since helical baffle heat exchanger is the recent development. Suitable modifications in Bell Delaware method can give the preliminary results. Suitable helix angle can be selected based upon the requirement and industrial applications. Nomenclature Symbol Quantity A Area (m 2 ) B Baffle spacing (m) Bc Baffle cut (%) C P Heat capacity at constant pressure (kj/kg k) D ctl D o D otl D s F c H ho h ideal J B Central tube limit diameter (m) Outside diameter of tube (m) Outer tube limit diameter (m) Inside diameter of shell (m) Fraction of tubes in cross flow between baffle tips Heat-transfer coefficient (W/m 2.k) Shell-side heat-transfer coefficient (W/m 2.k) Ideal tube bank heat-transfer coefficient (W/m 2.k) Heat-transfer correction factor for bundle bypass effects ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 36

J C J L N c N cw window N ss n b n t m Heat-transfer correction factor for effect of baffle window flow Heat-transfer correction factor for baffle leakage effects Number of tube rows crossed in flow between two baffle tips Effective number of tube rows crossed in flow through one baffle Number of pairs of sealing strips Number of baffles Number of tubes in bundle Mass flow rate (Kg/s) P Pressure (kg/m 2 ) Pr Prandtl number P T Tube pitch (m) P T Tube pitch parallel to flow direction (m) R B Re R L Pressure-drop correction factor for bundle bypass effects Shell-side Reynolds number Pressure-drop correction factor for baffle leakage effects F bp Bundle bypass flow area (m 2 ) S m Cross-flow area (m 2 ) S sb Shell-to-baffle leakage area (m 2 ) S tb Tube-to-baffle leakage area (m 2 ) S w Window flow area (m 2 ) Greek Letters P C Cross flow pressure drop (Pa) P o ( P S ) Total shell-side pressure drop (Pa) P w Pressure drop in one baffle window, uncorrected for baffle leakage Effects (Pa) δ sb Shell-to-baffle clearance (m) δ tb Tube-to-baffle clearance (m) μ Viscosity (kg.s/m 2 ) ρ Fluid density (kg/m 3 ) Maximum intertube velocity (m/s) V max Helix angle (degree) Acknowledgement: The authors would like to acknowledge BCUD, University of Pune for providing necessary financial support. ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 37

References [1] Andrews Malcolm, Master Bashir, Three Dimensional Modeling of a Helixchanger Heat exchanger using CFD, Heat Transfer Engineering, 26(6), pp.22-31, (2005) [2] Mukherjee R.,Effectively design Shell and Tube Heat exchangers, Chemical Engg Progress, pp. 1-8, (1998) [3] Gang Yong Lei,Ya-Ling He,RuiLi,Ya-Fu Gao, Effects of baffle inclination angle on flow and heat transfer of a heat exchanger with helical baffles,sciencedirect-chemical Engineering and Processing, pp.1-10(2008) [4] Peng B, Wang Q.W., Zhang C., An experimental Study of shell and tube heat exchangers with continuous Helical baffles,asme Journal of Heat transfer,(2007). [5] Hewitt G.F., Shires G.L., Bott T.B. CRC press Process heat transfer pp 275-285 [6] Serth Robert W 2007 Process heat transfer principles and application, ISBN:0123735882 pp. 246-270 [7] Prithiviraj, M., and Andrews, M. J., Three Dimensional Numerical Simulation of Shell-and-Tube Heat Exchangers, Part 1: Foundation and Fluid Mechanics, Numerical Heat Transfer Part AApplications, vol. 33, no. 8, pp. 799 816, 1998. [8] Master B.I, Chunagad K.S. Boxma A.J. Kral D, StehlikP, Most Frequently used Heat exchangers from pioneering Research to Worldwide Applications, vol. No.6, pp. 1-8, (2006) [9] Wadekar Vishwas,Enhanced and Compact Heat exchangers A Perspective from process industry, 5th international conference on Enhanced and Compact Heat exchangers: Science, Engineering and Technology, pp. 35-41, (2005) [10] Wang Qui, Dong Chen Gui, Xu Jing, PengJi Yan, Second-Law Thermodynamic Comparison and Maximal Velocity Ratio Design Of Shell-and-Tube Heat Exchanger With Continuous Helical Baffles, ASME, Vol.132/101801, pp. 1-8, (2010). ISSN : 2249-913X Vol. 2 No. 1 Mar-May 2012 38