Chapter 11 Heat Exchangers Chapter Objectives ◼ To introduce performance parameters for assessing the efficacy of a H.E. ◼ To develop methodology for designing a H.E. ◼ To predicting the performance of an existing exchanger What is heat exchanger? A device that exchange heat between two fluids that are at different temperature and separated by a solid wall is termed a heat exchanger. Heat exchangers are used in space heating and air-conditioning, power production, waste heat recovery, and chemical processing. Heat Exchanger Types Concentric tube heat exchangers Parallel Flow ➢ Simplest configuration. Counterflow ➢ Superior performance associated with counter flow. Cross-flow heat exchangers Finned-Both Fluids Unmixed Unfinned-One Fluid Mixed the Other Unmixed Heat Exchanger Types One Shell Pass and One Tube Pass Shell-andTube Heat Exchangers ➢ Baffles are used to establish a cross-flow and to induce turbulent mixing of the shell-side fluid, both of which enhance convection. One Shell Pass, Two Tube Passes Two Shell Passes, Four Tube Passes Heat Exchanger Types • Compact Heat Exchangers ➢ Widely used to achieve large heat rates per unit volume, particularly when one or both fluids is a gas. ➢ Characterized by large heat transfer surface areas per unit volume, small flow passages, and laminar flow. (a) (b) (c) (d) (e) Fin-tube (flat tubes, continuous plate fins) Fin-tube (circular tubes, continuous plate fins) Fin-tube (circular tubes, circular fins) Plate-fin (single pass) Plate-fin (multipass) Overall Heat Transfer Coefficient • An essential requirement for heat exchanger design or performance calculations. • Contributing factors include convection and conduction associated with the two fluids and the intermediate solid, as well as the potential use of fins on both sides and the effects of time-dependent surface fouling. • With subscripts c and h used to designate the cold and hot fluids, respectively, the most general expression for the overall coefficient is: 1 = 1 = 1 UA (UA)c (UA)h = Rf ,c Rf ,h 1 1 + + Rw + + (o hA)c (o A)c (o A)h (o hA)h (11.1) Overall Heat Transfer Coefficient 2 ➢ Rf → Fouling factor for a unit surface area (m K/W) → Table 11.1 ➢ Rw → Wall conduction resistance (K/W) ➢ o → Overall surface efficiency of fin array (Section 3.6.5) A o,c or h = 1 − f (1 − f ) A c or h A = At → total surface area (fins and exposed base) A f → surface area of fins only Heat Exchanger Analysis (1) LMTD - The Log Mean Temperature Difference (LMTD) Method • A form of Newton’s law of cooling may be applied to heat exchangers by using a log-mean value of the temperature difference between the two fluids: q = U A T m T m = T1 − T2 1n ( T1 / T2 ) Evaluation of T1 and T2 depends on the heat exchanger type. • Counter-Flow Heat Exchanger: T1 Th ,1 − Tc ,1 = Th ,i − Tc ,o T2 Th ,2 − Tc ,2 = Th ,o − Tc ,i (11.14) (11.15) Heat Exchanger Analysis (1) LMTD • Parallel-Flow Heat Exchanger: T1 Th ,1 − Tc ,1 = Th ,i − Tc ,i T2 Th ,2 − Tc ,2 = Th ,o − Tc ,o 과제: 예제 11.1에서 바깥쪽 환상공간의 직경을 45mm에서 40mm로 줄일 경우, 어떤 변화가 생기겠는가? Heat Exchanger Analysis (2) The Effectiveness-NTU Method General Considerations • Computational Features/Limitations of the LMTD Method: ➢ The LMTD method may be applied to design problems for which the fluid flow rates and inlet temperatures, as well as a desired outlet temperature, are prescribed. For a specified HX type, the required size (surface area), as well as the other outlet temperature, are readily determined. ➢ If the LMTD method is used in performance calculations for which both outlet temperatures must be determined from knowledge of the inlet temperatures, the solution procedure is iterative. ➢ For both design and performance calculations, the effectiveness-NTU method may be used without iteration. Heat Exchanger Analysis (2) The Effectiveness-NTU Method • Heat exchanger effectiveness, : q 0 1 = qmax (11.19) • Maximum possible heat rate: qmax = Cmin (Th,i − Tc,i ) Cmin (11.18) Ch if Ch Cc = or Cc if Cc Ch • Performance Calculations: ➢ = f ( NTU, Cmin / Cmax ) Cr 예제 11.3 예제 11.5 ➢ Relations → Table 11.3 or Figs. 11.10 - 11.15