Introduction & Context

In process engineering, batch retorts represent a significant source of intermittent thermal waste. The cooling phase of a retort cycle typically discharges large volumes of water at elevated temperatures. Recovering this thermal energy is a critical strategy for improving plant energy efficiency, specifically by preheating boiler feed water. This calculation methodology provides a standardized approach to sizing liquid-to-liquid heat exchangers for such applications, ensuring that the recovery system operates within thermodynamic limits and practical design constraints.

Methodology & Formulas

The calculation relies on steady-state energy balance and the Logarithmic Mean Temperature Difference (LMTD) method for heat exchanger design. The process follows these sequential steps:

  1. Recovered Heat Duty: The thermal energy extracted from the hot cooling water stream is determined by the sensible heat equation:
  2. \[ Q_{rec} = \dot{m}_h \cdot c_p \cdot (T_{h,in} - T_{h,out}) \]

  3. Cold Side Outlet Temperature: Assuming an adiabatic system where all heat lost by the hot stream is gained by the cold stream, the outlet temperature of the feed water is calculated as:
  4. \[ T_{c,out} = T_{c,in} + \frac{Q_{rec}}{\dot{m}_c \cdot c_p} \]

  5. Logarithmic Mean Temperature Difference (LMTD): The driving force for heat transfer is calculated based on the temperature differences at the exchanger terminals:
  6. \[ \Delta T_1 = T_{h,in} - T_{c,out} \] \[ \Delta T_2 = T_{h,out} - T_{c,in} \] \[ \Delta T_{lm} = \frac{\Delta T_1 - \Delta T_2}{\ln(\frac{\Delta T_1}{\Delta T_2})} \]

    Note: In cases where \(\Delta T_1 \approx \Delta T_2\), the LMTD is taken as \(\Delta T_1\).

  7. Service Heat Transfer Coefficient: To account for real-world fouling, the clean overall heat transfer coefficient is adjusted using the fouling resistance:
  8. \[ U_{service} = \frac{1}{\frac{1}{U_{clean}} + R_{fouling}} \]

  9. Required Heat Exchanger Area: The surface area required to achieve the target heat duty is derived from the fundamental heat transfer equation:
  10. \[ A = \frac{Q_{rec}}{U_{service} \cdot \Delta T_{lm}} \]

Parameter Constraint/Condition
Approach Temperature \(\Delta T_1 \ge 5^\circ C\) and \(\Delta T_2 \ge 5^\circ C\) (Required for feasibility)
Thermodynamic Limit \(T_{c,out} < T_{h,in}\) (Physical impossibility if violated)
Plate Exchanger U \(2000 - 3500 \text{ W/m}^2\cdot K\)
Shell-and-Tube U \(800 - 1500 \text{ W/m}^2\cdot K\)
Flow Velocity \(1.0 - 3.0 \text{ m/s}\) (To maintain turbulence and minimize fouling)