Energy Balance Fundamentals

Energy Balance Fundamentals

The First Law of Thermodynamics states that energy can neither be created nor destroyed; it can only change forms. In engineering, we apply this principle using an energy balance across a defined system boundary.

Closed Systems

A closed system can exchange heat and work with its surroundings, but no mass crosses its boundary. For a closed system undergoing a process from state 1 to state 2, the energy balance is:

ΔU+ΔEK+ΔEP=Q−W\Delta U + \Delta E_K + \Delta E_P = Q - W

where:

  • ΔU\Delta U = change in internal energy [J]
  • ΔEK\Delta E_K = change in kinetic energy [J]
  • ΔEP\Delta E_P = change in potential energy [J]
  • QQ = heat transferred to the system [J]
  • WW = work done by the system [J]

(Note: The sign convention Q−WQ - W assumes heat IN is positive and work OUT is positive. Some textbooks use Q+WQ + W with work defined as work done ON the system. Always verify the convention).

Often, changes in kinetic and potential energy are negligible for closed systems, simplifying the equation to ΔU=Q−W\Delta U = Q - W.

Open Systems (Steady-Flow)

An open system involves mass flowing across the system boundaries (e.g., pumps, turbines, heat exchangers). For steady-state open systems, energy entering the system equals energy leaving the system.

Because mass carries energy into and out of the system, we introduce Enthalpy (HH), which combines internal energy and flow work (U+PVU + PV). The macroscopic steady-flow energy balance on a rate basis is:

ΔH˙+ΔE˙K+ΔE˙P=Q˙−W˙s\Delta \dot{H} + \Delta \dot{E}_K + \Delta \dot{E}_P = \dot{Q} - \dot{W}_s

where:

  • ΔH˙\Delta \dot{H} = difference in enthalpy flow rate between outlets and inlets [W or J/s]
  • Q˙\dot{Q} = rate of heat transfer to the system [W]
  • W˙s\dot{W}_s = rate of shaft work done by the system [W]

Worked Example

Problem: Steam flows steadily through an adiabatic turbine (no heat transfer, Q˙=0\dot{Q} = 0). The inlet enthalpy is 3200 kJ/kg3200 \text{ kJ/kg} and the outlet enthalpy is 2400 kJ/kg2400 \text{ kJ/kg}. Changes in kinetic and potential energy are negligible. The mass flow rate of steam is 5 kg/s5 \text{ kg/s}. Calculate the power output (shaft work rate) of the turbine.

Solution:

  1. State the steady-flow energy balance: ΔH˙=Q˙−W˙s\Delta \dot{H} = \dot{Q} - \dot{W}_s
  2. Note that Q˙=0\dot{Q} = 0 (adiabatic). Therefore: W˙s=−ΔH˙\dot{W}_s = -\Delta \dot{H}
  3. Expand ΔH˙\Delta \dot{H} using the mass flow rate m˙\dot{m} and specific enthalpy hh: ΔH˙=m˙(hout−hin)\Delta \dot{H} = \dot{m} (h_{out} - h_{in})
  4. Calculate the work rate: W˙s=−5 kg/s×(2400 kJ/kg−3200 kJ/kg)\dot{W}_s = -5 \text{ kg/s} \times (2400 \text{ kJ/kg} - 3200 \text{ kJ/kg}) W˙s=−5×(−800)=4000 kW=4 MW\dot{W}_s = -5 \times (-800) = 4000 \text{ kW} = 4 \text{ MW}

Engineering Check

In the example above, the positive sign for W˙s\dot{W}_s confirms that 4 MW of power is produced by the system (the turbine), matching our chosen sign convention. If this were a compressor, W˙s\dot{W}_s would be negative, indicating work must be supplied to the system.\n

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