Lesson 13 of 15

Combustion

Reacting mixtures: balancing combustion equations, air–fuel ratios and excess air, enthalpy of formation, heating values, the adiabatic flame temperature — and how much CO₂ each kilowatt-hour of heat costs.

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The question

The combustor of our gas turbine burns natural gas in compressed air at a rate of tens of kilograms a second. Its walls must survive, the turbine blades downstream must survive, and every percent of fuel energy counts. Everything starts with two questions: how much air does the fuel need, and how hot can a flame get?

Counting atoms

A chemical reaction rearranges atoms; it never creates or destroys them. So a combustion equation is balanced by conserving each element. For methane burning completely in air — which we model as 21% oxygen and 79% nitrogen by moles, or 3.76 moles of N₂ for every mole of O₂:

CH4+2 (O2+3.76 N2)→CO2+2 H2O+7.52 N2.\mathrm{CH_4} + 2\,(\mathrm{O_2} + 3.76\,\mathrm{N_2}) \rightarrow \mathrm{CO_2} + 2\,\mathrm{H_2O} + 7.52\,\mathrm{N_2}.

That is the theoretical or Stoichiometric (theoretical) airExactly enough air to burn all the fuel completely, with no oxygen left over. amount of air: exactly enough oxygen for complete combustion. Engineers describe mixtures by the air–fuel ratio (17.2 kg of air per kg of methane at stoichiometric), the percent of theoretical air, or the equivalence ratio φ\varphi — actual fuel–air ratio divided by stoichiometric — below 1 for lean mixtures with excess air, above 1 for rich ones.

CalculatorBalancing the books of a flame
CH₄ + 2.00 (O₂ + 3.76 N₂) →7.52 N₂ + CO₂ + 2 H₂ON₂ 71.5%CO₂ 9.5%H₂O 19.0%products by mole fraction · water vapour condenses below 59 °C
0% · 100% theoretical air
Air–fuel ratio17.2 kg/kgmethane (natural gas)
Heating value50.0 MJ/kglower · higher 55.5
CO₂ per kWh of heat197 g
Challenges0/3
  • Find the fuel whose higher and lower heating values differ the most, in percent.
  • Find how many kilograms of air it takes to burn a kilogram of petrol at stoichiometric.
  • Compare the CO₂ per kWh of coal and natural gas.
Complete combustion of a fuel in air (21% O₂, 79% N₂ by moles, counted as 3.76 mol N₂ per mol O₂). Atoms are conserved: every carbon atom ends in CO₂, every hydrogen in H₂O. The bar shows the product composition by moles; most of it is nitrogen just along for the ride.

Notice how much of the product gas is nitrogen, carried through the flame unchanged. It absorbs a large share of the heat — which is why the flame temperature depends so strongly on how much excess air you use. Notice, too, the dew point of the products: around 55–60 °C for natural gas. Cool the exhaust below it, and the water vapour condenses, releasing its latent heat. That is the trick of a condensing boiler, and the difference between the two heating values below.

Energy in chemical bonds

Up to now, every enthalpy had an arbitrary zero for each substance — fine, as long as the substance didn't change. With chemical reactions, substances do change, so all enthalpies need a common reference. The convention: elements in their stable form at 25 °C and 1 atm have zero enthalpy. The enthalpy of a compound at that state is its enthalpy of formation, hˉf∘\bar h_f^\circ, the heat released or absorbed when it is formed from its elements. CO₂'s is −393 520 kJ/kmol: forming it releases a lot of energy. At any other temperature,

hˉ(T)=hˉf∘+[hˉ(T)−hˉ(Tref)].\bar h(T) = \bar h_f^\circ + \left[\bar h(T) - \bar h(T_\text{ref})\right].

The energy balance for a reactor in steady state, with no work, then reads

Q˙cvn˙F=∑Pne hˉe−∑Rni hˉi.\frac{\dot Q_\text{cv}}{\dot n_F} = \sum_P n_e\,\bar h_e - \sum_R n_i\,\bar h_i.

Heating values

The heat released when a fuel burns completely, with products cooled back to 25 °C, is its Heating valueThe heat released by complete combustion of a unit of fuel. The higher heating value counts the water in the products as liquid, the lower as vapour.. If the water in the products ends up as liquid, it is the higher heating value (HHV); as vapour, the lower heating value (LHV). The difference is the latent heat of that water: about 10% for natural gas, 18% for hydrogen. Power-plant efficiencies in Europe are usually quoted on the LHV, in the United States on the HHV — always check which.

Estimate first
How many grams of CO₂ does burning coal (as pure carbon) emit per kWh of heat?
1101001,00010,000100,000
Drag along the line to place your guess — each tick is ten times the last.

The adiabatic flame temperature

If a combustor lost no heat and burned completely, all the chemical energy would go into heating the products. The temperature they would reach is the Adiabatic flame temperatureThe temperature the products reach if all the chemical energy goes into heating them., found by setting the products' total enthalpy equal to the reactants':

∑Pne hˉe(Tad)=∑Rni hˉi(Tin).\sum_P n_e\,\bar h_e(T_\text{ad}) = \sum_R n_i\,\bar h_i(T_\text{in}).

With temperature-dependent heat capacities this needs a numerical solution — which the widget below does for five fuels:

ExploreHow hot can a flame get?
0.40.60.811.21.41.610001500200025003000equivalence ratio φadiabatic flame temperature (K)gas-turbine inlet limitH₂CH₄C₃H₈C₈H₁₈C
1.00 · stoichiometric
298 K
Flame temperature2339 K2066 °C
Challenges0/3
  • Find the excess air that brings natural gas down to a 1800 K turbine inlet temperature.
  • Make a flame hotter than 2900 K (in this complete-combustion model).
  • Use air preheat to raise a methane flame above 2600 K.
The adiabatic flame temperature — the temperature the products would reach if all the chemical energy went into heating them, with no heat loss and complete combustion (no dissociation; Lesson 14 shows why real flames near stoichiometric run around a hundred kelvin cooler). Curves for five fuels against equivalence ratio φ: below 1 is lean (excess air), above 1 rich.

The flame is hottest near stoichiometric and cools on either side: lean mixtures waste heat on excess air, rich ones leave fuel unburned. That gives engineers a powerful lever. A gas turbine can't run its combustor at 2300 K, so it burns lean — or burns near stoichiometric and dilutes with extra air — to bring the gas down to the 1600–1900 K the turbine blades can stand. Preheating the air raises the flame temperature degree for degree, which is how glass furnaces and steel reheating furnaces reach their temperatures.

Check your intuition
Why is the adiabatic flame temperature of methane in pure oxygen much higher (about 3000 K) than in air (about 2200 K)?
Going deeper
Going deeper: the absolute entropy and the Gibbs function of reactions

To apply the second law to reactions, entropies also need a common zero. The third law of thermodynamics provides it: the entropy of a pure crystalline substance is zero at absolute zero. Tables then list absolute entropies sˉ∘(T)\bar s^\circ(T) at 1 atm, and for an ideal-gas component of a mixture, sˉi=sˉi∘(T)−Rˉln⁡(yip/pref)\bar s_i = \bar s_i^\circ(T) - \bar R\ln(y_i p/p_\text{ref}).

Entropy generated by combustion can then be computed directly — and it is enormous, which is the origin of the large combustion exergy destruction of Lesson 7. Combining enthalpy and entropy gives the Gibbs function of formation, gˉf∘\bar g_f^\circ, from which the chemical exergy of a fuel follows: for most hydrocarbons, within a few percent of its higher heating value. A fuel cell, which converts that Gibbs function directly into electricity without burning, can in principle avoid the combustion loss altogether.

Recap
What to carry forward
  • Balance combustion equations by conserving atoms. Air is 3.76 mol N₂ per mol O₂.
  • Describe mixtures by air–fuel ratio, percent theoretical air or equivalence ratio φ.
  • Enthalpies of reacting substances use the enthalpy of formation at 25 °C as their reference.
  • Heating values: HHV with liquid water in the products, LHV with vapour; the difference is the latent heat.
  • The adiabatic flame temperature comes from equating product and reactant enthalpies; it peaks near stoichiometric and rises with air preheat.

Next: real flames never quite reach the adiabatic temperature, and their exhaust always contains traces of CO and NO. Why doesn't burning ever quite finish?

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