5.3.9Combustion Chemistry (Propulsion Bridge)

Pollutants — NOₓ, soot, unburned hydrocarbons

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1. NOₓ — nitrogen oxides

WHAT are the routes?

There are three mechanisms (you must know all three for the 80/20):

Route WHAT triggers it WHERE it matters
Thermal (Zeldovich) High temperature (>1800>1800 K) Hot lean flames, gas turbines
Prompt (Fenimore) Fuel radicals (CH) attacking N₂ Rich flame fronts
Fuel NOₓ Nitrogen bound in the fuel Coal, heavy oils

HOW thermal NOₓ forms — the Zeldovich derivation

The extended Zeldovich chain: O+N2NO+N(1)\text{O} + \text{N}_2 \rightleftharpoons \text{NO} + \text{N} \quad (1) N+O2NO+O(2)\text{N} + \text{O}_2 \rightleftharpoons \text{NO} + \text{O} \quad (2) N+OHNO+H(3)\text{N} + \text{OH} \rightleftharpoons \text{NO} + \text{H} \quad (3)

Derivation of the NO production rate from first principles.

WHY start with (1)? Reaction (1) is the rate-limiting step — it has the huge activation energy (must break N≡N). Reactions (2),(3) are fast.

Step 1 — write the rate of (1): d[NO]dt=k1[O][N2]\frac{d[\text{NO}]}{dt} = k_1[\text{O}][\text{N}_2] Why this step? Law of mass action: rate ∝ product of reactant concentrations.

Step 2 — invoke the quasi-steady-state for the N atom. N is consumed as fast as made: d[N]dt0\frac{d[\text{N}]}{dt}\approx 0 Why? N atoms are extremely reactive — their concentration is tiny and constant. This lets us eliminate the unknown [N].

Step 3 — combine. Both (1) and (2) make one NO, so accounting for the steady N: d[NO]dt=2k1[O][N2]\boxed{\frac{d[\text{NO}]}{dt} = 2\,k_1[\text{O}][\text{N}_2]} Why the factor 2? One NO from (1), then the N atom immediately makes a second NO via (2).

Step 4 — the temperature law. k1k_1 obeys Arrhenius: k1=Aexp ⁣(EaRT),Ea319 kJ/molk_1 = A\exp\!\left(-\frac{E_a}{RT}\right),\qquad E_a \approx 319\text{ kJ/mol} Why this matters: that giant EaE_a is why NOₓ roughly doubles for every ~7070 K rise near 20002000 K. Temperature, not residence time, dominates.


2. Soot — particulate carbon

HOW soot forms (the pathway you must recall)

  1. Pyrolysis: fuel cracks (no O₂) into small radicals, esp. C₂H₂ (acetylene).
  2. Aromatic ring formation: first benzene ring builds (the rate-controlling step).
  3. PAH growth by the HACA mechanism (H-Abstraction C₂H₂-Addition): a ring loses an H, then adds an acetylene unit, repeating to grow.
  4. Nucleation → tiny particles; surface growth + coagulation → visible soot.
  5. Oxidation: if soot then meets O₂/OH at high T, it can burn off. Net soot = formation − oxidation.

3. Unburned hydrocarbons (UHC) and CO

WHY does fuel escape unburned?

  • Wall quenching: cold walls extract heat; reactions freeze in a thin quench layer.
  • Crevices: fuel hides in gaps (e.g. piston ring crevice) too narrow for the flame.
  • Over-lean (flame-out) or over-rich local mixtures: outside the flammability limits.
  • Low temperature: COCO2\text{CO}\to\text{CO}_2 needs OH and time; if gases cool fast, CO is frozen in.

4. The master trade-off (THE 80/20 idea)

Figure — Pollutants — NOₓ, soot, unburned hydrocarbons

Common mistakes (Steel-man + fix)


Flashcards

What two species make up NOₓ?
NO and NO₂.
Where does the nitrogen in thermal NOₓ come from?
From N₂ in the air, not the fuel.
Name the three NOₓ formation routes.
Thermal (Zeldovich), Prompt (Fenimore), Fuel NOₓ.
What is the rate-limiting step of thermal NOₓ?
O + N₂ → NO + N (breaking the strong N≡N bond).
Why is NOₓ exponentially sensitive to temperature?
The rate-limiting step has a huge activation energy (~319 kJ/mol), so k₁ ∝ exp(−Eₐ/RT).
Roughly how much T rise doubles thermal NOₓ near 2000 K?
About a 70 K rise (because of the ~319 kJ/mol activation energy).
What factor of 2 appears in d[NO]/dt and why?
Each O+N₂ event ultimately makes 2 NO molecules (one directly, one from the leftover N via N+O₂→NO+O).
Under what conditions does soot form?
Hot AND fuel-rich (oxygen-starved) zones.
What is the key soot precursor molecule?
Acetylene, C₂H₂.
What does HACA stand for?
H-Abstraction, C₂H₂-Addition — the PAH/soot growth mechanism.
Net soot = ?
Formation minus oxidation (soot can burn off if it meets O₂/OH at high T).
Two main causes of unburned hydrocarbons?
Wall/quench-layer cooling and crevices (plus over-lean/over-rich local mixtures).
What single reaction dominates CO burnout?
CO + OH → CO₂ + H.
Why does lowering peak temperature raise CO and UHC?
Burnout of CO→CO₂ and finishing fuel oxidation are slow and need hot gas + radicals; cooling freezes them.
Where on the φ axis does NOₓ peak?
Slightly lean of stoichiometric (highest T with plenty of O).
Where does soot appear on the φ axis?
Only on the rich side (φ > 1), growing with richness.
The central pollutant trade-off in one line?
Cutting temperature lowers NOₓ but raises CO/UHC; you can't minimise both at once.

Recall Feynman: explain to a 12-year-old

Imagine a campfire. If the fire is super hot, even the air (which usually doesn't burn) gets cooked and makes a smelly gas — that's NOₓ. If you pile on too much wood and not enough air, black smoke comes off — that's soot, carbon clumping up because it can't find air. If part of the fire is too cold (like near a cold pot), some wood smoke escapes without burning — that's unburned fuel and CO. So: too hot → NOₓ, too much fuel → soot, too cold → smoke. The trick is finding the "just right" middle.


Connections

  • Adiabatic Flame Temperature — sets peak T that drives thermal NOₓ.
  • Equivalence Ratio and Flammability Limits — the φ axis underlying all three pollutants.
  • Arrhenius Equation and Activation Energy — why NOₓ is exp-sensitive to T.
  • Lean Premixed Combustion & Staging — engineering fix for NOₓ.
  • Diffusion vs Premixed Flames — diffusion flames sit at φ≈1 internally → more soot.
  • CO Oxidation and Chemical Kinetics — CO+OH burnout.
  • Quenching and Wall Heat Transfer — origin of UHC.

Concept Map

too hot

too rich

too cold quenched

thermal route

prompt route

fuel route

rate-limited by

steady-state N gives

k1 follows

large Ea 319 kJ/mol

drives

Non-uniform T and mixing

NOx = NO + NO2

Soot

UHC and CO

Zeldovich mechanism

Fenimore CH radicals

Fuel-bound nitrogen

O + N2 breaks N triple bond

d NO dt = 2 k1 O N2

Arrhenius exp -Ea/RT

Exponential T sensitivity

Hinglish (regional understanding)

Intuition Hinglish mein samjho

Dekho, combustor ka kaam hai fuel + air ko CO₂ + H₂O + heat me badalna. Pollutants asal me side-reactions hain jo isliye hoti hain kyunki real combustion uneven hota hai — kahi bahut garam, kahi bahut rich (fuel zyada), kahi bahut thanda. Teen main villains: NOₓ (jab flame bahut HOT ho, to air ka N₂ tak oxidise ho jata hai), soot (jab zone bahut RICH ho, carbon ko oxygen nahi milta to wo clump ban jata hai), aur UHC + CO (jab zone bahut COLD ho ya quench ho jaye, fuel poora jal hi nahi pata).

NOₓ ka asli funda: N≡N bond bahut strong hai (945 kJ/mol), isliye sirf bahut energetic, garam collision hi use todta hai — Zeldovich mechanism. Rate me eEa/RTe^{-E_a/RT} aata hai, matlab temperature thoda badao to NOₓ exponentially badh jata hai (roughly har ~70 K rise pe double, 2000 K ke aas-paas). Isliye sabse important cheez hai peak temperature ko control karna, residence time secondary hai. Yahi reason hai ki lean-premixed aur staged combustion use karte hain — taaki flame ka peak T neeche rahe. Ek chhota example: 2200 K se 2000 K pe le jao to NOₓ rate ka factor e1.740.18e^{-1.74}\approx0.18 ban jata hai — yani lagbhag 5 guna kam, sirf 200 K cut se.

Soot ka funda ulta hai: ye RICH, oxygen-starved aur hot zone me banta hai. Fuel crack hoke acetylene (C₂H₂) banata hai, fir HACA mechanism se PAH rings badhti hain, fir solid particle. Lekin agar baad me O₂/OH mile to soot jal bhi sakta hai — isliye net soot = formation minus oxidation.

Sabse important exam point: ek trade-off hota hai. Temperature kam karoge to NOₓ girega par CO/UHC badhega (incomplete burn). Dono ko ek saath minimum nahi kar sakte. Diagram me dekho — φ (equivalence ratio) ke against NOₓ slightly lean pe peak karta hai, soot sirf rich side pe, aur CO/UHC dono extremes pe high. Yahi ek graph poora chapter samjha deta hai.

Go deeper — visual, from zero

Test yourself — Combustion Chemistry (Propulsion Bridge)

Connections