5.4.10 · D4Materials Chemistry (Aerospace)

Exercises — Surface treatments — anodising, plasma spraying, vapour deposition

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Constants you may reuse throughout:


Level 1 — Recognition

Exercise 1.1 (L1)

State, in one word each, which electrode the aluminium part becomes during anodising, and what gas evolves at the other electrode.

Recall Solution 1.1

The part is the anode (it is oxidised to grow — "anodising"). At the cathode only hydrogen () is released. WHAT this checks: you can name the electrode from the process name, not from the "metal = cathode" reflex.

Exercise 1.2 (L1)

Rank the three processes — anodising, plasma spraying, vapour deposition — from thickest to thinnest typical coating.

Recall Solution 1.2

Thickest → thinnest:

  1. Plasma spraying.
  2. Anodising.
  3. Vapour deposition. WHY: plasma spraying stacks molten splats (bulk-like build-up), anodising grows oxide from the metal, and vapour deposition adds one atom at a time (slowest, thinnest).

Exercise 1.3 (L1)

In one word, what is the essential difference between PVD and CVD?

Recall Solution 1.3

Reaction. In CVD a gas precursor chemically reacts/decomposes on the hot surface; in PVD the material is only physically evaporated or sputtered — no chemical change.


Level 2 — Application

Exercise 2.1 (L2)

Anodise an area at for with efficiency . Oxide molar mass , density . Find the oxide thickness .

Recall Solution 2.1

WHAT: plug straight into . Numerator . Denominator . WHY the 6: the half-reaction releases 6 electrons per mole of , so 6 mol of charge (per ) builds only 1 mol of oxide.

Exercise 2.2 (L2)

A sputter source delivers of titanium, , film density . Find the growth rate in m/s and in µm/hr.

Recall Solution 2.2

Numerator . Denominator . Convert: . WHY divide by : is mass arriving per area per second; dividing by density turns mass-per-area into thickness.

Exercise 2.3 (L2)

How much energy (per kg) is needed to melt an alumina () spray particle from to ? Use , .

Recall Solution 2.3

Two terms — first heat, then melt. Heating: . Fusion: . WHY per kg: so we can compare against plasma enthalpy flux () without knowing particle size.


Level 3 — Analysis

Exercise 3.1 (L3)

Two anodising runs use the same total charge . Run A: for . Run B: for . Both use , same , , . Do they give the same thickness? Explain what the formula says and what practical caveat the formula hides.

Recall Solution 3.1

; . Since (with all else equal), the formula predicts identical thickness. WHAT the formula hides: is not truly constant. High current density () heats the bath and dissolves oxide, lowering ; low current for long may passivate cleanly with higher . So in reality Run B often gives a slightly thicker, better-quality film despite equal charge. Lesson: the equation is exact only in charge; real efficiency depends on current density and temperature.

Exercise 3.2 (L3)

A plasma-spray droplet is molten but the coating on the part still peels off. Using the parent note, name the true bonding mechanism and identify which surface-prep step was likely skipped, and why that step matters.

Recall Solution 3.2

Bonding is mostly mechanical interlocking (with minor local fusion), not a metallurgical weld. The skipped step is grit-blasting to roughen the surface. See Adhesion and Surface Roughness. WHY roughness matters: interlocking needs peaks and valleys for splats to hook into. A smooth surface gives no anchor points, so splats solidify and shrink, then pop off. More surface roughness → more contact area and mechanical keying → stronger adhesion.

Exercise 3.3 (L3)

For the same 5 µm coating on a turbine part, argue why PVD (TiN, wear resistance) but plasma spray (YSZ, heat shielding) are used — connect each to the physics that makes the other impractical.

Recall Solution 3.3
  • PVD for thin hard films: atom-by-atom deposition gives a smooth, dense, defect-free layer — ideal for a thin wear/diffusion barrier. Plasma spraying can't make a clean sub-10 µm layer because splats are tens of µm across (too coarse).
  • Plasma spray for thick heat shields: yttria-stabilised zirconia melts at ~2700 °C; only a plasma jet () can melt it and lay down fast. PVD at ~ would take hundreds of hours for the same thickness — utterly impractical. See Thermal Barrier Coatings. Rule: thickness need decides the process; PVD wins thin-and-smooth, plasma wins thick-and-refractory.

Level 4 — Synthesis

Exercise 4.1 (L4)

You must protect an aluminium bracket, area , with a anodic layer. Your rectifier gives at . (a) Find the time. (b) If you then need to make the surface harder still with a TiN top layer by PVD at , find that time. (c) Which step dominates the schedule, and what does that tell you about combining processes?

Recall Solution 4.1

(a) Rearrange for time: . Use , , . Numerator . ; ; ; . Denominator . (b) . (c) PVD (~95 min) dwarfs anodising (~10 min). Lesson: atom-by-atom PVD is the bottleneck; combine processes so each does what it's fastest at — thick protection by anodising, only the very thinnest ultra-hard skin by PVD.

Exercise 4.2 (L4)

A YSZ (zirconia) plasma-spray line feeds particles of mass each. Using , , , : (a) energy to fully melt one particle; (b) if the plasma delivers heat to a particle at , minimum in-flight (residence) time to melt it. Connect to Latent Heat and Phase Change.

Recall Solution 4.2

(a) Per kg: . . Times mass: . (b) . WHY the latent term dominates the danger: during melting the temperature stops rising while is absorbed (a phase-change plateau). If residence time is shorter than , the particle arrives partly solid and won't splat properly.


Level 5 — Mastery

Exercise 5.1 (L5)

Design check for an anodised part that must also be sealed and dyed. Given , , , target (, ): (a) find the required time; (b) the charge ; (c) the number of moles of grown; (d) explain, using porosity, why dyeing must precede sealing. Link to Corrosion and Passivation.

Recall Solution 5.1

(a) . Numerator . ; ; . Denominator . (b) . (c) Effective charge building oxide . Moles of oxide . (d) Anodic oxide is porous before sealing. Dye soaks into the open pores; sealing (hot water/steam hydrates the to boehmite, closing pores). So you must dye first, then seal — seal first and the dye can't get in, and the sealed passive layer is what resists corrosion. See Corrosion and Passivation.

Exercise 5.2 (L5)

A hybrid aerospace panel needs: (i) anodised base , (ii) plasma-sprayed YSZ TBC , (iii) PVD TiN wear cap . Using rates/values from earlier exercises ( from , , scaled; PVD ; assume plasma deposits at ), estimate the total process time and state which step you would try hardest to speed up.

Recall Solution 5.2

Anodising (20 µm): from Ex 4.1a a 15 µm layer took ; thickness , so takes . Plasma spray (300 µm at 50 µm/min): . PVD (3 µm at 1.27 µm/hr): . Total . Which to speed up: PVD dominates (~142 of ~161 min). It is the atom-by-atom step — increasing flux (higher sputter power) is the biggest lever. Insight: thickness-per-time varies by four orders of magnitude across these processes, so the thinnest layer can still cost the most time.


Recall Final self-check (open after all solutions)

Which process is fastest per micron? ::: Plasma spraying (tens of µm per minute) Which is slowest per micron? ::: PVD / vapour deposition (~µm per hour) In anodising, thickness depends on charge divided by what factor times F? ::: 6 (electrons per mole of oxide) Why dye before sealing? ::: sealing closes the pores the dye needs to enter

Connections

  • Parent topic
  • Faraday's Laws of Electrolysis — the charge → thickness link used in L2/L4/L5
  • Latent Heat and Phase Change — the melting-plateau term in plasma problems
  • Thermal Barrier Coatings — the YSZ layer sized in L3/L5
  • Adhesion and Surface Roughness — why grit-blasting matters (L3)
  • Corrosion and Passivation — sealing the porous anodic oxide (L5)
  • Aluminium Alloys in Aerospace — the substrate protected throughout