BS 1490 · Group C · Special Purpose — Limited Application
lm29
Aluminium Alloy
Al-Si23Cu1Mg1Ni1 — Highest Silicon in LM Series — Minimum Thermal Expansion
Sand Casting
Gravity Die Casting
Low Pressure Die Casting
T6 Heat-Treatable
ISO 9001:2015
At a Glance
- Nominal composition
- Si content
- Density
- Best tensile (min)
- Freezing range
- Thermal conductivity
- Hardness
- Al-Si23Cu1Mg1Ni1
- 22.0–25.0 %
- 2.66 g/cm³
- 190 N/mm²
- 575–520 °C
- 109 W/m·K
- 120–145 (TE and TF — mandatory) HB

Overview
Highest Silicon in LM Series — Minimum Thermal Expansion
LM29 has the highest silicon content (22–25%) of any alloy in the BS 1490 LM-series, making it the most extreme hypereutectic piston alloy. At this silicon level, the alloy has the lowest coefficient of thermal expansion (×10⁻⁶/K = 18), the highest wear resistance, and the best retention of strength at very high temperatures — at the cost of extremely difficult machinability and complex casting requirements.
LM29 shares the mandatory metallographic requirements of LM28 and is used almost exclusively for the most demanding piston applications in high-performance aviation and racing engines where LM28 does not provide sufficient wear resistance or where piston-to-bore clearance must be minimised to the absolute minimum.
Most Restrictive Alloy in BS 1490 — Specialist Use Only

Chemical Composition
LM29 Chemical Composition — BS 1490:1988
| ELEMENT | SYMBOL | MIN % | MAX % | ROLE IN ALLOY |
|---|---|---|---|---|
| Silicon | Si | 22.0 | 25.0 | 22–25% Si — the highest silicon content of any LM alloy. Extreme hypereutectic composition with very high primary silicon crystal content. Delivers minimum thermal expansion and maximum wear resistance. |
| Copper | Cu | 0.8 | 1.3 | 0.8–1.3% Cu — contributes to elevated temperature strength. |
| Magnesium | Mg | 0.8 | 1.3 | 0.8–1.3% Mg — contributes to complex precipitation system with Ni. |
| Iron | Fe | — | 0.7 | Controlled to ≤0.7% — relatively tight limit for a complex alloy. |
| Manganese | Mn | — | 0.6 | Impurity limit. Controlled to maintain clean melt. |
| Nickel | Ni | 0.8 | 1.3 | Impurity limit. |
| Zinc | Zn | — | 0.2 | Impurity limit. Higher Zn increases hot-cracking risk. |
| Lead | Pb | — | 0.1 | Impurity limit. |
| Tin | Sn | — | 0.1 | Impurity limit. |
| Titanium | Ti | — | 0.2 | Grain refiner when added as TiB₂ master alloy. |
| Aluminium | Al | — | Remainder | Base metal. Composition verified by OES (ARUN Technology UK, MERLIN-4 ULTRA). |
| Other elements | — | — | 0.05 each / 0.15 total | Each unspecified element ≤0.05%, total ≤0.15%. |

Global Standards
LM29 Equivalent Grades — International Standards
BS 1490
LM29
Group C · Special Purpose — Limited Application Al-Si23Cu1Mg1Ni1
EN 1706
—
EN AC-Al Si23Cu1Ni1Mg
ASTM / AA
—
No ASTM equivalent
JIS H 5302
—
No JIS equivalent
DIN 1725-2
G-AlSi23CuMgNi
Approximate — no current standard
ISO 3522
Al-Si23CuNiMg
ISO casting alloy designation

Mechanical Properties
LM29 Mechanical Properties — BS 1490:1988 Table 4
Minimum values from separately cast test samples per BS 1490:1988. These are guaranteed minimums — not average values. Properties in actual castings vary with section thickness, cooling rate, and local geometry.
| Condition | Process | Tensile N/mm² Min | 0.2% Proof N/mm² | Elongation % Min | Brinell HB |
|---|---|---|---|---|---|
| TE | Chill / GDC | 190 | — | — | 100–140 |
| TF | Chill / GDC | 190 | — | — | 100–140 |

Physical Properties
LM29 Physical & Thermal Properties
Density
2.66 g/cm³
Approx. 1/3 the density of steel
Freezing Range
575–520 °C
Solidification temperature range
Thermal Conductivity
109 W/m·K
Heat dissipation capability
Electrical Conductivity
— % IACS
Relative to copper standard
Linear Expansion
18 ×10⁻⁶/K
20–300°C range
Brinell Hardness
120–145 (TE and TF — mandatory) HB
As-cast or stated condition
| PROPERTY | RATING | NOTES |
|---|---|---|
| Corrosion resistance | Fair (C) | Used in internal engine applications — corrosion resistance is secondary to thermal performance. |
| Decorative anodising | Poor (D) | Not applicable for anodising. |
| Weldability | Poor | Hypereutectic Si — not weldable. |
| Machinability group | 1 — Very Difficult | Group 1 — most difficult to machine of all LM alloys. Diamond tooling mandatory. |

Casting Suitability
LM29 Casting Process Suitability — BS 1490:1988 Table 8
Ratings from BS 1490:1988 Table 8. Scale: 4 = Excellent, 3 = Good, 2 = Fair, 1 = Poor, n = Not normally recommended.
| CASTABILITY PROPERTY | RATING | EXPLANATION |
|---|---|---|
| Fluidity | 2 — Fair | Extreme Si level creates significant castability challenges. |
| Resistance to hot tearing | 3 — Good | High Si contributes to hot-tear resistance. |
| Pressure tightness | 2 — Fair | Moderate pressure tightness. |
| Machinability (as-cast) | 1 — Very Difficult | Group 1 — most difficult to machine of all LM alloys. Diamond tooling mandatory. |

Heat Treatment
LM29 Heat Treatment — BS 1490:1988 Conditions
M
As Cast
No heat treatment. Used as-cast. Dimensional stability is the priority.
TS
Stress Relieved
200–250°C, 2–4 hours. Reduces residual casting stresses without significant property change.
TB
Solution + Natural Age
Solution treat, quench, age at room temperature. Strength develops over days to weeks.
TB7
Solution + Stabilise
Solution treat, quench, then stabilise at low temperature. Good ductility and dimensional stability.
TE
Artificially Aged Only
Age at 160–180°C, 6–12 hours. Moderate strength improvement without solution treatment.
TF
T6 — Peak Strength
Solution treat + quench + artificial age. Peak strength condition. Full in-house at Creative Alucast.
TF7
T7 — Over-aged / Stabilised
Solution treat + quench + over-age. Slightly lower strength than TF but superior dimensional stability.
Mandatory Hardness and Microstructure Testing

Applications
Typical Applications of LM29
| INDUSTRY | TYPICAL PARTS | WHY LM13 |
|---|---|---|
| Aviation | Aircraft piston engine pistons, high-speed rotating components | Minimum thermal expansion at very high temperatures |
| Racing | Extreme-performance racing engine pistons | Maximum wear resistance + minimum expansion |
Aviation Pistons
Racing Pistons
High-Speed Components
Extreme-Temperature Parts
When NOT to Specify LM29
