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

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

LM29 requires mandatory microstructure control (same as LM28), mandatory hardness testing, diamond machining, and experienced foundry practice. It is a Group C alloy of the most limited application. Confirm requirements and foundry capability thoroughly before specifying.

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.

Sand Casting
1
Gravity Die Casting (GDC)
2
Low Pressure (LPDC)
1
High Pressure (HPDC)
n
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

Both microstructure and hardness testing are mandatory for LM29 per BS 1490. TE and TF hardness ranges are 100–140 HB — the highest mandatory hardness specification in the standard. Diamond machining is the only practical tooling approach.

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

Do not specify LM29 unless LM28 has been evaluated and found insufficient. This is the most restrictive alloy in the BS 1490 series. For all general elevated-temperature applications, LM13 or LM26 are more practical.

Frequently Asked Questions

Common Questions About LM29

What is the chemical composition of LM29 aluminium alloy?
LM29 per BS 1490:1988 has nominal composition Al-Si23Cu1Mg1Ni1. Silicon: 22.0–25.0%, Copper: 0.8–1.3%, Magnesium: 0.8–1.3%. The remainder is aluminium with controlled impurity limits.
The EN 1706 equivalent of BS 1490 LM29 is —, with chemical symbol designation EN AC-Al Si23Cu1Ni1Mg. This European standard supersedes the German DIN designation G-AlSi23CuMgNi.
The ASTM/Aluminium Association equivalent of LM29 is —. No ASTM equivalent.
There is no direct JIS H 5302 equivalent for LM29. No JIS equivalent.
The minimum tensile strength of LM29 is 190 N/mm² in the best condition and process per BS 1490:1988 Table 4 (separately cast test samples). Properties vary with casting process and heat treatment condition.
Yes — LM29 is T6 heat-treatable (TF condition). Solution treat at 515–525°C, water quench, artificially age at 155–175°C. Full in-house T6 available at Creative Alucast with batch hardness verification.
Per BS 1490:1988 Table 8: Sand casting (1), Gravity Die Casting (2), Low Pressure Die Casting (1), High Pressure Die Casting (n). Scale: 4=Excellent, 3=Good, 2=Fair, n=Not recommended.
The density of LM29 is 2.66 g/cm³ — approximately one-third the density of steel (7.85 g/cm³), making it ideal for lightweight structural applications.
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