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Before You Cut
Steel.

DFM Rule
Draft Angles
Sand Casting — External
1° – 3°
Pattern walls on cope and drag faces
Sand Casting — Internal / Cores
2° – 5°
Deeper draft needed for internal core faces
Gravity Die (GDC)
2° – 4°
Metal die requires more draft than sand
LPDC
2° – 4°
Consistent with GDC; inner surfaces 3°–5°
HPDC — External
0.5° – 2°
High pressure and smooth die surface allow shallower draft
HPDC — Internal
1° – 3°
Cores and deep pockets require increased draft

Why It Matters
Quick Reference — Draft by Depth
≤25 mm
Feature Depth
1° min
25–75 mm
Feature Depth
2° min
>75 mm
Feature Depth
3° min
Design This Way
- Apply draft to all walls parallel to the draw direction — external and internal
- Increase draft on deep pockets and narrow ribs beyond the minimum
- Note machined surfaces clearly — draft can be removed post-machining on datums and bores
- Agree draft direction with the foundry before finalising the parting line
Avoid This
- Zero-draft walls on non-machined surfaces — the part cannot be extracted cleanly
- Negative draft (reverse taper) — actively locks the casting into the tool
- Applying the same draft to internal and external surfaces — internal always needs more
- Forgetting draft on features designed in a different orientation to the main part

DFM Rule
Wall Thickness
Sand Casting
4–6 mm
Minimum for reliable fill; 5 mm recommended general
Gravity Die (GDC)
3–5 mm
Metal die conducts heat faster — 3.5 mm practical minimum
LPDC
3–4 mm
Controlled fill allows thinner sections reliably
HPDC
1.5–2.5 mm
High injection speed and pressure fill thin walls

Solidification Sequence Rule
Thick-to-Thin Transition Rule
Design This Way
- Target uniform wall thickness throughout — aim for variation <20% from nominal
- Use ribs to provide stiffness instead of increasing wall thickness
- Taper thick-to-thin transitions gradually over at least 3× the thickness change
- Core out thick sections — hollow bosses and pads rather than solid masses
Avoid This
- Abrupt junction of thin wall to thick flange — shrinkage porosity is almost certain
- Walls below process minimum — cold shuts and misruns will result
- Isolated thick sections surrounded by thin walls — "hot spot" with no feed path
- Uniform-thickness thinking from sheet metal — casting solidification is 3-dimensional

DFM Rule
Corner Radii & Fillets
Internal Fillet — Minimum
R 3 mm
Absolute minimum; R5 or greater strongly preferred
Internal Fillet — Recommended
R 5–8 mm
Prevents die chipping and sharp oxide formation in the casting
External Corner — Minimum
R 1.5 mm
Prevents die chipping and sharp oxide formation in the casting
Fillet at Rib Junction
0.5–1× wall thickness
Fillet radius = 0.5t to 1t where t = rib thickness

Fatigue Life Impact
Increasing an internal corner radius from zero (sharp) to R5 mm improves fatigue life by 20–40% in tested aluminium casting specimens — with no weight penalty and no tooling cost increase. It is the single cheapest design change with the highest mechanical return.
Hot Spot at Corner
A sharp internal corner creates a thermal hot spot — metal in the corner is surrounded on two sides by already-solidifying material, trapping heat. The last liquid metal to solidify shrinks, creating a micro-void or crack. A fillet distributes this zone over a curved surface, reducing peak temperature and allowing directional solidification away from the corner.
Design This Way
- Apply generous internal fillets everywhere — minimum R3, target R5 or greater
- At rib-to-wall junctions, fillet = 0.5× to 1× the wall thickness
- Break all external edges with at least R1.5 — no sharp arris on castings
- Where a sharp internal corner is functionally required, machine it in after casting
Avoid This
- Zero-radius internal corners — fatigue crack initiation is almost guaranteed
- Sharp rib-to-wall junctions — solidification stress concentration causes micro-cracking
- Inconsistent radii on the same surface — varies stress distribution unpredictably
- Specifying "break sharp edges" as a substitute for designed-in fillets

DFM Rule
Parting Line Design
The Core Principle
The parting line should follow the maximum cross-section of the part — the widest point when viewed in the draw direction. This minimises undercuts, simplifies tooling, and allows all surfaces to be drafted toward the parting plane. A poorly placed parting line multiplies tooling cost and reduces dimensional capability.
Flash & Fettling

Good Parting Line Practice
- Place at the maximum cross-section — the widest perimeter of the part in draw direction
- Keep parting line in a single plane wherever possible — stepped parting lines cost more
- Place on a non-cosmetic surface — parting line flash is visible and requires fettling
- Consider parting line position at the sketch stage — it's very difficult to move later
- Ask the foundry to mark the proposed parting line on your 3D model before tooling
Common Mistakes
- Placing the parting line on a sealing face, bearing surface, or cosmetic external face
- Designing features that force a stepped, angled, or curved parting plane
- Ignoring the parting line entirely and leaving it to the toolmaker — costly assumption
- Specifying tight tolerances across the parting line — it always introduces variability
Dimensional Note

DFM Rule
Ribs , Bosses & Pads
Ribs, bosses, and mounting pads are the features most commonly over-sized by designers unfamiliar with casting. A rib that is too thick relative to the wall it joins will create a shrinkage hot spot at the junction. A boss that is solid and thick will almost certainly contain internal porosity. Designing these features correctly adds stiffness and function at no weight or cost penalty.
Rib Thickness
0.5 – 0.8× wall
Rib thickness = 50–80% of the wall it joins. Never equal to or greater than the wall.
Rib Height Limit
≤ 5× rib thickness
Taller ribs need draft and are difficult to fill reliably. Maximum H/t ratio = 5.
Boss OD / Wall Ratio
≤ 2× wall thickness
Boss diameter should not exceed 2× the adjacent wall. Core out large bosses.
Boss — Coring
Core to 75% depth
Solid bosses shrink. Core out to leave a 1.5–2 mm base wall — removes hot spot.

Stiffness without Mass
Rib Design Rules
- Rib thickness = 0.6× wall for best results — thin enough to avoid hot spot, thick enough to fill
- Space parallel ribs at minimum 2× rib thickness apart — metal must flow between them
- Core out all bosses over 15 mm diameter — this is the single most effective porosity prevention step for bosses
- Add a generous fillet at every rib-to-wall junction — minimum R = 0.5× rib thickness
Common Mistakes
- Making ribs the same thickness as the wall they stiffen — guaranteed hot spot
- Intersecting ribs at right angles without adequate metal — creates a node hot spot
- Solid tall bosses — internal shrinkage is almost certain without coring
- Mounting pads machined directly into raw wall surfaces — always add a cast-in pad with machining allowance

DFM Rule
Machining Allowances
Sand Casting
2.5 – 5 mm
Largest allowance — widest casting tolerance (CT8–CT10)
Gravity Die (GDC)
1.5 – 3 mm
Better dimensional consistency; CT6–CT8 typical
LPDC
1.0 – 2.5 mm
Tighter process — CT5–CT7; smaller allowance needed
HPDC
0.5 – 1.5 mm
Best dimensional accuracy; CT4–CT6; minimum allowance

ISO 8062 Casting Tolerances
| PROCESS | CT GRADE |
|---|---|
| Sand Cast | CT8–CT10 |
| GDC | CT6–CT8 |
| LPDC | CT5–CT7 |
| HPDC | CT4–CT6 |
Hard Anodising — Special Case
If the finished component will be hard anodised (Type III), the coating grows ~50% outward. A 50 µm coating adds ~25 µm per face. Specify a “pre-anodise” dimension on all tolerance-critical features so the machining drawing reflects the dimension before coating, not after. This is a very common oversight causing fit failures after processing.
On the Drawing
- Show both the casting dimension (with allowance) and the machined final dimension — two dimension sets
- Mark machined surfaces with the standard machining symbol and Ra requirement
- Add datums — state which cast surface or machined feature is the datum for all machined dimensions
- Specify the casting tolerance standard (ISO 8062 CT grade) on the title block
Common Drawing Errors
- Providing only the final machined dimension — the foundry has no reference for stock allowance
- Applying the same allowance regardless of process — wastes material and machining time
- No datum defined — machinist cannot locate the part consistently
- No machining symbols — foundry cannot identify which surfaces need allowance

DFM Rule
Undercuts & Cores
Sand Casting
Most flexible
Sand cores can form almost any internal geometry — but cores must be supported and extractable
GDC / LPDC
Side actions + cores
External undercuts via slides; internal via sand or metal cores that can be pulled
HPDC
Sliders for external
No sand cores possible; internal undercuts extremely limited — plan geometry carefully
Dissolving-Core
Blind undercuts ✓
Complex hollow internal geometries impossible by conventional means — core dissolved in water

Advanced Capability — Dissolving-Core Casting
If Your Internal Geometry Has No Conventional Solution
Core Design Requirements
Design Principles
- Identify all undercuts early — mark them on the 3D model and discuss with the foundry before tooling
- Redesign external undercuts into draft-able features where possible — avoids sliders
- Ensure internal cores have both a print (support) and a draw path — core must be removable
- For blind internal geometry — consider dissolving-core casting as the right solution
Common Problems
- Designing internal passages that loop back on themselves — no extraction path for conventional core
- HPDC designs with complex internal geometry — the process cannot accommodate internal cores
- Undercuts on mating faces — slider witness marks fall on functional surfaces
- Assuming what is possible in 3D CAD is possible in casting — they are different constraints

DFM Decision 08
Choosing the Right Process
Process 01
Sand Casting
- Min Wall
- Tolerance
- Surface Finish
- Tooling Cost
- MOQ
- Weight Range
- 4–6 mm
- CT8–CT10
- Ra 6.3–25 µm
- Lowest
- 1 piece
- 0.1 – 500 kg
Best for
- Low volume
- Complex geometry
- Large parts
- Prototypes
Process 02
Tilt GDC
- Min Wall
- Tolerance
- Surface Finish
- Tooling Cost
- MOQ
- Weight Range
- 3–5 mm
- CT6–CT8
- Ra 3.2–6.3 µm
- Medium
- 50–200 pcs
- 0.05 – 50 kg
Best for
- Med volume
- Low porosity
- Structural parts
- Heat treatable
Process 03
LPDC
- Min Wall
- Tolerance
- Surface Finish
- Tooling Cost
- MOQ
- Weight Range
- 3–4 mm
- CT5–CT7
- Ra 1.6–3.2 µm
- Medium–High
- 200–500 pcs
- 0.5 – 30 kg
Best for
- Structural
- Safety-critical
- Thin walls
- High density
Process 04
HPDC
- Min Wall
- Tolerance
- Surface Finish
- Tooling Cost
- MOQ
- Weight Range
- 1.5–2.5 mm
- CT4–CT6
- Ra 0.8–1.6 µm
- Highest
- 1000+ pcs
- 0.01 – 25 kg
Best for
- High volume
- Thin wall
- Tight tolerance
- Best surface
Not sure which process fits your part?

DFM Decision 09
Alloy Selection Guide
| Alloy | Designation | Strength | Corrosion | Castability | Heat Treat | Best Process | Primary Use |
|---|---|---|---|---|---|---|---|
| LM2 | Al–Si10Cu2Fe | No | HPDC | General purpose die casting, enclosures | |||
| LM4 | Al–Si5Cu3 | T5 / T6 | SAND GDC | Versatile engineering, housings, brackets | |||
| LM5 | Al–Mg5Si | No | SAND GDC | Marine, chemical exposure, food equipment | |||
| LM6 | Al–Si12 | No | SAND GDC LPDC | Pump bodies, marine, thin sections, complex shapes | |||
| LM13 | Al–Si12CuMgNi | T5 | GDC LPDC | Pistons, wear surfaces, elevated temperature | |||
| LM16 | Al–Si5Cu1Mg | T5 / T7 | SAND GDC LPDC | Pressure-tight, structural, impact-resistant | |||
| LM25 | Al–Si7Mg | T4 / T5 / T6 | SAND GDC LPDC | Premium structural, automotive, aerospace-grade | |||
| LM26 | Al–Si9Cu3Mg | T5 | GDC LPDC | Automotive — high strength, wear resistant |

Before You Send the Drawing
DFM Self-Check Checklist
Work through this checklist before sending your design to any foundry. Each item is a common source of tooling revision, reject castings, or cost overrun — all of which are avoidable.
Geometry
- Draft angles applied to all surfaces parallel to draw direction — internal and external
- Internal fillets ≥ R3 mm on all internal corners and rib junctions
- Wall thickness meets minimum for chosen process; no wall below minimum anywhere
- Thick-to-thin transitions tapered — no abrupt step changes in wall thickness
- Bosses cored out where diameter exceeds 15 mm
- Rib thickness ≤ 80% of the wall they join
Drawing & Tolerances
- Machining allowance added to all surfaces to be finish-machined — pre- and post-machine dimensions both shown
- Machined surfaces marked with surface finish symbol and Ra requirement
- Datums defined — machining datum surface clearly identified
- CT grade specified on title block (ISO 8062) or casting tolerances called out explicitly
- Tight tolerances not placed across parting line — move critical dimensions to single mould half
Process & Material
- Casting process confirmed — wall thickness, volume, and tolerance are compatible
- Alloy specified — correct LM grade for strength, corrosion, heat treatment, and process requirements
- Heat treatment specified if required — T4, T5, T6, or T7 with hardness or mechanical property requirement
- Surface coating considered — anodise allowance on drawings if hard anodise specified
- 3D CAD file ready — STEP or IGES format, solid model, no open surfaces
Free Service
Send Us Your Design for a DFM Review
Our engineering team reviews your casting drawing against every principle on this page — draft, wall thickness, radii, parting line, machining allowances, alloy suitability, and process fit. You get back a marked-up file with specific recommendations, before any tooling cost is committed.
- No commitment required — the review is free
- STEP, IGES, STL, PDF or DXF accepted
- Turnaround typically 2–3 business days
- Marked-up CAD or annotated PDF returned
- Alloy and process recommendation included
- Applicable to new designs and existing parts
The Cost of Getting It Wrong
A pattern revision after tooling is cut costs 20–60% of original tooling cost. A casting reject rate of 15% on a production run often traces back to a design decision made in the first week of a project. A 30-minute DFM conversation at concept stage eliminates most of this risk entirely.
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