THE CENTRAL IDEA
The final geometry of a weldment is created by the entire manufacturing route—not by the welding operation alone. Design the route, then design the weldment.
Design question | Engineering response | |
|---|---|---|
How does the load move through the structure? | Create a clear load path and place joints where they can be manufactured and inspected. | |
Can the assembly be built repeatedly? | Design for cutting, forming, fit-up, clamping, welding, fixture release and handling. | |
How will welding heat move the geometry? | Plan sequence, restraint, symmetry and post-weld correction before tolerancing. | |
Which dimensions truly drive function? | Separate functional interfaces from general fabricated dimensions. | |
Which surfaces require machining? | Leave appropriate stock and machine after the geometry-changing operations. | |
How will quality be verified? | Define weld requirements, NDT, dimensional checks and documentation before RFQ. | |
1. Think in Manufacturing Routes, Not Individual Welds
A fabricated assembly passes through multiple geometry-changing operations: material preparation, cutting, forming, fit-up, tack welding, welding, straightening, heat treatment where required, machining, inspection and surface protection. Each stage can influence the next.
A design that looks simple in CAD can become difficult when a welder cannot reach the joint, a fixture blocks the torch, a machined face distorts after welding, or a closed section cannot be coated or inspected. DFM therefore begins by mapping the complete route.
FABRIOX FABRICATION FRAMEWORK
FUNCTION → LOAD PATH → MATERIAL → JOINT → PROCESS → WELD SEQUENCE → DISTORTION CONTROL → FINAL MACHINING → INSPECTION → PROTECTION
2. Material Selection for Fabricated Structures
Material selection should begin with structural and service requirements, then consider weldability, thickness, delivery condition, forming, machining, coating and commercial availability. Two steels with similar yield strength may require different welding controls because chemistry, carbon equivalent, heat-treatment condition or thickness changes cracking risk and procedure requirements.
Material family | Why it is used | Fabrication considerations |
|---|---|---|
S235 / S275 / S355-type structural steels | General fabricated structures and machinery | Broad availability; grade/subgrade, thickness and impact requirements still matter. |
Higher-strength structural steels such as S460 / S690 families | Weight reduction or higher load capacity | More demanding forming/welding procedure, heat input and consumable control may apply. |
Wear-resistant plate | Abrasion zones and liners | Hardness, heat-affected-zone behavior, forming and machining require specific planning. |
Stainless steels | Corrosion, hygiene or temperature requirements | Contamination control, distortion, filler/process and surface restoration matter. |
Aluminum alloys | Low mass and corrosion resistance | High thermal conductivity, oxide control, distortion and alloy/temper-specific weldability. |
Profiles / tubes / hollow sections | Efficient structural geometry | Availability, corner radii, seam location, vent/drain and internal coating access can matter. |
Specify the material completely
A purchase or drawing specification should identify the applicable material standard, grade, delivery condition and any required impact, through-thickness, traceability or certification conditions. Do not approve an 'equivalent' grade from chemistry alone when mechanical properties, delivery condition, toughness, weldability or product standard are part of the requirement.
3. Design the Load Path Before the Weld Detail
A weld is a load-transfer feature, not decoration. Joint geometry should be developed from the forces the assembly must transmit and the applicable design rules. The manufacturing team should not be expected to choose weld size or length solely from shop habit.
The engineering design should distinguish structural welds, sealing welds, attachment welds and cosmetic requirements. This prevents a common problem: increasing weld volume in areas where it adds heat and distortion but little functional value.
IMPORTANT
More weld is not automatically safer. Weld size and length should come from engineering design and the governing specification. Excess weld can add filler, arc time, heat input, shrinkage and distortion.
4. Joint Design and Welding Access
Joint | Design considerations |
|---|---|
Butt joint | Edge preparation, root access, penetration requirement, backing/gouging and inspection access. |
T-joint | Load path, fillet/groove choice, access to both sides, distortion from unbalanced welding. |
Lap joint | Eccentric load path, corrosion/sealing, access and trapped coating areas. |
Corner joint | Torch access, shrinkage at the corner, sealing and finishing. |
Boss / machined insert | Weld sequence, local stiffness, machining allowance and heat distortion. |
Tube / closed section connection | Internal access, venting, coating, drainage and inspection limitations. |
A joint may be theoretically weldable but industrially poor if the torch angle is restricted, the welder cannot see the root, slag cannot be removed, a robot cannot reach the path, or NDT cannot access the examination surface. These constraints should be resolved during design review.
5. Choose the Welding Process Around the Joint and Production System
Process | Strengths | Typical constraints |
|---|---|---|
GMAW / MIG-MAG | High productivity, mechanization/robot potential, broad industrial use | Shielding and parameter control; access and transfer mode matter. |
FCAW | High deposition and productivity in many fabrication applications | Slag/fume, consumable/process control and cleaning. |
GTAW / TIG | High control and clean welds | Lower deposition rate; often used for precision/root/special-material work. |
SMAW | Portable and flexible | Lower productivity; electrode handling and operator dependence. |
SAW | Very high deposition for suitable long seams/heavy fabrication | Generally limited by position, joint access and equipment arrangement. |
Robotic welding | Repeatability and arc-on productivity | Requires repeatable fit-up, stable joint location, access and volume justification. |
There is no universal 'best' welding process. Selection depends on material, thickness, position, joint type, access, required properties, production volume, equipment and applicable procedure qualification.
6. WPS, Procedure Qualification and Welder Qualification
Production welding should be controlled by the applicable welding procedure system. A Welding Procedure Specification (WPS) gives the welder/operator the approved production variables. Procedure qualification demonstrates that the proposed welding procedure can achieve the required result under the governing standard. Welder or welding-operator qualification demonstrates personnel capability within the applicable qualification range.
Terminology and qualification rules differ between ISO/EN and AWS/ASME systems. PQR and WPQR are related concepts but should not be presented as universally interchangeable documents. The contract should define the governing system.
ISO 3834-1:2021 provides criteria for selecting among comprehensive, standard and elementary quality-requirement levels in the ISO 3834 series for fusion welding. It applies in workshop and field manufacturing, but it is not itself a complete quality-management system.
7. Fit-Up Is a Manufacturing Process
Welding quality begins before the arc starts. Gap, alignment, edge preparation, cleanliness, tack quality and component location determine whether the WPS can be executed consistently.
Create functional locating datums and repeatable stops in the fixture.
Control root gaps and alignment where the joint design requires them.
Place tack welds so they stabilize the assembly without creating inaccessible defects or excessive restraint.
Check that clamps do not block the welding torch, cleaning or inspection.
Plan how the assembly is released from the fixture without springing into an uncontrolled shape.
Control drawing revision and component identity before fit-up.
FIXTURE DESIGN QUESTION
Can this be located, clamped, welded, inspected and removed from the fixture repeatedly?
8. Welding Distortion: The Core DFM Problem
Welding introduces concentrated heat. The heated metal expands, then contracts as it cools. Because heating and restraint are nonuniform, the final assembly can shrink, rotate, bow, buckle or twist. Distortion is therefore a predictable manufacturing phenomenon—not evidence by itself that a welder has performed poorly.
Distortion mode | What happens |
|---|---|
Longitudinal shrinkage | The welded region contracts along the weld direction. |
Transverse shrinkage | The joint contracts across the weld. |
Angular distortion | Unequal shrinkage through thickness rotates the joined parts. |
Bowing / bending | Unbalanced shrinkage curves the assembly. |
Buckling | Thin plate loses stability under compressive residual stress. |
Local distortion | Heat affects a localized flange, wall, boss or machined interface. |
Design it out
Use only the weld volume required by design.
Keep stiffness and weld placement as balanced as practical.
Avoid abrupt thickness changes and heavily restrained local details where possible.
Place critical machined interfaces so they can be finished after welding when necessary.
Use subassemblies to create manageable welding and fixture sequences.
Control it during fabrication
Develop a defined tack and weld sequence.
Use balanced, skip or back-step concepts only where validated for the joint/process.
Control heat input and interpass conditions through the qualified procedure.
Use fixtures, strongbacks or temporary restraint strategically—not simply maximum clamping force.
Use presetting or pre-camber only where engineering/process experience supports the compensation.
Map first-article dimensions to understand actual movement before serial production.
Correct only what remains
Straightening, thermal correction and post-weld machining can be valid production operations, but they should not compensate for a fundamentally unstable design. The preferred hierarchy is:
DISTORTION HIERARCHY
DESIGN IT OUT → CONTROL IT DURING FABRICATION → MACHINE / CORRECT ONLY WHAT REMAINS
9. Tolerancing a Welded Structure
A large weldment should not be toleranced like a small machined block. Weld shrinkage, plate flatness, profile variation, forming and fixture release all contribute to final geometry. The drawing should distinguish general fabricated tolerances from individually critical functional characteristics.
ISO 13920:2023 is the current second edition for general tolerances of welded constructions. It defines four tolerance classes for linear/angular dimensions and shape/position based on customary workshop accuracy, with class selection driven by functional requirements. ISO explicitly states that the applicable tolerances are those stated on the drawing and that complex structures may require special provisions.
Dimension type | Recommended strategy |
|---|---|
Overall fabricated envelope | Use an appropriate fabrication tolerance framework where contractually applicable. |
Mounting hole pattern | Individually control if assembly depends on it; consider final machining/drilling strategy. |
Machined mounting face | Control in the final machined condition relative to functional datums. |
Bracket / attachment location | Set tolerance according to actual interface need, not arbitrary CAD precision. |
Free edge / nonfunctional plate location | Allow practical fabrication variation where it does not affect function. |
Flexible thin structure | Define inspection/support condition if gravity or restraint changes measurement. |
TOLERANCE PRINCIPLE
Do not force machined-part thinking onto every dimension of a large weldment. Control the dimensions that drive assembly and function, and choose the manufacturing sequence that can actually achieve them.
10. Machining Before or After Welding?
Machining sequence is one of the most important weldment decisions. Features machined before welding may move because of welding heat; features machined after welding require enough stock, machine access and a stable datum strategy.
Strategy | Use when | Risk to manage |
|---|---|---|
Machine before welding | Feature cannot be accessed later or only rough accuracy is required | Weld distortion may move the finished feature. |
Rough machine before / finish after | Large stock removal or datum creation is useful before welding | Need sufficient finishing allowance after distortion. |
Machine after welding | Final interfaces must relate to the completed structure | Machine envelope, setup and handling of large weldment. |
Machine after stress relief / heat treatment | High-precision geometry must follow a geometry-changing thermal step | Additional route time and careful allowance planning. |
Large fabricated bases, bearing housings, pivot interfaces and aligned bores may require face milling, line boring or large-envelope machining after welding. Design should reserve access and stock for that operation from the beginning.
11. Weld Quality Levels and Acceptance
ISO 5817:2023 is the current fourth edition specifying quality levels for imperfections in fusion-welded joints in steels, nickel, titanium and their alloys within its stated scope. It defines levels B, C and D; level B corresponds to the highest requirement on the finished weld.
That does not mean every industrial weldment should automatically specify level B. The appropriate acceptance requirement depends on design, load, service, applicable code and contract. A higher workmanship requirement can add preparation, process control, inspection and repair cost without adding value if the product does not require it.
Imperfection is not automatically a reject
Terms such as porosity, undercut, reinforcement, lack of fusion or profile describe conditions that must be evaluated against the applicable acceptance criteria. The existence of a visible imperfection and the decision to reject the weld are not the same thing.
Imperfection family | Prevention / control focus |
|---|---|
Cracking | Material/weldability, hydrogen control, restraint, heat treatment and qualified procedure. |
Porosity | Cleanliness, shielding, consumable/material condition and process stability. |
Lack of fusion / penetration | Joint preparation, access, parameters, technique and procedure compliance. |
Undercut / profile | Parameter balance, travel/technique and joint access. |
Slag / inclusions | Process technique, cleaning and joint geometry. |
Dimensional distortion | Design, sequence, heat balance, restraint and correction strategy. |
12. Inspection and NDT
Inspection should be selected from the defect mechanism, material, joint, thickness, access, service risk and governing specification. No single NDT method finds every relevant discontinuity.
Method | Useful for | Key limitation |
|---|---|---|
VT – Visual Testing | Surface condition, profile, obvious cracks, dimensions and workmanship | Only visible/accessible surface conditions. |
PT – Penetrant Testing | Surface-breaking discontinuities in suitable nonporous materials | Surface must be accessible and properly prepared. |
MT – Magnetic Particle Testing | Surface and near-surface discontinuities in ferromagnetic materials | Limited to magnetizable materials. |
UT – Ultrasonic Testing | Internal discontinuities in suitable weld geometries/materials | Geometry, thickness, access and procedure/skill strongly affect effectiveness. |
RT – Radiographic Testing | Volumetric imaging of suitable joints | Radiation safety, access, orientation and sensitivity to defect type matter. |
Dimensional inspection | Final geometry, datums and interfaces | Must reflect the specified free/restrained state and final manufacturing stage. |
The extent, technique and acceptance criteria for NDT should be stated by the applicable product/code/customer specification. Inspection should not be added as a generic percentage without understanding the risk it is intended to control.
13. Surface Protection Is Part of the Design
System | Design implications |
|---|---|
Blast + wet paint | Surface preparation, stripe coating, inaccessible crevices, DFT and masking. |
Powder coating | Part size/oven, hanging points, masking, cure temperature and coating build. |
Hot-dip galvanizing | Vent/drain paths, trapped volumes, distortion risk, coating access and post-galvanizing fit. |
Metallizing / thermal spray | Surface preparation, access and sealing/topcoat system. |
Stainless pickling/passivation | Weld discoloration/contamination control and specified restoration process. |
Closed hollow sections sent for hot-dip galvanizing require correctly engineered venting and drainage for process safety and coating quality. Do not publish generic vent-hole sizes without validating the part geometry, galvanizer requirements and applicable guidance.
14. Fabrication Cost Drivers
Cost driver | Why it matters |
|---|---|
Material / yield | Plate format, profile length, nesting and remnants affect purchased mass. |
Cutting / edge prep | Thickness, bevels, holes and cleanup add processing. |
Forming | Press capacity, tooling, handling and springback influence time/risk. |
Fit-up | Complex locating and manual measurement consume skilled labor. |
Weld volume | Arc time, filler, gas and heat input grow with weld size/length. |
Welding position / access | Poor access slows deposition and may block automation. |
Fixture | NRE can improve repeatability and serial cycle time. |
Distortion / rework | Straightening and late correction add hidden cost. |
Tolerance | Tight fabricated geometry can force machining or special fixtures. |
NDT / documentation | Inspection, reports and traceability add skilled work. |
Surface treatment | Blasting, coating, masking, cure and handling. |
Handling / logistics | Large structures require cranes, lifting points, special packing and transport. |
PROCUREMENT INSIGHT
The cheapest €/kg fabrication quote is not necessarily the lowest-cost assembly. Dimensional instability, rework, coating repair, late inspection failure, packaging damage and assembly problems can dominate the economics.
15. 20-Point Metal Fabrication DFM Checklist
Is the structural load path clear?
Are material grade, standard and delivery condition unambiguous?
Are thickness changes and high-restraint details justified?
Can every weld be physically accessed?
Can the joint be cleaned and inspected after welding?
Is weld size/length defined from engineering requirements?
Are unnecessary sealing/cosmetic welds avoided?
Can the parts be located repeatably in a fixture?
Does the fixture allow torch and inspection access?
Has a weld/tack sequence been considered?
Are distortion-sensitive interfaces identified?
Are functional dimensions separated from general fabricated dimensions?
Is post-weld machining planned where necessary?
Is sufficient machining allowance provided?
Can the completed weldment fit the required machine envelope?
Are NDT method, extent and acceptance criteria defined where required?
Are material and weld traceability requirements defined?
Is surface protection compatible with closed sections, threads and fits?
Are lifting, packing and transport constraints designed into the assembly?
Have manufacturing and quality teams reviewed the drawing before serial release?
16. What to Include in a Metal Fabrication RFQ
RFQ input | Why it matters |
|---|---|
3D model + controlled drawings | Defines geometry, welds, interfaces and revision. |
BOM | Controls material, quantity and purchased components. |
Material specifications | Grade, condition, certificates and substitutions. |
Weld requirements / weld map | Defines joint intent and quality scope. |
Applicable standards | Prevents supplier assumptions about code/acceptance. |
Fabrication tolerances | Separates general and critical dimensions. |
Machining requirements | Defines sequence, stock and final datums. |
NDT / inspection plan | Defines method, extent, reports and hold points. |
Surface treatment | Defines preparation, coating system, masking and final condition. |
Documentation | MTCs, WPS/WPQR/PQR, welder qualifications, NDT, dimensional and CoC scope. |
Annual volume / batch size | Drives fixture, automation and capacity economics. |
Packaging / lifting | Critical for large weldments and finished coatings. |
Delivery / Incoterm | Enables realistic landed-cost and logistics planning. |