| name | friction-stir-welding |
| description | Friction stir welding (FSW) — tool design (shoulder/pin), process parameters (RPM/feed/tilt), material flow zones, heat generation, microstructure (TMAZ/HAZ/nugget), defects, AWS D17.3, aluminum/titanium/steel FSW, FSW-to-MIG comparison. |
| metadata | {"priority":7,"promptSignals":{"phrases":["friction stir welding","FSW","FSW tool design","friction stir weld defects","AWS D17.3","FSW aluminum"],"minScore":3}} |
Friction Stir Welding (FSW) — Complete Skill
FSW Process Fundamentals
Process: rotating non-consumable tool (shoulder + pin) plunged into joint; tool traverses along joint; frictional + adiabatic heat softens material; plasticized material flows around pin → solid-state bond
Advantages over fusion welding:
- No melting → no hot cracking, porosity, or solidification defects
- Low distortion (lower peak temperature than arc welding)
- Fine grain microstructure in weld zone (recrystallization from severe plastic deformation)
- No filler metal, shielding gas, or flux required
- Suitable for alloys difficult to fusion weld (6xxx, 7xxx, 2xxx aluminum)
Limitations:
- Requires rigid fixturing (high tool forces: 5–30 kN downward)
- Exit hole from tool retract (remedied by retractable pin tools or runoff tab)
- Not suitable for complex 3D geometries (traditionally linear welds)
- Limited to softer materials (Al, Mg, Cu, Ti with special tools; steel is challenging)
Tool Design
Shoulder
Function: generates most of the frictional heat; contains plasticized material; forge workpiece surface
Shoulder diameter D_s: D_s / t ≈ 3–5 (t = plate thickness); typical D_s = 15–30 mm for 3–10 mm Al
Shoulder features:
- Flat: simple; effective for thin sheet
- Concave (scrolled): improves material containment; reduces flash; most common
- Convex: for filling T-joints or lap welds
- Scroll channels: improves material flow inward → better containment
Shoulder material: H13 tool steel for Al; WC-Co or Si₃N₄ for titanium/steel (harder)
Pin (Probe)
Function: plunges to root of joint; stirs through-thickness; provides threaded or featured path for material transport
Pin geometry types:
- Cylindrical smooth: simplest; lowest heat input; basic research
- Cylindrical threaded: most common; enhances material flow axially
- Tapered threaded: conical; better penetration, reduced forces
- MX-Triflute (The Welding Institute patented): three flutes + right/left hand threads → improved flow, reduced defects
- Trilobite / threaded with flats: non-circular cross-section → pulsating action → improved mixing
Pin length: L_pin = 0.9–0.95 × t (sheet thickness) [leave small unfused root: ≤ 0.5 mm]
Pin diameter d_p: d_p = 0.3–0.4 × D_s [shoulder-to-pin diameter ratio: ~2.5–3.5]
Process Parameters
Tool rotation speed N [RPM]: 300–1500 RPM for Al (higher for thin sheet; lower for thick)
Weld speed v [mm/min]: 50–800 mm/min for Al; slower for thick or harder materials
Tilt angle: 1–3° (tool tilted from perpendicular toward trailing edge) → promotes forging action
Pitch (mm/rev): v / N [mm/revolution; lower pitch = more heat/energy per unit length]
Heat generation model:
Q = 2π²/3 × μ_friction × P_axial × N × (D_s³ - D_p³) / (60 × 1000) [W; simplified shoulder heat]
μ_friction ≈ 0.3–0.5 (sliding friction); P_axial = axial tool pressure [MPa]
Shoulder heat fraction: ~80–90% of total heat from shoulder; 10–20% from pin
Heat index (process heat input):
HI = N² / v [RPM²/(mm/min); higher HI = hotter weld; can cause defects if too high]
Or: Energy/length = Tool torque × 2π × N / (60 × v) [J/mm]
Weld Zone Microstructure
Zone Definitions
Nugget (weld core/stir zone):
Direct contact with pin; severe plastic deformation + heat → dynamic recrystallization
Result: very fine equiaxed grains (1–5 μm in Al); uniform microstructure
Properties: high strength (precipitation may be dissolved); hard in some alloys
TMAZ (Thermomechanically Affected Zone):
Adjacent to nugget; influenced by both heat and plastic strain
Deformed grains (not recrystallized in Al); elongated grain structure visible
Lower strength than nugget; transition zone
HAZ (Heat Affected Zone):
Thermal influence only; no plastic strain
For precipitation-hardened alloys (7075, 2024): over-aging in HAZ → strength reduction of 10–30%
HAZ width: 5–20 mm depending on parameters; minimum with high weld speed
Parent material: unaffected beyond HAZ
Microstructure-Property Relationships
Hardness profile (7075-T6 typical):
Parent: HV 180; nugget: HV 100–120 (dissolution); HAZ minimum: HV 90–110 (over-aged)
UTS: nugget ≈ 80% of parent; joint efficiency = σ_weld_UTS / σ_parent_UTS × 100%
Typical joint efficiency: 70–90% for 2xxx/7xxx Al; 90–98% for 5xxx/6xxx Al
Defects
Wormhole/void: insufficient material flow; caused by too-low heat input (high weld speed or low RPM)
Detection: UT (phased array), X-ray; fatal defect
Kissing bond (cold lap at root): weak oxide layer not disrupted at root; requires sufficient plunge depth; detected by UT
Flash: excess material expelled at surface; too-high heat (excessive shoulder pressure or too-slow travel)
Nugget collapse: high heat + insufficient forging force → material flows out; hollow nugget
Surface galling/roughness: tool wear or incorrect shoulder geometry; affects surface finish
Lack of penetration (LOP): pin too short; root unfused → notch effect; critical fatigue location
Prevention: verify L_pin = 0.9 × t; use PAUT (phased array UT) for inspection
Inspection and Quality
NDE methods:
Phased array UT (PAUT): most effective; detects internal voids, kissing bonds, LOP
X-ray: detects voids; cannot detect kissing bonds (planar defect)
Dye penetrant: surface cracks only
AWS D17.3 (Aerospace FSW):
Inspection: 100% UT on all welds; accept/reject criteria per standard
Weld class A, B, C: different defect allowances for different criticality levels
Cross-section metallography required for process qualification
Tensile testing per ASTM E8:
Longitudinal tensile: weld parallel to gauge (checks parent + weld zone)
Transverse tensile: weld perpendicular to gauge; measures joint efficiency
FSW of Non-Aluminum Materials
Magnesium (Mg):
Similar to aluminum; lower forces; tool: H13 or WC; N = 500–2000 RPM
Joint efficiency: 85–95% typical
Copper:
Higher flow stress; H13 tool wears quickly → WC-Co or PCBN tools
N = 200–500 RPM; v = 50–150 mm/min
Titanium:
Very high flow stress + high temperature → tool wear severe
PCBN or Si₃N₄ tools; inert gas shielding required; N = 100–400 RPM; v = 30–100 mm/min
Joint efficiency: 90–100%; microstructure: fine α+β in nugget
Steel (low-carbon):
PCBN or WC-Re tools; short tool life
N = 100–300 RPM; v = 50–200 mm/min; preheating may help
Limited industrial use due to tool cost; research active
Standards
| Standard | Scope |
|---|
| AWS D17.3/D17.3M | Friction stir welding for aerospace |
| AWS D1.2 | Structural welding code — aluminum (includes FSW) |
| ISO 25239 | Friction stir welding — general requirements |
| ASTM E2700 | Contact ultrasonic testing for friction stir welds |
| MIL-STD-1839 | Defense material joining (includes FSW criteria) |
Output
Provide: material(s) and thickness [mm], joint configuration (butt/lap/T), tool design (shoulder D_s [mm], pin d_p [mm], L_pin [mm], geometry type), process parameters (N [RPM], v [mm/min], tilt angle [°]), heat input [J/mm], weld zone characterization (nugget grain size [μm], HAZ width [mm]), microhardness profile (nugget/HAZ/parent HV), joint efficiency [%] (UTS_weld/UTS_parent), defects detected (type, size), NDE method used, AWS D17.3 weld class (if aerospace), and applicable standard (AWS D17.3, ISO 25239).