Friction Stir Welding of Magnesium-Aluminum Dissimilar Alloys for New Energy Battery Trays

1. Definition and Fundamental Principles

Friction Stir Welding (FSW) of magnesium-aluminum dissimilar alloys is a solid-state joining process applied to the fabrication of lightweight battery tray structures in new energy vehicles (NEVs). Unlike conventional fusion welding methods, FSW operates below the melting point of both parent materials, utilizing a non-consumable rotating tool to generate plastic deformation and frictional heat at the weld interface. The tool, typically composed of a rotating shoulder and a trailing pin, is plunged into the joint line between the magnesium alloy (e.g., AZ31, AZ91, or ZK60) and the aluminum alloy (e.g., 5052, 5754, or 6061), forging a metallurgical bond through dynamic recrystallization and severe plastic deformation.

The fundamental challenge in Mg-Al dissimilar FSW lies in the formation of intermetallic compounds (IMCs), particularly Mg₂Al₃ and Mg₁₇Al₁₂, at the weld interface. These brittle phases can significantly degrade mechanical properties and fatigue resistance if their thickness exceeds critical thresholds. The solid-state nature of FSW inherently suppresses excessive IMC growth compared to fusion welding, making it the preferred joining method for Mg-Al hybrid battery tray architectures where weight reduction and structural integrity must coexist.

2. Category and Business Positioning

This research entry falls under the company's advanced solid-state joining technology portfolio, complementing the established TIG/MIG weld overlay, hydraulic explosive bonding, and explosion welding capability routes. While the three primary routes address clad plate/pipe fabrication for pressure vessels, pipelines, and corrosion-resistant overlays, FSW of dissimilar alloys extends the company's technical boundary into lightweight structural joining for the NEV sector.

The business positioning is threefold:

3. Technical Purpose and Value

The primary technical purpose of Mg-Al FSW research for battery trays is to develop qualified welding procedures that achieve:

The value proposition for NEV OEMs is substantial: a battery tray that combines magnesium's ultra-low density (1.74 g/cm³) for weight savings with aluminum's superior formability and crashworthiness can reduce vehicle curb weight by 15–25% compared to all-steel or all-aluminum trays, directly improving range performance by 5–10%.

4. Key Process and Implementation Points

4.1 Material Selection Matrix

Component Material Specification Typical Thickness Key Property
Battery Tray Frame AZ31B / AZ91D (Mg alloy) 2.0–3.0 mm ρ = 1.74 g/cm³, UTS 200–260 MPa
Battery Tray Floor 5052-H32 / 5754-H22 (Al alloy) 1.5–2.5 mm ρ = 2.68 g/cm³, UTS 190–260 MPa
Corner Brackets 6061-T6 (Al alloy) 2.0–4.0 mm UTS 310 MPa, formability
Tool Pin WC-Co / H13 Tool Steel Wear resistance, thermal conductivity

4.2 Critical Process Parameters

Parameter Recommended Range Influence on Joint Quality
Tool Rotation Speed 800–1500 rpm Higher speed → increased temperature → thicker IMC layer; lower speed → incomplete bonding
Traverse Speed 20–60 mm/min Slower speed → more heat input → larger stir zone; faster speed → reduced heat → possible lack of fusion
Tool Tilt Angle 2°–5° (toward leading edge) Compensates for material flow asymmetry; critical for defect-free nugget formation
Plunge Depth 0.3–0.8 mm below surface Insufficient plunge → flash defects; excessive plunge → tunneling and tool damage
Tool Pin Length 90–95% of total plate thickness Determines penetration completeness; must account for sheet flatness variation
Heat Input Ratio (n/v) 30–80 rpm/(mm/min) Optimized for Mg-Al interface temperature of 250–350°C

4.3 Process Implementation Sequence

  1. Substrate Preparation: Mill or grind joint surfaces to remove oxide layers (MgO and Al₂O₃); apply anti-spatter coating to tool; verify sheet flatness within ±0.1 mm/m.
  2. Fixture Setup: Clamp both plates with uniform pressure (5–10 MPa) to prevent lift-off and misalignment; ensure gap between plates does not exceed 0.05 mm.
  3. Preheating (Optional): Apply localized induction preheat at 100–150°C to reduce tool force and improve plasticity of Mg alloy without accelerating IMC formation.
  4. Welding Execution: Initiate tool plunge at controlled rate (1–3 mm/s), achieve steady-state rotation, then traverse at programmed speed with consistent tilt angle.
  5. Post-Weld Treatment: Allow natural cooling to room temperature; apply stress-relief annealing at 150–180°C for 1 hour if residual stress exceeds 80 MPa.
  6. Inspection: Conduct visual examination, ultrasonic testing (UT), and cross-sectional metallographic analysis of IMC layer thickness.

4.4 Microstructural Zones and Defect Identification

Zone Characteristics Potential Defects Detection Method
Stir Zone (SZ) Fully recrystallized, fine grains (2–5 μm), dynamic recrystallization Void/tunnel formation, unmixed material UT C-scan, cross-section SEM
Thermo-Mechanically Affected Zone (TMAZ) Partially recrystallized, elongated grains, precipitate coarsening Softening, reduced yield strength Microhardness traverse, optical microscopy
Heat Affected Zone (HAZ) No plastic deformation, precipitate dissolution/re-precipitation Age softening in Al alloys Microhardness mapping
Parent Material (PM) Original microstructure retained Reference baseline
Interface Region IMC layer (Mg₂Al₃, Mg₁₇Al₁₂), thickness 1–8 μm Excessive IMC → brittle fracture SEM-EDS line scan, FIB-TEM

5. Applicable Standards and Acceptance Criteria

5.1 Material Standards

5.2 Welding Process Standards

5.3 Inspection and Acceptance Standards

5.4 Acceptance Criteria

Criterion Acceptance Limit Test Method
Joint Tensile Strength ≥ 70% of weaker PM (Mg alloy) ASTM E8 / GB/T 228.1
IMC Layer Thickness ≤ 5 μm at Mg-Al interface SEM-EDS cross-section
UT Defect Indication No indications exceeding acceptance level B per ISO 17637 Phased array UT (PAUT)
Visual Surface Quality No visible cracks, flash, or surface irregularities > 0.2 mm Visual examination (VT)
Fracture Location Fracture in parent material or TMAZ (not at interface) Tensile test coupon fracture analysis
Corrosion Resistance No intergranular corrosion after 48h salt spray (ASTM B117) Salt spray test

6. Common Risks and Control Measures

6.1 Technical Risks

Risk Mechanism Control Measure
Excessive IMC Formation Prolonged exposure of Mg-Al interface at elevated temperature promotes diffusion and Mg₂Al₃/Mg₁₇Al₁₂ growth Limit welding temperature to 300°C max; use higher traverse speed; minimize heat input ratio; apply Al₂O₃ barrier layer on Mg surface
Tunnel/Void Defects Incomplete material flow behind tool pin creates voids in stir zone Optimize tool geometry (pin profile: concave or threaded); increase plunge depth by 0.2–0.5 mm; verify pin length = 95% of thickness
Tool Wear and Failure High friction forces, thermal cycling, and abrasive contact with Mg/Al debris degrade tool Use WC-Co (6–8% Co) tool material; apply PVD coating (TiAlN); limit production to 200–500 m weld length per tool; monitor tool force for early failure detection
Galvanic Corrosion Electrochemical potential difference between Mg (−1.76 V) and Al (−1.66 V) drives Mg dissolution in corrosive environments Apply cathodic protection; use conformal coating on tray interior; select Mg alloy with Al content > 4% to reduce potential difference
Residual Stress and Distortion Asymmetric thermal expansion during welding causes angular and longitudinal distortion Pre-bend compensation fixtures; use backer plate with thermal mass; apply post-weld stress relief (180°C × 1h)
Hydrogen Embrittlement (Mg side) Hydrogen absorption during welding reduces Mg alloy ductility and fatigue life Ensure dry shop conditions (RH < 60%); avoid oil-based cleaning agents on Mg surfaces; apply hydrogen scavenger coatings

6.2 Quality Management Risks

7. Application Scenarios Across Technology Routes

7.1 Direct Application: Structural Battery Tray Assembly

The primary application is the structural welding of Mg-Al hybrid battery trays for NEVs. The Mg alloy forms the lightweight frame and side walls, while the Al alloy provides the crash-resistant floor and mounting interfaces. FSW enables seamless, leak-tight joints without filler material, avoiding dilution and segregation issues inherent to fusion welding.

7.2 Synergy with TIG/MIG Weld Overlay

The knowledge gained from Mg-Al FSW interface metallurgy directly informs the company's TIG/MIG weld overlay operations:

7.3 Synergy with Hydraulic Explosive Bonding

Hydraulic explosive bonding, used by the company for clad plate production, shares the solid-state joining philosophy with FSW:

7.4 Synergy with Explosion Welding

Explosion welding, the company's flagship technology for high-integrity clad plates, benefits from FSW research in the following ways:

8. Contribution to Qualification Building and Customer Value

8.1 Qualification Building

8.2 Product Delivery Enhancement

8.3 Customer Value Proposition

"By mastering Mg-Al dissimilar alloy FSW for battery trays, Cladding Technology Shanxi Co., Ltd. transitions from a specialist in corrosion-resistant clad plate manufacturing to a comprehensive lightweight structural solutions provider. This strategic expansion aligns with the global automotive industry's imperative for weight reduction and range improvement, positioning the company as a critical supplier in the NEV value chain."

The research investment in FSW technology yields measurable customer benefits:

9. Conclusion and Forward Path

The research into Mg-Al dissimilar alloy FSW for new energy battery trays represents a strategically significant extension of Cladding Technology Shanxi Co., Ltd.'s solid-state joining expertise. While the company's core competency remains in clad plate and pipe fabrication through TIG/MIG overlay, hydraulic explosive bonding, and explosion welding, the FSW research establishes critical knowledge bridges between these traditional processes and the emerging lightweight structural joining market.

Recommended next steps include:

  1. Scale-up from laboratory specimens to production-scale battery tray welding (lengths > 2000 mm) with automated FSW equipment.
  2. Conduct fatigue testing (≥ 10⁶ cycles) per GB/T 3075 to validate long-term durability for automotive applications.
  3. Establish formal WPS qualification with third-party certification body for Mg-Al FSW joints.
  4. Pursue partnerships with NEV OEMs for joint development programs and pre-qualification of battery tray welding procedures.
  5. Extend FSW research to other dissimilar pairs relevant to the company's clad plate portfolio (e.g., Ti/Al, Cu/Al) to further diversify the technology platform.