1. Material Composition & Manufacturing Process
5A06 H112 aluminum forged ring is a high-strength, non-heat-treatable aluminum-magnesium alloy (Al-Mg series) particularly renowned for its excellent corrosion resistance (especially to seawater), good weldability, moderate strength, and superior cryogenic properties. The H112 temper indicates that the material has been forged and subsequently not subjected to precise cold working or heat treatment, thus retaining its forged microstructure and some residual stress. Through a precise forging process, its internal microstructure is optimized, with grain flow aligned along the ring’s geometry, making it an ideal choice for applications demanding extreme corrosion resistance, weldability, and cryogenic toughness, such as shipbuilding, offshore engineering, nuclear industry, cryogenic equipment, and pressure vessels:
Primary Alloying Elements:
Magnesium (Mg): 5.8-6.8% (primary strengthening element, provides high strength and good weldability)
Manganese (Mn): 0.5-0.8% (further enhances strength and refines grain)
Chromium (Cr): 0.10-0.20% (inhibits recrystallization, improves stress corrosion resistance)
Titanium (Ti): 0.02-0.10% (grain refinement)
Base Material:
Aluminum (Al): Balance
Controlled Impurities:
Iron (Fe): ≤0.25% max
Silicon (Si): ≤0.40% max
Copper (Cu): ≤0.10% max
Zinc (Zn): ≤0.20% max
Beryllium (Be): 0.0001-0.005% (inhibits oxidation)
Other elements: ≤0.05% each, ≤0.15% total
Premium Forging Process:
Melt Preparation:
High-purity primary aluminum
Precise control of alloying elements with ±0.05% tolerance
Advanced filtration and degassing treatments (e.g., SNIF or rotary degassing) ensure melt cleanliness
Grain refinement (typically with Al-Ti-B master alloy)
Direct-Chill (DC) semi-continuous casting to produce high-quality ingots
Homogenization:
450-480°C for 8-16 hours
Uniform temperature control: ±5°C
Ensures uniform distribution of alloying elements and eliminates microsegregation
Billet Preparation:
Ingot surface conditioning (scalping or milling)
Ultrasonic inspection to ensure internal flawlessness
Preheating: 380-420°C, with precise temperature uniformity control
Forging Sequence (Ring Forging):
Upsetting: Forging the ingot into a disk or preform ring at 380-420°C
Piercing/Punching: Creating a central hole using intermediate dies or mandrels, gradually forming the ring shape
Ring Rolling: Using a ring rolling machine to axially and radially expand the ring preform, further refining grain structure and controlling dimensions
Die Forging Finish: Final shaping in dies to ensure geometric precision and surface finish
Forging Temperature: 350-400°C
Forging Pressure: Thousands of tons, depending on ring size and complexity
Minimum Reduction Ratio: 3:1 to 5:1, ensuring dense, uniform internal structure, elimination of cast structure, and formation of optimized grain flow
Annealing (Optional):
If further processing or microstructural adjustment is needed, annealing can be performed after forging to achieve the O temper.
H112 Temper Formation:
After forging, the material undergoes only minor mechanical processing (if needed), such as flattening or straightening, without further heat treatment or cold working, retaining its as-forged condition.
All production stages are subject to stringent quality control, non-destructive testing, and traceability management.
2. Mechanical Properties of 5A06 H112 Forged Ring
Property | H112 | Test Method |
Ultimate Tensile Strength | 300-340 MPa | ASTM E8 |
Yield Strength (0.2%) | 150-180 MPa | ASTM E8 |
Elongation (2 inch) | 16-22% | ASTM E8 |
Hardness (Brinell) | 70-85 HB | ASTM E10 |
Fatigue Strength (5×10⁸ Cycles) | 120-150 MPa | ASTM E466 |
Shear Strength | 170-200 MPa | ASTM B769 |
Fracture Toughness (K1C, typical) | 28-35 MPa√m | ASTM E399 |
Property Distribution:
Radial vs. Tangential properties: Forged rings exhibit good anisotropy, with grain flow distributed tangentially (circumferentially), providing higher tangential strength and fatigue resistance.
Wall thickness effect on properties: Strength may slightly increase in thinner wall sections.
Core to surface hardness variation: Less than 5 HB.
Residual Stress: H112 temper retains some residual stress from forging; if sensitivity to residual stress is a concern, subsequent processing may require stress relief.
Fatigue Performance: Optimized grain flow formed by the forging process helps improve the material’s fatigue life.
Cryogenic Performance: Strength and toughness even improve in extremely low-temperature environments, with no brittle transition, making it an excellent cryogenic structural material.
3. Microstructural Characteristics
Key Microstructural Features:
Grain Structure:
Fine, uniform mixed structure of recrystallized grains and elongated non-recrystallized grains aligned tangentially
Grain flow highly matched with the ring’s geometry, uniformly distributed tangentially, maximizing material performance
Fine dispersoids formed by Manganese (Mn), Chromium (Cr), and Titanium (Ti) effectively inhibit grain growth and recrystallization
ASTM grain size 6-9 (45-16μm)
Precipitate Distribution:
β-Mg₅Al₈ phase: Fine and uniformly dispersed, acting as the primary strengthening phase
Mg-Al intermetallic compounds: Distribution at grain boundaries effectively controlled to avoid stress corrosion sensitivity
Small amounts of primary intermetallic compounds like AlFeMn are effectively broken down and dispersed
Texture Development:
Forging process creates specific texture beneficial for tangential properties
Special Features:
High metallurgical cleanliness, minimizing non-metallic inclusion defects
Controlled continuous precipitation of beta-phase at grain boundaries enhances stress corrosion resistance
4. Dimensional Specifications & Tolerances
Parameter | Standard Range | Precision Tolerance | Commercial Tolerance | Test Method |
Outer Diameter | 100-2000 mm | ±0.8mm up to 500mm | ±1.5mm up to 500mm | Micrometer/CMM |
±0.2% above 500mm | ±0.4% above 500mm | |||
Inner Diameter | 80-1900 mm | ±0.8mm up to 500mm | ±1.5mm up to 500mm | Micrometer/CMM |
±0.2% above 500mm | ±0.4% above 500mm | |||
Wall Thickness | 10-400 mm | ±0.5mm | ±1.0mm | Micrometer/CMM |
Height | 20-600 mm | ±0.5mm | ±1.0mm | Micrometer/CMM |
Flatness | N/A | 0.2mm/100mm Diameter | 0.4mm/100mm Diameter | Flatness Gauge/CMM |
Concentricity | N/A | 0.2mm | 0.4mm | Concentricity Gauge/CMM |
Surface Roughness | N/A | 6.3 μm Ra max | 12.5 μm Ra max | Profilometer |
Standard Available Forms:
Forged Rings: Outer diameter 100mm to 2000mm, wall thickness 10mm to 400mm
Custom dimensions and geometries available according to customer drawings and requirements
Various processing conditions available, e.g., Forged As-Is, Rough Machined
5. Temper Designations & Work Hardening Options
Temper Code | Process Description | Optimal Applications | Key Characteristics |
O | Fully annealed, softened | Applications requiring maximum formability, or subsequent deep processing | Maximum ductility, lowest strength |
H111 | Moderately strain hardened after full annealing | General structures, excellent post-weld properties | Good balance of strength and ductility |
H112 | Flattened only after forging | Suitable for further processing before machining, with residual stresses from forging | As-forged condition, moderate strength, excellent corrosion resistance |
H321 | Stabilized H32 temper | High strength, strict corrosion resistance requirements | Excellent SCC resistance, higher strength |
Temper Selection Guidance:
H112: When utilizing the as-forged microstructure and properties, and further processing is required.
O: When complex cold forming operations or maximum ductility are needed for the ring.
H111: When higher strength than H112 is required, while maintaining good ductility and weldability.
H321: When extremely high requirements for corrosion resistance (especially stress corrosion cracking) are present, along with higher strength demands.
As an Al-Mg series alloy, 5A06 is not strengthened by heat treatment; different H tempers are primarily achieved through cold working. Forging itself is a form of plastic deformation, thus H112 represents the as-forged condition.
6. Machining & Fabrication Characteristics
Operation | Tool Material | Recommended Parameters | Comments |
Turning | Carbide, PCD | Vc=150-400 m/min, f=0.1-0.4 mm/rev | Easy to achieve good surface finish, moderate tool wear |
Drilling | Carbide, TiN coated | Vc=60-150 m/min, f=0.15-0.35 mm/rev | Through-coolant drills recommended, good for deep holes |
Milling | Carbide, HSS | Vc=200-600 m/min, fz=0.1-0.25 mm | High-positive rake angle tools, large depth of cut, high feed |
Tapping | HSS-E-PM, TiCN coated | Vc=15-30 m/min | Proper lubrication for good thread quality |
Reaming | Carbide, HSS | Vc=50-100 m/min, f=0.2-0.5 mm/rev | H7/H8 tolerance achievable |
Sawing | Carbide-tipped blade | Vc=800-2000 m/min | Efficient cutting for large diameter bars |
Fabrication Guidance:
Machinability Rating: 70% (1100 aluminum = 100%), good machinability, lower than 2xxx and 7xxx alloys
Chip Formation: Gummy chips, tend to wrap around tools, requires good chip breakers
Coolant: Water-soluble cutting fluid (8-12% concentration), high flow rate cooling
Tool Wear: Moderate, regular tool inspection needed
Weldability: Excellent with TIG and MIG welding, one of the best weldable aluminum alloys
Cold Working: Good formability in O temper, moderate in H112 temper
Hot Working: Recommended temperature range 300-400°C
Stress Corrosion Cracking: H112 temper has excellent resistance to stress corrosion cracking
Cryogenic Properties: Retains or improves strength and toughness at extremely low temperatures
7. Corrosion Resistance & Protection Systems
Environment Type | Resistance Rating | Protection Method | Expected Performance |
Industrial Atmosphere | Excellent | Clean surface | 20+ years |
Marine Atmosphere | Excellent | Clean surface | 15-20+ years |
Seawater Immersion | Very Good | Cathodic protection or painting | 10-15+ years with maintenance |
High Humidity | Excellent | Clean surface | 20+ years |
Stress Corrosion | Excellent (H112 temper) | No additional protection needed | Extremely low susceptibility |
Exfoliation | Excellent | Standard protection | Extremely low susceptibility |
Galvanic Corrosion | Good | Proper isolation | Careful design with dissimilar metals |
Surface Protection Options:
Anodizing:
Type II (Sulfuric): 10-25μm thickness, provides additional protection and aesthetics
Type III (Hard): 25-75μm thickness, increases wear resistance and hardness
Dyeing and sealing: Enhances aesthetics and corrosion resistance
Conversion Coatings:
Chromate conversion coatings (MIL-DTL-5541): Excellent base for paints or adhesives
Chromium-free alternatives: Environmentally compliant
Painting Systems:
Epoxy primer + polyurethane topcoat: Provides excellent long-term protection, especially for marine applications
8. Physical Properties for Engineering Design
Property | Value | Design Consideration |
Density | 2.66 g/cm³ | Lightweight design, center of gravity control |
Melting Range | 575-635°C | Welding and casting parameters |
Thermal Conductivity | 121 W/m·K | Thermal management, heat transfer design |
Electrical Conductivity | 34% IACS | Electrical conductivity in electrical applications |
Specific Heat | 897 J/kg·K | Thermal mass and heat capacity calculations |
Thermal Expansion (CTE) | 24.0 ×10⁻⁶/K | Dimensional changes due to temperature variations |
Young’s Modulus | 70.3 GPa | Deflection and stiffness calculations |
Poisson’s Ratio | 0.33 | Structural analysis parameter |
Damping Capacity | Moderate | Vibration and noise control |
Design Considerations:
Operating Temperature Range: -200°C to +80°C (long-term use above this temperature may lead to sensitization, affecting SCC resistance)
Cryogenic Performance: Maintains or improves strength and toughness at extremely low temperatures, ideal for cryogenic structural materials
Magnetic Properties: Non-magnetic
Recyclability: 100% recyclable with high scrap value
Formability: Good in O temper, moderate in H112 temper
Dimensional Stability: Good dimensional stability after forging and stress relief
Strength-to-Weight Ratio: Advantageous in applications requiring high strength and corrosion resistance
9. Quality Assurance & Testing
Standard Testing Procedures:
Chemical Composition:
Optical emission spectroscopy
X-ray fluorescence analysis
Verification of all major elements and impurity content
Mechanical Testing:
Tensile testing (radial, tangential, axial)
Hardness testing (Brinell, multiple locations)
Impact testing (Charpy V-notch, especially for cryogenic applications)
Fatigue testing (as required)
Nondestructive Testing:
Ultrasonic inspection (100% volumetric, per ASTM B594/E2375, or AMS 2630)
Eddy current testing (surface and near-surface defects)
Penetrant inspection (surface defects)
Radiographic testing (internal macroscopic defects)
Microstructural Analysis:
Grain size determination
Precipitate and intermetallic compound evaluation
Grain flow pattern verification
Stress corrosion sensitivity testing
Dimensional Inspection:
CMM (Coordinate Measuring Machine) verification
Outer diameter, inner diameter, wall thickness, height, flatness, concentricity, etc.
Standard Certifications:
Material Test Report (EN 10204 3.1 or 3.2)
Chemical analysis certification
Mechanical properties certification
Heat treatment/forging certification
Nondestructive testing certification
Conformance to ASTM B247 (forgings), GB/T 3880 (Chinese standard), EN AW-5083/5A06, etc.
10. Applications & Design Considerations
Primary Applications:
Marine Industry:
Shipbuilding and yacht construction (hull structures, deck equipment, seawater piping)
Offshore drilling platform structural components
Desalination equipment
Submarine components
Cryogenic Engineering:
Liquefied Natural Gas (LNG) storage tanks and transfer pipeline rings
Cryogenic equipment components
Pressure Vessels:
Medium to high-pressure vessel flanges and rings
Pressure-bearing equipment components
Nuclear Industry:
Nuclear reactor cooling system components
Radiation shielding structures
Rail Transit:
High-speed train body structural components
Design Advantages:
Excellent corrosion resistance, especially in marine and industrial environments, with very high resistance to seawater corrosion
Superior weldability, with high weld strength and good ductility
Exceptional cryogenic toughness, with improved properties at extremely low temperatures
Moderate strength and good ductility, suitable for structural components
Forging process optimizes grain flow and internal quality
Excellent resistance to stress corrosion cracking and exfoliation corrosion
Lightweight, contributing to energy savings and emission reduction
Non-magnetic
Design Limitations:
Cannot be strengthened by heat treatment; strength limit is lower than 2xxx and 7xxx series high-strength alloys
Long-term use above 65°C may lead to sensitization (due to Mg₂Al₃ phase precipitation), increasing susceptibility to stress corrosion. Operating temperature needs to be controlled or H321 temper chosen.
Strength level is lower than 5083’s H116/H321 tempers, but may perform better in specific corrosive environments.
Relatively higher cost.
Economic Considerations:
High-performance material, higher initial cost but long lifespan and low maintenance costs
Excellent corrosion resistance reduces long-term protection needs
Good weldability lowers the cost of fabricating complex structures
Lightweight properties help reduce transportation fuel costs
Sustainability Aspects:
100% recyclable with high resource utilization efficiency
Aluminum production processes are becoming increasingly environmentally friendly, with reduced energy consumption
Long service life reduces waste generation
Material Selection Guidance:
Choose 5A06 H112 forged rings when high strength, exceptional corrosion resistance (especially to seawater), excellent weldability, and cryogenic properties are required, and the upper limit of strength is not as critical as for 7075/7050.
For structures serving long-term at temperatures above 65°C, H321 temper should be selected, or other alloys considered.
Suitable for critical applications in marine, cryogenic, and nuclear industries as structural and pressure-bearing components.