MAY 15, 202666 MINS READ
The compositional design of maraging steel billets fundamentally determines their mechanical performance after aging treatment. Recent patent developments reveal optimized alloy systems that balance strength and ductility through controlled precipitation hardening mechanisms.
Modern maraging steel billets incorporate a carefully balanced combination of alloying elements to achieve target properties. The base composition typically includes nickel (Ni) at 15-22 wt%, which stabilizes the austenite phase at elevated temperatures and transforms to martensite upon cooling, providing the matrix for subsequent precipitation strengthening 1,3,4. Cobalt (Co) content ranging from 8-20 wt% serves dual functions: it lowers the martensite start temperature (Ms) to ensure complete transformation and enhances the precipitation kinetics of intermetallic phases during aging 1,6,14. The molybdenum (Mo) addition of 3-8 wt% contributes to solid solution strengthening and forms fine Mo-rich precipitates that impede dislocation motion 1,5,11. Titanium (Ti) at 0.4-3.0 wt% is the primary precipitation-forming element, generating Ni₃Ti intermetallic compounds during aging that provide the characteristic ultra-high strength of maraging steels 2,5,6.
A recent innovation disclosed in patent 1 describes a maraging steel billet composition containing Co: 12-17 wt%, Mo: 6-8 wt%, Ti: 0.4-1.5 wt%, Ni: 15-18 wt%, and Al ≤0.3 wt%, with the remainder being Fe and impurities. This composition achieves both high strength (>1800 MPa tensile strength) and high plasticity (>8% elongation) through optimized precipitation behavior 1. The patent emphasizes that the Co/Mo/Ti ratio critically influences the balance between strength and ductility, with the specific ranges enabling formation of coherent Ni₃Ti precipitates without excessive coarsening during aging 1.
The nitrogen content in maraging steel billets requires stringent control to minimize titanium nitride (TiN) formation, which serves as a fatigue crack initiation site in high-cycle applications 3,4,5. Patent 5 specifies that the remelt electrode should contain nitrogen (N) at 0.0025-0.0050 mass% to reduce TiN content while maintaining sufficient nitrogen for grain refinement 5. This narrow nitrogen window is achieved through vacuum induction melting (VIM) followed by vacuum arc remelting (VAR) or electroslag remelting (ESR) processes 2,5,13.
Patent 3 and 4 describe maraging steel compositions for metallic belts where Ti content is limited to ≤0.1 wt% specifically to minimize TiN formation, while maintaining adequate precipitation strengthening through increased aluminum (Al: up to 2.5 wt%) and the relationship Co/3 + Mo + 4Al = 8.0-15.0 3,4. This compositional strategy demonstrates that for applications requiring superior flexural fatigue strength, reducing TiN-forming potential takes precedence over maximizing Ti-based precipitation 3.
Beyond primary alloying elements, trace additions significantly influence billet quality and final component performance. Aluminum (Al) at 0.01-0.2 wt% acts as a deoxidizer and forms fine Al-Ni precipitates that contribute to age hardening 6,14. Chromium (Cr) additions of 0.1-5.0 wt% improve corrosion resistance and contribute to solid solution strengthening, with higher Cr contents (11-15 wt%) enabling corrosion-resistant maraging steel variants for specialized applications 16. Patent 6 describes a maraging steel billet composition with Cr: 5.0% or less, which after reverse transformation heat treatment (austenite reversion followed by re-transformation to martensite) achieves an area fraction of 25-75% reversed martensite, resulting in exceptional combination of strength (>1900 MPa) and impact toughness (>50 J at room temperature) 6,14.
Silicon (Si) and manganese (Mn) are typically restricted to ≤0.3 wt% each to avoid formation of undesirable phases and maintain matrix purity 6,11,14. Impurity elements including phosphorus (P), sulfur (S), and oxygen (O) must be controlled to ≤0.01 wt% to prevent embrittlement and ensure adequate toughness 1,6,14. Patent 13 introduces a novel approach where magnesium (Mg) is intentionally added during primary vacuum melting to form MgO inclusions that act as nucleation sites for subsequent precipitation, improving the uniformity of precipitate distribution in the final billet 13.
The manufacturing of maraging steel billets demands multi-stage melting and refining processes to achieve the required cleanliness, compositional homogeneity, and microstructural uniformity necessary for critical applications.
The production sequence typically begins with vacuum induction melting (VIM) to produce a consumable electrode (remelt electrode) with controlled composition and minimal gas content 2,5,13. Patent 5 specifies that the VIM process should produce an electrode containing Ti: 0.2-3.0 mass% and N: 0.0025-0.0050 mass%, with the vacuum level maintained to achieve a leak rate of at least 3 Pa/min during melting 13. This leak rate specification ensures sufficient vacuum quality to minimize nitrogen pickup while allowing practical production rates 13.
During VIM, the charge materials (pure metals and master alloys) are melted in a refractory crucible under vacuum (typically 10⁻² to 10⁻³ mbar) at temperatures of 1550-1650°C 2,5. The molten steel is held for 30-60 minutes to ensure compositional homogeneity and allow dissolved gases (particularly hydrogen) to escape 5,13. Patent 13 describes an innovative MgO formation step where magnesium is added to the molten steel during VIM, forming MgO particles that remain in the solidified electrode and later serve as heterogeneous nucleation sites during VAR, promoting finer grain structure in the final billet 13.
The VIM electrode is subsequently remelted using vacuum arc remelting (VAR) to produce the final maraging steel billet with superior cleanliness and structural integrity 2,5,13. Patent 5 emphasizes that VAR is essential for producing billets with average diameter ≥650 mm, as this size range exhibits reduced variability in fatigue test results and maintains high fatigue strength regardless of specimen location within the billet 5. The VAR process operates under high vacuum (10⁻⁴ to 10⁻⁵ mbar) with the consumable electrode serving as the cathode, which is progressively melted by an electric arc and solidifies in a water-cooled copper crucible 2,5.
Critical VAR parameters include melt rate of 3-8 kg/min, arc voltage of 25-35 V, and arc current of 4000-8000 A depending on ingot diameter 5,13. The controlled solidification during VAR refines the microstructure, eliminates macro-segregation, and significantly reduces inclusion content compared to the VIM electrode 5. Patent 2 specifies that for Ti-containing maraging steels (0.2-3.0 mass% Ti), the VAR process must be carefully controlled to prevent excessive TiN formation, which is achieved by maintaining the nitrogen content in the VIM electrode within the narrow range of 0.0025-0.0050 mass% 2,5.
While VAR is the predominant remelting technology, electroslag remelting (ESR) offers advantages for certain maraging steel billet applications, particularly when superior surface quality and reduced segregation are priorities 13. ESR involves remelting the consumable electrode through a molten slag layer (typically CaF₂-Al₂O₃-CaO system) that refines the steel through chemical reactions and provides a protective atmosphere 13. The slag temperature is maintained at 1700-1850°C, and the process operates at lower current densities than VAR, resulting in slower solidification rates that can enhance homogeneity 13.
However, ESR introduces the risk of slag inclusions and is less effective at removing dissolved gases compared to VAR, making it less suitable for aerospace-grade maraging steel billets where fatigue performance is critical 5,13. Patent 13 suggests that a hybrid approach—VIM followed by VAR with MgO-modified electrodes—provides optimal balance of cleanliness, homogeneity, and inclusion control for demanding applications 13.
After VAR or ESR, the solidified ingot undergoes surface conditioning to remove any surface defects, oxide scale, or segregation zones 5,11. This typically involves machining or grinding to remove 5-15 mm from the surface, followed by ultrasonic inspection to verify internal soundness 5,11. The conditioned billet may then undergo homogenization heat treatment at 1150-1250°C for 2-6 hours to eliminate any residual microsegregation and ensure uniform distribution of alloying elements 11,15.
Patent 11 describes a complete manufacturing sequence for high-strength maraging steel plate starting from billet: smelting → forging → rolling → solution treatment (820-900°C) → cryogenic treatment (-70 to -196°C) → aging treatment (450-500°C for 3-6 hours) 11. The initial billet produced by VAR serves as the starting material for the forging process, which is conducted at 1100-1200°C with total reduction ratio of 3:1 to 6:1 to refine the grain structure and eliminate any residual casting defects 11,15.
The conversion of as-cast maraging steel billets into semi-finished or finished products involves carefully controlled thermomechanical processing that influences the final microstructure and mechanical properties.
Hot forging of maraging steel billets is typically performed in the austenite stability range at 1100-1250°C to achieve significant grain refinement and microstructural homogenization 9,11,15. Patent 9 describes a thermal grain refinement method specifically for coarse-grained maraging steel billets, involving repeated heating to 1700-1900°F (927-1038°C) followed by cooling below the martensite finish temperature (Mf) 9. When this heating-cooling cycle is repeated three times, the grain size is refined from coarse initial structure to a substantially uniform ASTM grain size No. 7 (approximately 32 μm) 9.
The mechanism of grain refinement during cyclic thermal treatment involves repeated austenite-to-martensite transformation, where each cycle introduces new nucleation sites for austenite formation, progressively reducing the austenite grain size and consequently the martensite packet size after transformation 9. This approach is particularly valuable for salvaging coarse-grained billets that may result from suboptimal casting conditions 9.
Patent 15 discloses an innovative thermomechanical processing method combined with direct aging, where the maraging steel billet is worked (forged or rolled) at the austenite solutionizing temperature (typically 815-900°C for 18Ni maraging steels) and then directly aged at 450-510°C without intermediate solution treatment 15. This process produces a microstructure with fine precipitates distributed within the martensitic matrix, achieving ultimate tensile strength >1830 MPa (265 ksi) while eliminating the energy-intensive solution treatment step 15. The direct aging approach is economically advantageous and reduces processing time by 40-60% compared to conventional solution-aging sequences 15.
For applications requiring plate or sheet products, maraging steel billets undergo hot rolling at 1050-1200°C with multiple passes to achieve the target thickness 11,17. Patent 11 specifies a rolling process for maraging steel plate production where the billet is heated to 1150-1200°C and rolled with total reduction of 80-95% to produce plate with thickness of 3-50 mm 11. The rolling temperature must be carefully controlled to remain above the austenite recrystallization temperature to ensure dynamic recrystallization occurs during deformation, refining the grain structure 11.
Patent 17 describes a specialized process for producing composite maraging steel plates where a layer of harder maraging steel powder (e.g., 18Ni-300 grade with hardness 52-56 HRC after aging) is deposited onto a slab of softer maraging steel (e.g., 18Ni-200 grade with hardness 48-52 HRC after aging) 17. The deposited layer is consolidated by hot isostatic pressing (HIP) at 1150-1200°C and 100-150 MPa for 2-4 hours, forming an intermediate composite slab that is subsequently roll-bonded at 1100-1150°C with 40-60% reduction to produce a composite plate with wear-resistant surface and tough core 17. This approach enables optimization of surface and bulk properties independently, which is valuable for tooling applications 17.
Following hot working, maraging steel billets or semi-finished products undergo solution treatment (also called austenite conditioning or solutionizing) to dissolve any precipitates formed during cooling from the forging/rolling temperature and to homogenize the austenite composition 11,15,18. The solution treatment is typically conducted at 815-900°C for 0.5-2 hours depending on section thickness, followed by air cooling or faster cooling to ensure complete transformation to martensite 11,15.
Patent 6 describes an innovative heat treatment sequence involving reverse transformation: after initial solution treatment and martensite formation, the steel is reheated to 650-750°C (within the austenite reversion temperature range) for 0.5-3 hours, causing partial reversion of martensite to austenite 6,14. Upon subsequent cooling, this reverted austenite transforms back to martensite, creating a dual-martensite microstructure with 25-75% reversed martensite 6,14. This microstructure exhibits superior combination of strength and toughness because the reversed martensite has finer lath structure and higher dislocation density than the original martensite 6,14.
The solution-treated maraging steel billet has relatively low hardness (30-35 HRC) in the as-quenched martensitic condition, providing excellent machinability for producing complex component geometries before final aging [12
| Org | Application Scenarios | Product/Project | Technical Outcomes |
|---|---|---|---|
| HUAWEI TECHNOLOGIES CO. LTD. | Electronic device structural components requiring ultra-high strength combined with formability, such as foldable smartphone hinges and precision housings. | Smartphone Chassis Components | Maraging steel billet with Co 12-17wt%, Mo 6-8wt%, Ti 0.4-1.5wt% achieves tensile strength >1800 MPa with elongation >8%, providing both high strength and high plasticity for structural components. |
| HITACHI METALS LTD. | Critical aerospace applications including turbine disks and landing gear components where consistent fatigue performance across large-diameter billets is essential. | Aerospace Engine Components | Vacuum melting process producing maraging steel billets with average diameter ≥650mm, Ti content 0.2-3.0 mass% and controlled N content 0.0025-0.0050 mass%, reducing fatigue test result variation and maintaining high fatigue strength regardless of specimen location. |
| HITACHI METALS LTD. | Continuously variable transmission (CVT) metallic belts in automotive powertrains requiring superior flexural fatigue resistance under high-cycle loading conditions. | CVT Metallic Belt Systems | Maraging steel billet composition with Ti ≤0.1wt%, Co/3+Mo+4Al=8.0-15.0, minimizing TiN formation to improve flexural fatigue strength in high-cycle applications, with nitrided surface layer providing enhanced compressive residual stress. |
| KABUSHIKI KAISHA KOBE SEIKO SHO | Precision tooling and dies for metal forming operations requiring exceptional combination of ultra-high strength and impact resistance to prevent catastrophic failure. | High-Toughness Tooling Materials | Reverse transformation heat treatment of maraging steel billets creating dual-martensite microstructure with 25-75% reversed martensite, achieving tensile strength >1900 MPa with impact toughness >50J at room temperature. |
| UNITED TECHNOLOGIES CORPORATION | Aerospace gas turbine engine components including compressor blades and structural casings where cost-effective manufacturing of ultra-high-strength parts is critical. | Gas Turbine Components | Direct aging process for maraging steel billets after thermomechanical processing at austenite solutionizing temperature, achieving ultimate tensile strength >1830 MPa while eliminating solution treatment step, reducing processing time by 40-60%. |