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Chromium Molybdenum Steel Normalized Steel: Comprehensive Analysis Of Composition, Heat Treatment, And Industrial Applications

MAY 26, 202656 MINS READ

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Chromium molybdenum steel normalized steel represents a critical class of heat-resistant alloys extensively utilized in pressure vessels, power generation equipment, and high-temperature structural components. This steel category combines chromium (0.5–6.0 wt%) and molybdenum (0.4–1.5 wt%) to achieve superior creep strength, oxidation resistance, and mechanical stability under thermal cycling conditions. Normalizing heat treatment—typically conducted at 1,100–1,250°C followed by air cooling—refines the microstructure to a uniform fine-grained bainite or tempered martensite, ensuring optimal balance between strength and ductility for demanding service environments 1,2,3.
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Chemical Composition And Alloying Strategy Of Chromium Molybdenum Steel Normalized Steel

Chromium molybdenum steel normalized steel derives its performance from precise control of alloying elements and their synergistic interactions. The base composition typically includes 0.05–0.20 wt% carbon, which is intentionally kept low to minimize weld heat-affected zone (HAZ) embrittlement and improve ductility after stress relief annealing 1,8. Carbon content directly influences hardenability and carbide precipitation behavior: steels with 0.08–0.12 wt% C exhibit fine bainite structures post-normalization, whereas higher carbon levels (0.15–0.20 wt%) promote tempered martensite with enhanced tensile strength but reduced toughness 4,7.

Chromium is added in the range of 0.8–6.0 wt% to provide oxidation resistance and solid-solution strengthening 5,13. In pressure vessel applications, Cr content of 1.0–2.5 wt% is standard, forming stable Cr₂₃C₆ carbides that pin grain boundaries and resist coarsening at elevated temperatures 3,7. Molybdenum (0.4–1.5 wt%) serves dual roles: it retards carbide coagulation during long-term exposure at 500–600°C and enhances creep resistance by forming fine Mo₂C precipitates 4,18. The synergy between Cr and Mo is critical—steels with Cr+Mo totals of 2.5–4.0 wt% demonstrate optimal creep rupture life exceeding 100,000 hours at 550°C 7,18.

Microalloying additions further refine performance:

  • Vanadium (0.05–1.0 wt%): Forms fine V(C,N) carbonitrides that inhibit austenite grain growth during normalizing and provide precipitation strengthening during tempering 7,11,16. Steels with 0.65–1.0 wt% V exhibit 15–20% higher creep strength than V-free grades 18.
  • Niobium (0.005–0.07 wt%): Acts as a grain refiner by forming Nb(C,N) particles that resist dissolution even at normalizing temperatures above 1,150°C 6,8,16. This eliminates the need for post-weld normalizing in certain applications 6.
  • Aluminum (0.01–0.10 wt%): Deoxidizes the melt and forms AlN precipitates that stabilize fine grain size 1,4. Acid-soluble Al content of 0.04–0.08 wt% is optimal for enhancing boron hardenability effects 1.
  • Boron (0.0003–0.004 wt%): Dramatically improves hardenability in thick sections (>100 mm) by segregating to austenite grain boundaries and suppressing ferrite nucleation 1,10. Effective only when Ti or Al is present to tie up nitrogen as TiN or AlN, preventing BN formation 10.

Impurity control is equally critical. Phosphorus must be limited to ≤0.015 wt% and sulfur to ≤0.010 wt% to minimize temper embrittlement and reheat cracking susceptibility 8,13,17. Calcium treatment (0.0005–0.005 wt% Ca) with Ca/S ratios of 1–10 modifies sulfide morphology from elongated MnS stringers to globular CaS particles, improving transverse ductility and resistance to hydrogen-induced cracking 12,17.

Normalizing Heat Treatment Process And Microstructural Evolution

Normalizing is the cornerstone heat treatment for chromium molybdenum steel, designed to homogenize the microstructure, refine grain size, and establish a baseline for subsequent tempering. The process involves heating the steel to the austenite region—typically 1,100–1,250°C—holding for sufficient time to dissolve carbides and homogenize alloying elements, then air cooling to room temperature 2,3,16.

Austenitization Temperature Selection

The austenitization temperature must be carefully selected based on alloy composition:

  • For low-carbon grades (0.05–0.12 wt% C) with 1.0–2.5 wt% Cr and 0.4–1.0 wt% Mo, normalizing at 1,100–1,150°C ensures complete carbide dissolution while limiting austenite grain growth 3,12.
  • High-strength variants with 0.15–0.20 wt% C and elevated V content (0.65–1.0 wt%) require 1,150–1,200°C to dissolve V(C,N) precipitates, which otherwise remain undissolved and reduce hardenability 16,18.
  • Temperatures exceeding 1,250°C cause excessive grain coarsening (ASTM grain size <3), leading to reduced toughness and increased susceptibility to intergranular cracking during subsequent welding 16.

Holding time at austenitization temperature typically ranges from 30 minutes for thin sections (<25 mm) to 2 hours for heavy forgings (>200 mm), ensuring through-thickness temperature uniformity 3,11.

Cooling Rate And Transformation Behavior

Post-austenitization cooling rate governs the final microstructure. Air cooling from normalizing temperature produces cooling rates of 0.4–1.1°C/s at the center of thick sections (170–330 mm diameter), which is sufficient to suppress ferrite-pearlite formation and promote bainite transformation in Cr-Mo steels 11. The continuous cooling transformation (CCT) behavior is composition-dependent:

  • Steels with Cr+Mo ≥3.0 wt% and B addition exhibit bainite start temperatures (Bs) of 500–550°C, ensuring fully bainitic structures even in sections up to 300 mm diameter 10,11.
  • Lower-alloy grades (Cr+Mo <2.5 wt%) may form mixed ferrite-bainite structures in thick sections unless accelerated cooling (fan air or mist cooling) is applied 19.

The resulting normalized microstructure consists of fine bainite with lath widths of 0.5–2.0 μm, interspersed with fine carbides (primarily M₂₃C₆ and M₂C types) 1,7. This structure provides an optimal combination of strength (yield strength 350–450 MPa) and toughness (Charpy V-notch impact energy >60 J at room temperature) 3,9.

Post-Normalization Tempering

Normalized chromium molybdenum steel is invariably tempered to relieve residual stresses, reduce hardness to machinable levels, and optimize the carbide distribution. Tempering is conducted at 650–730°C for 1–4 hours, depending on section thickness and target mechanical properties 3,11,13. During tempering:

  • Retained austenite (if present) transforms to bainite or tempered martensite.
  • Bainitic ferrite undergoes recovery, reducing dislocation density.
  • Fine M₂C carbides precipitate within lath interiors, providing dispersion strengthening 7,18.
  • Coarse M₂₃C₆ carbides form at prior austenite grain boundaries and lath boundaries, pinning these interfaces and enhancing creep resistance 18.

Tempering at 680–700°C produces tensile strengths of 550–650 MPa with elongations of 18–22% and reduction of area >50%, meeting ASME Section VIII Division 1 requirements for pressure vessel steels 3,9.

Mechanical Properties And Performance Characteristics

Tensile And Yield Strength

Normalized and tempered chromium molybdenum steel exhibits tensile strengths ranging from 550 MPa to 1,100 MPa, depending on carbon content and tempering temperature 9,15. Low-carbon variants (0.08–0.12 wt% C) tempered at 680–700°C achieve:

  • Yield strength (YS): 350–450 MPa
  • Tensile strength (UTS): 550–650 MPa
  • Elongation: 18–22%
  • Reduction of area: 50–60% 3,9

Medium-carbon grades (0.30–0.50 wt% C) subjected to quenching and high-frequency surface tempering can attain UTS ≥1,100 MPa with core hardness of 400 HV and surface hardness of 340 HV, suitable for high-strength fasteners and PC steel bars 15.

Creep Strength And High-Temperature Performance

Creep resistance is the defining attribute for chromium molybdenum steel in power generation and petrochemical applications. Steels with 2.0–2.5 wt% Cr, 0.9–1.1 wt% Mo, and 0.65–1.0 wt% V demonstrate creep rupture strengths of 100–120 MPa at 600°C for 100,000 hours, outperforming ASTM A387 Grade 22 (2.25Cr-1Mo) by 20–30% 7,18. The superior creep performance derives from:

  • Fine V(C,N) and Mo₂C precipitates (5–20 nm diameter) that pin dislocations and subgrain boundaries, inhibiting recovery and grain boundary sliding 7,18.
  • Stable M₂₃C₆ carbides at prior austenite grain boundaries that resist coarsening via Ostwald ripening, maintaining boundary pinning forces during prolonged exposure 18.
  • Low carbon content (0.11–0.15 wt%) that minimizes thermodynamically unstable cementite formation, reducing the driving force for carbide coagulation 7.

Creep testing at 600°C under 100 MPa stress reveals minimum creep rates of 1×10⁻⁹ s⁻¹ for optimized compositions, with creep life exceeding 150,000 hours 18.

Toughness And Ductility

Charpy V-notch impact toughness is critical for pressure vessel applications subject to thermal shock and cyclic loading. Normalized and tempered Cr-Mo steels exhibit:

  • Room temperature impact energy: 60–100 J
  • Transition temperature (50% shear fracture): -20 to 0°C 3,9

Toughness is maximized by:

  • Fine grain size (ASTM 7–9) achieved through Nb or V microalloying and controlled normalizing 6,8.
  • Low impurity levels (P ≤0.010 wt%, S ≤0.008 wt%) to minimize grain boundary segregation 13,17.
  • Calcium treatment to spheroidize sulfides, eliminating crack initiation sites 17.

Hardenability And Through-Thickness Property Uniformity

Hardenability—the ability to form martensite or bainite throughout thick sections—is enhanced by boron additions and optimized Cr+Mo content. Steels with 0.001–0.0035 wt% B and Cr+Mo totals of 2.5–3.5 wt% achieve critical diameter (Dc) values of 200–300 mm, ensuring uniform properties in heavy forgings and thick-walled pressure vessels 10. Jominy end-quench tests show hardness gradients of 40 HV/mm from surface to core in 150 mm diameter bars, confirming excellent hardenability 10,15.

Welding Considerations And Heat-Affected Zone Behavior

Chromium molybdenum steel normalized steel is widely welded using gas tungsten arc welding (GTAW), shielded metal arc welding (SMAW), and submerged arc welding (SAW) processes. However, the HAZ is susceptible to several degradation mechanisms that must be mitigated through proper welding procedures and post-weld heat treatment (PWHT).

Weld Heat-Affected Zone Embrittlement

The HAZ adjacent to the fusion line experiences peak temperatures of 1,200–1,400°C, causing austenite grain coarsening and formation of untempered martensite upon cooling 2,13. This coarse-grained HAZ exhibits reduced toughness (impact energy <30 J) and increased susceptibility to cold cracking. Mitigation strategies include:

  • Preheat to 150–250°C to reduce cooling rates and promote bainite rather than martensite formation 2.
  • Interpass temperature control (≤300°C) to limit cumulative heat input and minimize HAZ width 2.
  • Low-hydrogen electrodes (E7018 or equivalent) to prevent hydrogen-induced cracking 12.

Post-Weld Heat Treatment

PWHT is mandatory for Cr-Mo steel pressure vessels per ASME Section VIII. The standard PWHT cycle involves:

  • Heating at ≤200°C/hour to the hold temperature of 680–730°C 3,13.
  • Holding for 1 hour per 25 mm of thickness (minimum 1 hour) 3.
  • Cooling at ≤300°C/hour to 300°C, then air cooling 3.

PWHT tempers the HAZ martensite, precipitates fine carbides, and relieves residual stresses, restoring toughness to >60 J and reducing hardness to <250 HV 13. However, prolonged PWHT (>4 hours at 700°C) can induce temper embrittlement in steels with high P, Sn, or Sb content, necessitating strict impurity control 13,17.

Reheat Cracking Resistance

Reheat cracking—intergranular cracking in the HAZ during PWHT—is a critical concern for thick-section Cr-Mo steel welds. Cracking occurs due to stress concentration at grain boundaries weakened by carbide precipitation and impurity segregation 17. Resistance is improved by:

  • Reducing carbon to <0.12 wt% to limit M₂₃C₆ precipitation at grain boundaries 17.
  • Adding 0.005–0.015 wt% Ti to form fine TiC particles that pin boundaries 17.
  • Controlling Cu+Ni to 0.25–1.2 wt% and Ca/S ratio to 1–10 to modify sulfide morphology 17.

Steels meeting these criteria exhibit reheat crack ratios <5% in Varestraint testing, compared to >20% for conventional compositions 17.

Innovative Welding Techniques

Recent patents disclose methods to eliminate HAZ weakening by subjecting normalized steel to partial tempering (500–600°C) prior to welding, followed by full tempering (680–700°C) post-weld 2. This pre-temper treatment reduces the hardness differential between base metal and HAZ, minimizing stress concentration and improving fatigue life by 30–50% 2.

Applications Of Chromium Molybdenum Steel Normalized Steel In Industrial Sectors

Pressure Vessels And Boilers For Power Generation

Chromium molybdenum steel normalized steel is the material of choice for fossil-fuel and nuclear power plant pressure vessels operating at 500–600°C and pressures up to 20 MPa 1,3,7. Typical applications include:

  • Boiler drums
OrgApplication ScenariosProduct/ProjectTechnical Outcomes
KAWASAKI SEITETSU KKPressure vessels for chemical plants and power generation facilities operating at elevated temperatures requiring long-term stress relief annealing resistance.Low Carbon Cr-Mo Pressure Vessel SteelUniform fine bainite structure with 0.02-0.08% C, 0.04-0.1% Al, and 0.0003-0.0040% B achieves superior strength and toughness after high-temperature stress relief annealing while maintaining excellent weldability and reduced cracking susceptibility.
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE UNITED STATES DEPARTMENT OF ENERGYWelded structural components and pressure vessels in power generation systems requiring enhanced weld joint integrity and resistance to HAZ embrittlement.Welded Cr-Mo Steel ComponentsPartial tempering at 500-600°C prior to welding followed by full tempering at 680-700°C eliminates heat-affected zone weakening, improving fatigue life by 30-50% and optimizing strength-ductility balance.
POSCOBoiler tubes, pressure vessels, and high-temperature structural components in fossil-fuel and nuclear power plants operating at 500-600°C under sustained loading conditions.High Creep Strength Cr-Mo Steel PlateControlled composition (C: 0.11-0.15%, Cr: 2.0-2.5%, Mo: 0.9-1.1%, V: 0.65-1.0%) with optimized heat treatment produces fine carbonitrides that achieve creep rupture strength of 100-120 MPa at 600°C for 100,000+ hours, outperforming ASTM A387 Grade 91 by 20-30%.
JAPAN STEEL WORKS LTDHeavy forgings, thick-walled pressure vessels, and large-diameter components requiring through-thickness property uniformity in petrochemical and power generation equipment.High Hardenability Cr-Mo SteelAddition of 0.001-0.0035% B with 1.00-2.50% Cr and 0.45-1.10% Mo achieves critical diameter of 200-300 mm with hardness gradient <40 HV/mm, ensuring uniform properties in thick sections up to 300 mm diameter.
MITSUBISHI HEAVY INDUSTRIES LTD.High-temperature piping systems, boiler tubes, and structural components in power generation facilities requiring superior creep strength and thermal cycling resistance above 500°C.High-Strength Heat-Resistant Steel PipeNormalizing at 1,100-1,250°C followed by hot working with ≥50% final reduction ratio and controlled cooling produces fine-grained microstructure with V, Nb, Ti carbonitrides that provide enhanced creep resistance and mechanical stability at elevated temperatures.
Reference
  • Chromium molybdenum steel with low carbon content for pressure vessel
    PatentInactiveJP1982041355A
    View detail
  • Method for welding chromium molybdenum steels
    PatentInactiveUS4612070A
    View detail
  • Manufacture of high toughness chromium molybdenum steel covered with stainless steel
    PatentInactiveJP1986076613A
    View detail
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