C-Cr-V-Ti-Nb-Zr-B Chemical Composition: VFC Microalloying in High-Chromium Cast Iron
How C, Cr, V, Ti, Nb, Zr and B change carbide chemistry, martensite fraction and heat-treated performance in high-chromium cast iron.
A C-Cr-V-Ti-Nb-Zr-B chemical composition is not created by adding seven independent marketing ingredients. The base C-Cr white iron establishes the M7C3 carbide and matrix system; a V-rich Fe-Ti-Nb-Zr-B master alloy then modifies nucleation, carbide chemistry, hardenability and phase balance during casting and heat treatment.
This guide reconstructs the published master-alloy calculation, compares phase and property results, and explains what evidence is needed before using the concept for mining wear plates. Research specimens, preliminary RFQ ranges and commercial heat guarantees are kept separate.
Base HCCI
Approximately 2.76%C and 17.91%Cr provide the high-chromium white-iron foundation.
3.1% VFC
A V-rich master alloy contributes Ti, Nb, Zr, B and additional C/Fe at controlled low levels.
Measured result
The study reports changed phase fractions, higher heat-treated hardness/toughness and lower test wear loss.
Why this Blog has a separate search role
The paired product page targets commercial searches such as wear plate for mining equipment and multi-alloy high-chrome chute liner. This Blog targets the informational phrase C-Cr-V-Ti-Nb-Zr-B chemical composition and the narrower topic VFC microalloying in high-chromium cast iron.
That distinction matters for the site’s keyword strategy. Engineers can enter through chemistry research, follow the evidence to the paired product, and then submit a drawing. Google receives one technical URL and one commercial URL instead of two near-identical pages.
| Search intent | Primary URL | Keyword theme | Next action |
|---|---|---|---|
| Composition research | This Blog | C-Cr-V-Ti-Nb-Zr-B chemical composition | Understand elements and data |
| Product sourcing | Paired product | Multi-alloy wear plates for mining equipment | Send drawing/RFQ |
| Material comparison | Selection guide | How to choose mining wear plates | Compare families |
| Broad product browsing | Wear plates category | Wear plate products | Review alternatives |
Primary research design
The 2023 Materials paper prepared a base high-chromium cast iron in a medium-frequency induction furnace, produced a V-rich multi-element master alloy by vacuum arc melting, and then remelted the base with 3.1 wt.% of that master alloy. Both base and modified materials were examined in as-cast and heat-treated conditions.
The value of the experiment is its traceable chain: defined starting chemistry, calculated addition, phase characterization, hardness, impact and wear testing. The limitation is equally important: the specimens and thermal route do not automatically represent a full-size chute liner.
Base high-chromium cast iron composition
The authors reported a base ingot containing 2.76% C, 0.27% Si, 0.52% Mn, 17.91% Cr, 0.12% Mo and 0.22% Ni by mass, with iron as the balance. That chemistry is a high-chromium white cast iron rather than a low-alloy cast steel.
Carbon and chromium create the primary M7C3 carbide/matrix architecture. Modest Mo and Ni influence hardenability and retained-austenite behavior. Si and Mn support melting and transformation control.
| Base HCCI element | C | Si | Mn | Cr | Mo | Ni | Fe |
|---|---|---|---|---|---|---|---|
| Reported wt.% | 2.76 | 0.27 | 0.52 | 17.91 | 0.12 | 0.22 | Balance |
VFC master-alloy composition
The separate VFC ingot contained 75.9% V, 12.6% Fe, 5.0% Ti, 3.1% Nb, 2.2% Zr, 0.6% C and 0.6% B. Vanadium therefore dominated the master alloy; Ti, Nb, Zr and B were supporting additions rather than equal fractions.
The name VFC is a convenient label from the paper, not a universal commercial master-alloy designation. A supplier may use different ferroalloys or addition sequences if the final heat chemistry and qualified microstructure are achieved.
| VFC master alloy | V | Fe | Ti | Nb | Zr | C | B |
|---|---|---|---|---|---|---|---|
| Reported wt.% | 75.9 | 12.6 | 5.0 | 3.1 | 2.2 | 0.6 | 0.6 |
Calculating the 3.1% VFC addition
Multiplying each master-alloy fraction by the 3.1% addition gives the approximate contribution to the melt. The paper states additions equivalent to 2.29% V, 0.46% Fe, 0.15% Ti, 0.10% Nb, 0.07% Zr, 0.02% C and 0.02% B.
This mass-balance step is useful for checking a technical claim. It still describes charge addition, not guaranteed recovery. Oxidation, slag reaction, holding and sampling can make final heat analysis differ from the nominal calculation.
| Added through 3.1% VFC | V | Fe | Ti | Nb | Zr | C | B |
|---|---|---|---|---|---|---|---|
| Approx. wt.% contribution | 2.29 | 0.46 | 0.15 | 0.10 | 0.07 | 0.02 | 0.02 |
Approximate research alloy after addition
A simple addition of the reported base and contribution suggests roughly 2.78% C, 17.91% Cr, 2.29% V, 0.15% Ti, 0.10% Nb, 0.07% Zr and 0.02% B before accounting for dilution details, recovery or any change during remelting. Si, Mn, Mo and Ni remain part of the system.
This reconstructed row is educational, not a substitute for the authors’ measured final heat or a production certificate. Commercial acceptance must use actual analysis with defined methods and permissible variation.
| Reconstructed alloy concept | C | Cr | V | Ti | Nb | Zr | B |
|---|---|---|---|---|---|---|---|
| Approx. nominal wt.% | 2.78 | 17.91 | 2.29 | 0.15 | 0.10 | 0.07 | 0.02 |
| Commercial result | Heat analysis | Heat analysis | Heat analysis | Heat analysis | Heat analysis | Heat analysis | Heat analysis |
Carbon and chromium establish M7C3
At nearly 2.8% C and 18% Cr, solidification creates a substantial population of chromium-rich M7C3-type carbides within an iron-based matrix. Their volume, continuity, orientation and spacing depend on Cr/C balance and cooling. These carbides resist cutting but can crack when contact stress or impact is excessive.
Multi-element additions modify this foundation; they do not replace it. A wear plate still succeeds or fails according to how the primary carbide network is supported by the matrix and backing.
Vanadium is not a micro-trace here
The calculated 2.29% V addition is large compared with Ti, Nb, Zr and B. Vanadium can enter alloyed carbide lattices, contribute V-rich compounds and affect matrix hardenability. The paper’s EDS interpretation and phase results indicate a genuine multicomponent structural change.
Because V is oxidation-sensitive, actual recovery and distribution matter. A supplier must control addition form, melt temperature, holding and mixing; total V alone does not reveal particle size or location.
Titanium and niobium as strong carbide formers
Ti and Nb additions of approximately 0.15% and 0.10% are small but chemically potent. Both have strong affinity for carbon and can influence nucleation, refinement and hard-particle formation. Their effect depends on local supersaturation and solidification sequence.
Fine dispersed particles may help refinement; coarse clusters may become crack or pull-out sites. This is why microalloying requires more than a target chemistry table.
Zirconium and boron at low concentration
The calculated 0.07% Zr and 0.02% B additions can influence inclusions, nucleation, grain boundaries and carbide/boride chemistry. The study described Zr and small V contributions within matrix phases and B-containing multicomponent carbides.
Low values challenge analytical resolution. Laboratory method, detection limit and sampling should be agreed if these elements are contractual.
| Highlighted element | Approx. addition | Likely metallurgical role | Verification need |
|---|---|---|---|
| V | 2.29% | Alloy carbide/matrix hardenability | Heat analysis + structure |
| Ti | 0.15% | Carbide/nucleation refinement | Analysis + representative microscopy |
| Nb | 0.10% | Strong carbide-forming/refinement | Analysis + phase/distribution evidence |
| Zr | 0.07% | Inclusion/nucleation/matrix interaction | Low-level analysis |
| B | 0.02% | Carbide/boride and boundary effects | Suitable B method + structure |
From M7C3 to multi-element M7(C,B)3
The researchers concluded that V, Ti, Nb and B entered M7C3-related carbides to form a multicomponent (Cr,Fe,V,Ti,Nb)7(C,B)3 concept. Substitution changes lattice chemistry and can alter stability, hardness, morphology and the matrix/carbon balance.
This formula is a structural interpretation, not a bulk composition. A certificate in weight percent cannot prove a specific crystallographic phase. XRD, SEM/EDS and metallography provide the supporting evidence.
| Evidence type | Bulk/phase question | Use | Boundary |
|---|---|---|---|
| OES/combustion | Bulk heat chemistry | Grade identity | No phase proof |
| XRD | Crystal phases/fractions | Martensite/austenite/carbide analysis | Sample representation |
| SEM | Morphology and distribution | Particle/carbide observation | Local field |
| EDS | Local elemental association | Cr/V/Ti/Nb/Zr clues | Semi-quantitative/local |
| Hardness | Local mechanical response | Matrix/bulk comparison | No chemistry proof |
Published phase fractions
After the reported heat treatment, base HCCI contained 70.7 wt.% martensite, 6.0 wt.% austenite and 23.3 wt.% hexagonal M7C3. HCCI-VFC contained 82.5 wt.% martensite, 0.9 wt.% austenite, 8.7 wt.% hexagonal M7C3 and 7.9 wt.% orthorhombic M7C3.
The total identified M7C3 fraction decreased while martensite increased. The result shows a redistributed phase balance rather than simply ‘more carbide equals more wear resistance.’
| Heat-treated phase | Base HCCI | HCCI-VFC | Interpretation |
|---|---|---|---|
| Martensite | 70.7 wt.% | 82.5 wt.% | Higher supporting hard matrix |
| Austenite | 6.0 wt.% | 0.9 wt.% | Lower retained fraction |
| Hexagonal M7C3 | 23.3 wt.% | 8.7 wt.% | Lower |
| Orthorhombic M7C3 | Not listed | 7.9 wt.% | Additional carbide structure |
| Total listed M7C3 | 23.3 wt.% | 16.6 wt.% | Lower but modified |
Hardness results by condition
The base and modified alloys were close in the as-cast state: 48.6 and 49.3 HRC. After quenching, values were 58.3 and 59.6 HRC. After tempering, values were 60.9 and 63.4 HRC. The alloying effect became more visible after the full thermal sequence.
This demonstrates chemistry-process interaction. Quoting only the final 63.4 HRC omits the condition, specimen and baseline required to interpret it.
| Condition | Base HCCI | HCCI-VFC | Reported increase |
|---|---|---|---|
| As cast | 48.6 HRC | 49.3 HRC | 1.4% |
| As quenched | 58.3 HRC | 59.6 HRC | 2.2% |
| Tempered | 60.9 HRC | 63.4 HRC | 4.1% |
Matrix hardness results
Vickers matrix hardness was reported as 430.7 versus 464.8 HV in the as-cast state, 690.3 versus 736.7 HV after quenching, and 713.4 versus 763.2 HV after tempering. The modified alloy therefore showed about seven-percent higher tempered matrix hardness.
Matrix hardness matters because the matrix supports carbides against undermining and pull-out. It still does not guarantee a full-size casting’s core response.
| Matrix condition | Base HCCI | HCCI-VFC | Reported increase |
|---|---|---|---|
| As cast | 430.7 HV | 464.8 HV | 7.9% |
| As quenched | 690.3 HV | 736.7 HV | 6.7% |
| Tempered | 713.4 HV | 763.2 HV | 7.0% |
Impact-toughness result
Heat-treated impact toughness increased from 7.1 to 8.3 J/cm2, reported as a 16.9% increase. Fracture-zone proportions also changed. This is notable because high-Cr iron selection often involves a hardness-versus-fracture tradeoff.
The result belongs to the paper’s specimen geometry, test method and condition. It must not be converted into a claim that every microalloyed mining liner is 16.9% tougher.
Wear and friction result
The paper reported a 2.3% decrease in friction coefficient and a 7.0% decrease in wear loss for HCCI-VFC under its test conditions. Those changes occurred together with a harder matrix and modified phase balance.
Field wear includes particle size, hardness, impact, trajectory, moisture and backing. A fair industrial conclusion requires paired liners in comparable positions and exposure normalized by processed tonnes or hours.
| Published outcome | Reported change | Valid statement | Invalid statement |
|---|---|---|---|
| Tempered hardness | +4.1% | Study specimen became harder | Every casting reaches 63.4 HRC |
| Impact toughness | +16.9% | Study specimen result improved | Field fracture risk falls 16.9% |
| Friction coefficient | -2.3% | Test friction decreased | Chute flow improves 2.3% |
| Wear loss | -7.0% | Test wear loss decreased | Service life rises 7% |
Casting scale changes the outcome
Laboratory ingots cool more uniformly than a large chute liner with ribs, bolt bosses and mixed thickness. Solidification rate changes M7C3 spacing, microalloy distribution, segregation and retained matrix chemistry. Heavy sections also respond differently during heat treatment.
Commercial development therefore needs section review, casting-process control and representative verification. A small coupon can support a qualification but cannot automatically stand for the most massive junction.
Induction melting and alloy recovery
Medium-frequency induction melting provides control of temperature and charge chemistry, but V, Ti, Nb, Zr and B have different oxidation and recovery behavior. Master-alloy form, addition timing, slag practice, holding and mixing influence the result.
A charge sheet predicts input; heat analysis measures output. Production acceptance must use the measured heat rather than nominal recovery assumptions.
| Melt step | Question | Risk | Evidence |
|---|---|---|---|
| Raw materials | Are residuals known? | Unplanned chemistry | Charge record |
| Master-alloy addition | Is sequence/recovery qualified? | Fade or segregation | Process record/analysis |
| Temperature/hold | Are oxidation and dissolution controlled? | Loss/coarse phases | Furnace record |
| Mixing/sample | Is melt representative? | Local chemistry | Qualified sample basis |
| Pouring | Is temperature/cleanliness maintained? | Inclusions/cold fill | Visual/NDT |
Sand casting and solidification
Resin-sand or sodium-silicate-sand molding may be chosen for custom liners. Pattern allowance, gating, feeding, risering and chills must account for high-Cr iron shrinkage and the desired thermal gradient. Abrupt section changes can create hot spots and coarse phases.
Casting method is part of alloy design. A perfect laboratory chemistry cannot rescue shrinkage, an unfed boss or an unsupported edge.
| Casting feature | Microstructural effect | Design response | Verification |
|---|---|---|---|
| Heavy boss | Slow cooling/segregation | Blend and feed | NDT + section response |
| Thin edge | Fast cooling/stress | Adequate ligament/radius | Visual/MT/dimension |
| Deep recess | Fill/core difficulty | Practical profile | Gauge/profile |
| Large bearing face | Distortion/rocking | Support/finish plan | Flatness/contact |
| Mixed thickness | Uneven phases/hardness | Map critical zones | Hardness/metallography |
Reading the published heat treatment
The paper vacuum-heated alloys at 960 C for three hours, cooled them to room temperature, tempered at 450 C for two hours and furnace-cooled. These parameters explain the reported specimen results and make the experiment reproducible.
They are not a universal shop recipe. Production castings require a route qualified for actual mass, section, furnace load, alloy recovery and property requirements.
Why tempering increased reported hardness
In this study, tempered hardness exceeded the as-quenched value. Secondary-carbide precipitation, retained-austenite transformation and matrix changes can produce secondary hardening in high-alloy systems. The trend should be understood within the specific alloy and cycle.
Do not assume that any higher temper temperature will keep increasing hardness. The supplier process and final verification govern.
| Thermal stage | Main mechanism | Variable | Commercial check |
|---|---|---|---|
| Heating | Matrix/carbide conditioning | Temperature/time/section | Qualified cycle |
| Cooling | Martensite/austenite balance | Rate and delay | Hardness/phase |
| Tempering | Stress/secondary hardening | Temperature/time | Final properties |
| Furnace cooling | Stability/thermal gradient | Load and rate | Dimensional/property check |

Where the alloy concept may fit
A multi-alloy HCCI may be evaluated in supported sliding zones, fine-to-medium ore sidewalls, crusher or feeder discharge liners, hopper tiles and shaped wear plates where abrasion dominates and impact is controlled. Cast geometry can add curves, ribs and recessed fixing.
Direct large-lump impact, unsupported spans or field-welded flat panels may favor high-manganese steel, heat-treated cast steel or rolled NM plate. Application zoning is more credible than one material across every chute surface.
| Duty | Multi-alloy HCCI fit | Alternative |
|---|---|---|
| Supported sliding abrasion | Strongest candidate | Cr-Mo/Nb-Mo HCCI |
| Fine/medium ore sidewall | Candidate for controlled trial | Ni-Hard/NM plate |
| Direct severe impact | High caution | High-Mn or alloy steel |
| Fabricated flat panel | Casting may be unnecessary | NM plate |
| Loose support/edge strike | Correct interface first | No chemistry substitutes for support |

Chemistry testing and PMI limits
Commercial heat analysis should report C, Si, Mn, Cr, V, Ti, Nb, Zr, B, Mo, Ni, P and S as required. Carbon and low boron need appropriate laboratory methods. Portable XRF can screen many heavier elements but cannot directly measure carbon and may not quantify B reliably.
Detection limits, calibration, surface preparation and sampling must match the acceptance range. Handheld PMI is supporting evidence, not a complete certificate.
| Element group | Preferred evidence | Why |
|---|---|---|
| C/S | Combustion or qualified OES | Light-element accuracy |
| Cr/V/Ti/Nb/Zr/Mo/Ni | Qualified OES/ICP and heat identity | Multielement result |
| B | Method with suitable low-level detection | 0.01-0.03% range sensitivity |
| P and residuals | Contract-defined heat analysis | Cleanliness/identity |
| PMI | Calibrated screening | Useful but incomplete |
Hardness, phase and NDT evidence
Specify bulk hardness scale, points and range. If matrix hardness or phase fraction is required, define sample location and method. XRD, metallography and SEM/EDS can support first-article qualification but should not be demanded generically without acceptance criteria.
NDT likewise needs method, extent, zones, surface condition and acceptance. Complex hard cast iron is not fully described by a line reading 100% UT.
Fixing and backing remain decisive
A hard multi-alloy casting must bear correctly against the shell. Rocking creates bending; exposed flow-facing joints concentrate impact; thin ligaments around recesses become crack starters. Chemistry cannot compensate for these interface errors.
Define backing contact, bolts, recess geometry, joint direction, gap, lifting and replacement method in the drawing and installation plan.
| Interface | Control | Failure avoided |
|---|---|---|
| Backing | Contact/finish/shim plan | Rocking and bending |
| Bolts | Property, seat and tightening | Loosening/local cracks |
| Joint | Flow direction, gap and step | Edge impact/packing |
| Lifting | Mass and approved feature | Unsafe handling |
| Welding | Prohibition or qualified method | Thermal cracking |

Field trial design
Before installation, record part ID, heat, baseline thickness, hardness points, mass where practical, backing and photographs. Track tonnes or hours, particle size, throughput, moisture, abnormal impact, bolt condition and repeated thickness on a numbered grid.
Compare the multi-alloy liner with a conventional HCCI control in equivalent positions where possible. At removal, classify abrasion, carbide spalling, cracks, deformation and installation failure, then calculate cost per processed tonne.
| Trial metric | Record | Use |
|---|---|---|
| Position | Matched duty zones | Controls trajectory |
| Exposure | Tonnes/hours | Normalizes wear |
| Abrasive | Size/hardness/moisture | Defines severity |
| Installation | Backing/joints/bolts | Separates interface failure |
| Outcome | Wear map/cracks/downtime | Tests economic value |
Common interpretation errors
Do not treat the reconstructed nominal chemistry as a measured heat, call VFC a universal master-alloy grade, or claim that every casting reaches 63.4 HRC, 8.3 J/cm2 or seven-percent lower wear. Do not infer phase fractions from bulk chemistry.
Avoid maximizing the number of elements, copying laboratory heat treatment into a large casting, ignoring section effects, using XRF as full proof, or selecting the material without an equivalent-position field trial.
RFQ information derived from the chemistry
A useful RFQ identifies full chemistry limits, standard or modification, delivery condition, hardness and phase requirements, test locations, residuals and analysis methods. It also provides drawing, section map, quantity, fixing, bearing faces and critical tolerances.
Duty data include particle size/hardness, impact, sliding speed, throughput, moisture, temperature, current material, wear map and failure mode. Without both metallurgy and duty, a complex chemistry cannot be evaluated responsibly.
| RFQ block | Input | Decision |
|---|---|---|
| Composition | C-Cr-V-Ti-Nb-Zr-B plus residuals | Melt feasibility |
| Geometry | Drawing, mass and sections | Casting/thermal response |
| Duty | Abrasion, impact and particles | Material fit |
| Condition | Heat treatment/properties | Final matrix/carbides |
| QA | Chemistry, hardness, phases, NDT | Release plan |
| Trial | Baseline and monitoring | Field-value proof |
Decision summary
C-Cr-V-Ti-Nb-Zr-B HCCI is a coordinated alloy-process system. C and Cr create the base carbide architecture; V is the major added alloy; Ti, Nb, Zr and B modify nucleation, carbide chemistry and matrix response. Heat treatment converts those changes into a different phase and hardness balance.
Use the published data to ask better questions, not to promise identical field numbers. Specify the actual casting, verify the production lot and compare it under controlled service conditions.
From VFC chemistry research to a controlled wear-plate RFQ
Review the paired C-Cr-V-Ti-Nb-Zr-B multi-alloy wear-plate product, compare the C-Cr-Nb-Mo product, or read how to choose mining wear plates. Send the drawing and wear history or email wear@ebcastings.com.
Primary source and engineering boundary
The chemistry, phase, hardness, toughness and wear results are from ‘Effect of Multi-Element Microalloying on the Structure and Properties of High Chromium Cast Iron,’ Materials 2023, 16, 3292, DOI 10.3390/ma16093292. The PubMed record provides an independent index of the article.
Final chemistry, casting, thermal process, geometry, support, fixing and installation require customer and qualified-engineer approval. Research specimens and website tables do not guarantee service life. Site isolation, stored-energy control and safe lifting procedures apply.

