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Testing Insights

No pretty spec-sheet numbers — only the pitfalls you actually hit in the lab: how to pick capacity, how to prep samples, how to turn microstructure into usable data.

Tensile Testing2026 / 09 / 28~5 min

How to choose tensile tester capacity? 10kN or 100kN

Algorithm first: max test force ≈ material tensile strength × original cross-sectional area, plus 20%–30% margin. But the real buying mistake isn't "too big" — it's only looking at the upper limit, not the lower. Pull a 5kN thin sheet on a 100kN machine and the data is still untrustworthy.

Step 1: Calculate the maximum force you actually need

Fmax ≈ Rm (tensile strength, MPa) × S0 (original cross-section, mm²) ÷ 1000 → kN

Take Rm as the highest among all your materials, and S0 as your largest common sample cross-section. Multiply and add margin — that's the capacity tier to choose.

Material / SampleRm refArea S0Est. max forceRecommended
Q235 round Φ10400 MPa78.5 mm²31 kN50 kN
45 steel (QT) round Φ10600–750 MPa78.5 mm²47–59 kN100 kN
6061 Al plate 2 × 12.5 mm300 MPa25 mm²7.5 kN10 kN
304 SS plate 2 × 12.5 mm515 MPa25 mm²13 kN30 kN
10.9 bolt M201040 MPa245 mm²255 kN300–600 kN
HRB400 rebar Φ25540 MPa490.9 mm²265 kN600 kN
Cu foil / wire Φ0.5 mm250–400 MPa0.196 mm²50–80 N500 N – 1 kN cell

Values above are for selection estimation; actual per material cert and GB/T 228.1 sample dimensions.

Step 2: Make sure small samples also fall in range

Force error is assessed over the measuring range (GB/T 16825.1 / ISO 7500-1). The controlled interval of typical machines is usually 20%–100% of full scale; below that, indication error is no longer covered by the calibration certificate.

In one line: the fracture force of your smallest common sample should not be below 20% of the chosen capacity.

  • 100 kN machine on 7.5 kN Al plate → only 7.5%, out of range, error may exceed ±1%;
  • same machine on 47 kN 45 steel → 47%, normal;
  • conclusion: this machine can pull steel but not thin Al plate — not "a big machine does everything".
Practical fix: labs with a wide sample span should choose a frame with interchangeable load cells (e.g. 100 kN frame with 100 / 10 / 1 kN cells) — each sample uses its own cell, one machine covers all scenarios, cheaper than buying two.

Step 3: Don't miss these four items

  • Test type: tension only? or compression, bending, shear, peel? Bending needs 3/4-point bending fixtures and larger test space.
  • Yield & modulus?: to measure Rp0.2, ReL or E, you must have an extensometer (sized by gauge length). Without it, yield is only back-calculated from crosshead displacement — not accepted.
  • Speed control: GB/T 228.1 / ISO 6892-1 recommends strain-rate control (Method A), requiring closed-loop strain control — ask before buying.
  • Frame rigidity & space: large-tonnage machines deform the frame during small-force tests, mixing into displacement; also confirm the largest sample (with fixture) fits the test space.

Selection checklist (send us and we'll design)

  • material list with each highest tensile strength;
  • sample form: round / plate / wire / foil / finished part, and size range;
  • which metrics: Rm, Rp0.2, A, Z, E, n;
  • standard: GB/T 228.1, ISO 6892-1, ASTM E8 or in-house;
  • need thermal chamber, extensometer, special fixtures;
  • need LIMS / fixed-format report export.
Send us your material list and sample sizes — we'll specify capacity, fixtures and load cells within 48 hours. Send Drawings →
OES2026 / 09 / 10~6 min

OES grade ID — the most error-prone sample-prep steps

Experience: of questionable OES results, 70% come from sample prep, not the instrument. The spectrometer only reads the point you give it — whether that point is clean, flat and the base metal itself, the instrument can't judge.

Mistake 1: Exciting with scale / coating / plating still on

Spark only burns tens of microns deep. If the surface is oxide scale, paint, zinc plating or carburized layer, you're not measuring base composition. Fix: grind or mill off 0.5–1 mm+ to expose fresh base metal; coated plates must have coating fully removed first.

Mistake 2: Mixing grinding wheels / paper → cross-contamination

Paper used on steel then on aluminum carries Fe in, inflating Al's Fe content. Fix: color-code abrasives by base metal — Fe, Al, Cu, Ti each get their own paper/wheel; a dedicated grinder is better; idle-grind a few seconds when switching.

Mistake 3: Wrong surface roughness

  • Too rough (visible scratches): poor seal, argon leak → diffuse discharge, scattered data, light elements C/S/P especially unstable;
  • Too smooth (mirror): soft metals like Al get abrasive pressed in during polish, also contaminating;
  • recommended: uniform fine striations (Ra ~0.8–1.6 μm); dedicated grinder or 40–80 grit alumina wheel/belt in one pass is stablest.

Mistake 4: Sample too thin / too small

Thin samples dissipate heat poorly → local overheating or even burn-through; backside scale also discharges. Generally: flat excitation face, area fully covering the excitation hole (common Ø12–16 mm), thickness ≥ 3 mm; thin plate, wire, small parts use dedicated small-sample fixtures or mounting, noted in method.

Mistake 5: Random excitation-point position

  • ≥ 3–5 mm from sample edge, else argon seal fails;
  • avoid porosity, sand holes, inclusions, cracks, welds and obvious segregation;
  • space between points; no re-striking on old spots;
  • tubes, round bars (curved) must be machined flat before measuring — curved face can't seal;
  • take 2–3 points per sample, drop outliers, average.

Mistake 6: Fingers, oil and moisture

Fingerprints bring C, H, O contamination; moisture makes discharge unstable. No touching the excitation face; if needed clean with anhydrous ethanol or acetone and fully blow dry before measuring.

Mistake 7: Argon & standardization ignored

  • argon purity ≥ 99.999%; insufficient → white spot, drifting data;
  • after startup, bottle change, big temp/humidity change, before continuous runs → do standardization;
  • for wide base/grade spans, use type standardization (control samples) — far more accurate than global-only.

How to read the spark spot: a diagnosis table

Spot shapePossible causeAction
Centered dark-grey round spot, sharp edgeNormal condensed dischargeAccept directly
Bright white spot, spreading outwardLow argon / leak / rough or warped surfaceCheck gas path & seal, re-prep
Shallow small spot, low-energy feelLow argon pressure, loose contactAdjust pressure, check fixture
Black spot with holes or radial cracksInternal porosity, inclusionsRe-measure elsewhere, record defect
Large point-to-point variationSegregation / inconsistent prepMore points, unify prep method
Two special base metals:
① Cast iron must be chilled (white/mottled) before spark-OES for C, Si, else carbon exists as graphite and results are severely distorted;
② Aluminum is better turned than ground — grinding presses abrasive into the soft base and masks true composition (Si, Mg especially).

Common method standards: steel per GB/T 4336, stainless per GB/T 11170, Al & alloys per GB/T 7999; report per the current valid edition.

Unsure how to prep your sample? Send a photo — engineers give a prep plan directly. Ask Prep Method →
Metallography2026 / 08 / 22~7 min

Metallography five-step method: cut, mount, polish, etch, observe

Prep quality decides the reading. One line for the whole flow: cold cutting, edge-protected mounting, clean polishing, light etching, right observation mode. 80% of bad metallography photos come from step 3 — polishing.

StepPurposeKey controlTypical error
1 CutTake representative sectionAdequate coolant, wheel matched to hardnessHeat burn, cutting in HAZ
2 MountEasy handling, edge protectionHot vs cold mount; edge-protection needEdge rounding on coating/case
3 PolishDamage-free, deformation-free mirrorStep down grit, rotate 90° each step, clean betweenSkipped grit, comet tail, scratch, relief
4 EtchReveal structureReagent matched to material, time shallow→deepOver-etch, slow rinse/dry
5 ObserveQualify + rateBright/dark/polarized/DIC each have useWrong mode, insufficient mag

1. Cutting: representative position, low temperature

  • define purpose first: banding → longitudinal; grain/decarburization → transverse; failure must include crack source;
  • wheel rule: hard material → soft wheel, soft material → hard wheel, avoid clogging & overheating;
  • adequate cooling mandatory — overheating changes local structure (re-quench, temper), making the reading completely wrong;
  • after cutting, remove another 1–2 mm inward to leave the cutting HAZ outside.

2. Mounting: when to use cold mount

  • Hot mount (phenolic / epoxy, ~150–180°C, pressure, minutes): fast, hard, for high-volume regular samples;
  • Cold mount (epoxy / acrylic, room-temp cure): for heat-sensitive, coated, porous, tiny or irregular parts;
  • measuring case depth, coating thickness, decarburization → must use edge-protecting filler (glass-fiber/ceramic) or dedicated edge-clamp, else edge rounds and depth reads low.

3. Polishing: four-stage progression, clean between

StageAbrasiveGoal
Coarse#180 → #320 → #600 SiC paperRemove cutting damage, flatten
Fine#800 → #1200 → #2000Eliminate coarse scratches
Rough polishDiamond 9 μm → 3 μm → 1 μmMirror finish
Final polish0.05 μm alumina / silicaRemove deformed layer (high-mag, EBSD)
  • each step rotate 90°, polish until previous scratches gone;
  • ultrasonic clean between steps — one leftover coarse grit is the primary source of a through-scratch;
  • polish pressure & time: smaller is safer — high pressure → deep deformation layer, relief;
  • cast iron, Al (soft) prone to comet tail; final light polish, shorter time helps.

4. Etching: match reagent, converge time

  • Carbon / low-alloy steel: 2%–4% Nital, seconds to ~15 s;
  • Stainless: aqua regia, ferric chloride-HCl, or 10% oxalic electrolytic;
  • Aluminum: Keller (HF + HCl + HNO₃), 10–30 s;
  • Titanium: Kroll;
  • rule: shallow over deep — shallow can be added, deep means back to polish; after etch immediately water → alcohol → blow dry, one delay and you get an oxide tint.

5. Observe: four modes each cover a range

  • Bright field: default for general structure, grain size, phase composition;
  • Dark field: grain boundaries, fine inclusions, micro-relief on polished face — higher sensitivity;
  • Polarized: graphite spheroids, non-metallic inclusions, coatings, anisotropic structures;
  • DIC: relief without etching — for coating, case, post-surface-treatment cross-sections.

Common rating standards: grain size GB/T 6394 (≈ ASTM E112, comparison/interception), non-metallic inclusions GB/T 10561 (≈ ASTM E45), carburized hardened layer GB/T 9450, induction/flame hardened layer GB/T 5617, decarburization GB/T 224, microstructure general rules GB/T 13298.

Seven common defects: symptom → cause → fix

SymptomMain causeFix
Through-scratchNo clean between / skipped grit / abrasive in clothStep back one grit, ultrasonic clean, change cloth
Comet tail (dark tail behind graphite/inclusion)Over-polish, single directionShorten time, add lube, final light polish
Relief / step (phase-height difference)Over-polish, soft phase removedReduce time, use short-nap cloth
Pits / black holesInclusion/graphite dropout, material porosityShorten polish, judge if material defect first
Edge roundingNo edge protection, high pressureCold mount + edge filler, lower pressure
Oxide tint / yellowingSlow rinse/dry after etchImmediately water → alcohol → cold air dry
False structure (e.g. deformed martensite in austenitic steel)Cutting/grinding damage layer not removedIncrease coarse removal, or electrolytic polish
Remember this: spending 3 extra minutes cleaning between polish steps saves 30 minutes of re-prep later. Metallography cost is almost all in rework.
Need a prep line (cutter, mounter, polisher)? Tell us material and inspection items. Configure Prep Line →
ONH Analysis2026 / 10 / 30~6 min

What does an ONH analyzer measure? The quality issues behind O, N and H

Your mill cert lists C, Si and Mn — but O, N and H are often missing. Yet flake cracking (shatter cracks), strain-aging embrittlement and early fatigue failure are usually caused by exactly these three "invisible elements". They sit at ppm level, beyond conventional OES — only an oxygen-nitrogen-hydrogen (ONH) analyzer can measure them.

First, know what each element wrecks

  • H (hydrogen): the culprit behind flakes (shatter cracks). Large forgings, spring steel, line-pipe steel and gear steel are most hydrogen-sensitive — hydrogen-charged steel cracks late, under combined stress and microstructural transformation, often days or even weeks after quenching;
  • N (nitrogen): the driver of strain aging. When low-carbon sheet is stamped, Lüders bands (slip lines) appear on the surface and scrap rates climb. In stainless steel nitrogen is actually good (solid-solution strengthening), but poor control during welding causes porosity;
  • O (oxygen): present as oxide inclusions, directly cutting fatigue life and cleanliness ratings. Oxygen content in bearing and spring steels is a must-check item for high-end customers.

The principle, in one paragraph

The sample goes into a graphite crucible and is pulse-heated above 2500 °C in inert gas until it melts: oxygen reacts with crucible carbon to form CO/CO2, quantified by an infrared detector; nitrogen and hydrogen are released as N2 and H2, separated and measured by a thermal-conductivity detector. One machine, one fusion, three elements — all within a few minutes.

Ranges & precision: how to read the table

Using the model we deliver (Nake ONH 3500) as an example:

ElementMeasuring range (dual)PrecisionQuality concern
O oxygen0.1ppm – 0.5% / 0.5% – 20%1ppm or RSD ≤ 1.0%Bearing-steel cleanliness, weld oxygen
N nitrogen0.1ppm – 0.5% / 0.5% – 50%1ppm or RSD ≤ 1.0%Aging control, nitrided case, N in stainless
H hydrogen0.1ppm – 200ppm / 200ppm – 5000ppm0.2ppm or RSD ≤ 2.0%Flake prevention, diffusible H in weld metal

Analysis time is within about 3 minutes, fully automatic. Actual values are governed by the instrument calibration certificate and current standards.

Why dual ranges: the low range preserves ppm-level resolution (bearing steel requires O ≤ ~10 ppm), while the high range keeps high-content samples (powder metallurgy, hydrided titanium) from exceeding the detection limit. When selecting, match both ranges against your material content window.

Sampling & prep: at ppm level, contamination is error

  • Surface condition: remove scale, oil and moisture. O and H are extremely surface-sensitive — sweat injects hydrogen directly. Gloves and tweezers from sampling to testing, no exceptions;
  • Sample form: typically a block (~0.5–1 g) with clean, pore-free surface; chips and powders need dedicated crucibles and methods;
  • Test hydrogen promptly: hydrogen diffuses out. Weld seams, deposited metal and pickled parts should be tested as soon as possible or stored cold — wait two weeks and half the hydrogen may be gone;
  • Flux & blank: tungsten-tin flux and crucibles carry background blanks; blank drift eats ppm-level resolution — run blank and CRM calibration first thing every day;
  • Control samples: type-calibrate with reference materials of similar composition — far better than instrument-only calibration at suppressing matrix effects.

Which industries really need an ONH

  • Producers of bearing, spring and gear steel (full O/N/H control + customer audits);
  • Welding consumables and welding procedure qualification (diffusible hydrogen in deposited metal is a mandatory test);
  • Titanium alloys, powder metallurgy, cemented carbides (H and O define product grade);
  • Third-party labs taking outsourced testing from steel mills.
Not sure whether your materials need O/N/H control? Send us the grade and customer requirement — our engineers will assess. Ask About ONH →
Hardness Testing2026 / 10 / 16~5 min

HRC, HRB or HV? Choosing a hardness scale and the limits of conversion

Hardness is not one physical quantity — it is a family of test methods for resistance to indentation. On the same material, HRC 45 and HV 450 can both be "correct" at once. The two real mistakes are using a scale outside its valid range, and taking a conversion table as a measurement.

How the three families divide the work

FamilyPrincipleStrengthTypical useStandard
Rockwell HRC / HRB / HRAReads depth difference directly, no indentation measurementFast, non-destructive to appearance, ideal for batch sampling of finished partsQuenched parts HRC, annealed stock HRB, carbides HRAGB/T 230.1 / ISO 6508
Brinell HBWLarge carbide ball, measure indentation diameterLarge indentation, highly representative, insensitive to structureCast iron, annealed/normalized steel, Al & Cu partsGB/T 231.1 / ISO 6506
Vickers HVDiamond pyramid, measure diagonals, full force coverageOne scale from HV0.01 to HV30+, measures thin layersCase/decarburization gradients, thin sheet, weld zones, referee testingGB/T 4340.1 / ISO 6507

Valid ranges at a glance

  • HRC valid 20–70: below 20 switch to HRB or HBW; above 70, to HRA or HV;
  • HRB valid 20–100: for medium-low hardness materials such as annealed steel, copper and aluminum alloys;
  • Minimum specimen thickness: about 10× the indentation depth — visible deformation on the back voids the data. Thin sheet and cases (typically 0.1–1.5 mm) are punctured by a single HRC indent; use superficial Rockwell (HRN/HRT) or low-force Vickers instead;
  • Cylindrical & spherical surfaces: curvature affects readings. HRC on a convex cylinder needs the standard curvature correction; spheres should not be tested directly — align round bars with a V-anvil.

Conversion tables: reference only, never a result

Hardness conversion tables for ferrous metals (GB/T 1172, ASTM E140) are statistical correlations, reliable only within the specified material class and hardness interval. Three practical boundaries:

  • The drawing calls HV for referee testing but you measured HRC and converted — it does not count in arbitration; the specified scale must be measured directly;
  • Cross-family conversion error can reach ±30 HV; near acceptance limits (e.g. ≥ HV 600) never conclude from a converted value;
  • Special materials like cast iron and austenitic stainless steel need their own tables — applying the general steel table doubles the error.
Remember one line: conversion tables are for quick internal judgment and communication; formal reports use the measured value on the scale specified by contract or drawing.

The five easiest field mistakes

  • Indentation spacing too small: centers closer than 3–4× indentation diameter, or nearer than 2.5–3× to an edge — stress fields overlap and readings distort;
  • Anvil and indenter not concentric: dirty anvil or a rocking specimen makes Rockwell readings jump — run an intermediate check on a reference block before each batch;
  • Punching through the case: a carburized part with 0.8 mm case vs an HRC indentation 0.1–0.2 mm deep — add the soft core's influence and readings read low. For effective case depth, use a Vickers gradient (GB/T 9450);
  • Temperature & vibration: standards require 10–35 °C (precision grade 23 ± 5 °C); a station facing a punch press gives unstable readings — the machine is not broken;
  • No verification on direct-reading testers: after every scale change, anvil change, or before/after large batch runs, test a reference block — the single most common audit nonconformity here.

Selection decision: four steps to a scale

  • ① Thickness & case: solid stock works down the list; thin sheet/layers go straight to Vickers or superficial Rockwell;
  • ② Hardness interval: match against the ranges above — which scale's valid window does it fall into;
  • ③ Surface condition: rough cast/forged surfaces suit Brinell; machined faces and finished parts suit Rockwell;
  • ④ Customer & standard: whatever the drawing, company spec or audit requires — measure that; conversion is for internal reference only.
Unsure which hardness tester to configure? Send us material, thickness and acceptance clauses. Ask Hardness Selection →

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