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© Peter Kruse DEFECTS DEFECTS ON & IN SLABS ON & IN SLABS SS AB Oh my GOD! Ugly Cracks!!

DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

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Page 1: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

DEFECTSDEFECTSON & IN SLABSON & IN SLABS

SSAB

Oh my GOD!Ugly Cracks!!

Page 2: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

ContentContentClassification of defects

TypeSize

Factors influating the cracking susceptibility.

Material propertiesExternal factors

Short solidification theoryCalculation of shellthicknessCrack types & causesActions to avoid cracking

Page 3: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

ClassificationClassificationDefect types

Shape defects kod 30-39Surface defects kod 40-49Other actions kod 50-59Internal defects kod 60-69

SizeMinor, relatively harmless defects(0-3mm)Semi deep defects(4-11mm; treatment nessesary)Deep defects(12-20mm; Heavy treatment)Very deep defects(> 20mm: could be scrap)

Page 4: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

FactorsFactors influatinginfluatingthe cracking the cracking

susceptibilitysusceptibility..Material properties

Steel analysisTemperature properties

External factors causingtension in the strand

MecanicalThermal

Page 5: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

InfluenceInfluence of of analysesanalyses

Low carbon, low alloy steelhas low susceptibility for cracking.

Steel with carbon ~0,08-0,14% is very susceptible to surfacecracks

High carbon, high alloy steelhas high susceptibility to internal defects

S, P, V, Nb normally increasesthe crack susceptibility.

Page 6: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

PropertiesProperties at at different different

temperaturestemperaturesThe ductility variates during the solidification and cooling period.

Ts

600 900 1200 1500

Duc

tility

IIII II

γ γγ

(Fe,Mn)S-OCu,Sn,SbAlN,BN,Nb(C,N)

γ liquid

Page 7: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

SolidificationSolidification theorytheory

Internal defectsis created whenthe two-phaseregion is exposed to tensions exceeding the strength of the material.

TS

TY

TY

Q

QTL

TY

TL

QTL

dT

dT

dT

dx

dx

dx

dq=-k*dTdt dx

Q=

solid

liquid

Soldification interval

Page 8: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Shell growth:1Shell growth:1

It is possible to calculate the approximate shell thicknesswith the following formula:

s=Cs* l/Vc

s=shell thickness [mm]Cs=solidification constant (~25-27)l =distance from meniscus [m]Vc=casting speed [m/min]

This relatively simple formulagives you a rough idea of the shell thickness. You must try to find out the Cs for different conditions.

Page 9: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

If you want to know where in the machine a defect is created you can rearrange the formula as below :

l=Vc*(s/Cs)2

The length is not exact, but it will give you a hint where to search for problems in your caster

Shell Shell growthgrowth :2:2

Page 10: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

ExternalExternal faktorsfaktors

MECHANICALTaper errorsBad mould lubricationBadly aligned rolls/segmentsSkidding rollsStrand unbending

THERMALUneven coolingFast reheatingTo soft coolingTo hard cooling

Page 11: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

InternalInternaldefectsdefects

1. Longitudinal narrow face cracks

2. Longitudinal cracks3. Corner cracks4. Transversal cracks5. Diagonal cracks

1

25

3

4

Page 12: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Longitudinal Longitudinal narrownarrow face face crackscracks

Causes:Bulging of broad sidePressing of narrow faceOvercooling and reheating of the narrow face

Page 13: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Longitudinal Longitudinal crackscracks

Causes :Bulging of broad sides down in the machine

Bearing- or roll damage, misaligned rolls and/or segments.Insufficient cooling

Can extend to slab surfaceand cause a breakout

Page 14: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Corner Corner crackscracks

Causes :Narrow face bulging

Insufficient taperInsufficient cooling

Reheating

Can extend to slab surface and cause a breakout

Page 15: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Corner Corner crackscracks

Page 16: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Transversal Transversal crackscracks

Causes:BulgingDeprsession of shell

Roll alignmentUnbending of the strandTo high pressure from driven rolls

Page 17: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Transversal Transversal crackscracks

Page 18: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Diagonal Diagonal crackscracks

”Triple-point cracks”Causes:

Sensitive analysesC-content >0,15 %Low Mn/S ratio

Bulging

Page 19: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

SurfaceSurface crackscracks

1. Transversal cracks2. Transversal corner cracks3. Longitudional cracks4. Short Longitudional cracks5. Longitudional corner cracks6. Star/net cracks

3

4

5

6

1

2

5

Page 20: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Transversal Transversal crackscracks

Causes:Large temperature gradients in the cooling zone.Straightening at low-ductiletemp.Misaligned/damaged/skidding rolls can be the cause.

The cracks are normallysituated in oscillation marks

Page 21: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Transversal corner Transversal corner crackscracks

Causes:Large temperature gradients in the cooling zone.Straightening at low-ductiletemp.

The cracks are normallysituated in oscillation marks

Page 22: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

LongitudionalLongitudional crackscracks

Long, deep ”mid face cracks”Causes:

Uneven shell growth due to bad mould powder function.Tensions generated in the mould ie. bad lubrication, scratches, insufficient taper.

Page 23: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

ShortShort LongitudionalLongitudionalcrackscracks

Causes:High casting temperature => thin shell.Uneven shell growth.

Page 24: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Longitudinal corner Longitudinal corner crackscracks

Causes:Uneven corner cooling.Bulging below the mould.due to insufficient narrow face

cooling and/or taperThis type of crack cansome time cause severebreakouts.

Page 25: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

Star/Star/netnet crackscracks

Cause:Cupper pick-up from the moulddue to bad powder functioncauses ”hot shortness”.This is cupper entrained in the grain boudaries that cause lowductility =>cracks.

Page 26: DEFECTS - Luleå University of Technology/cracks_eng.pdf · ©Peter Kruse Shell growth:1 ¾It is possible to calculate the approximate shell thickness with the following formula:

© Peter Kruse

CountermeasuresCountermeasures

Avoid tension in problem areas.

Temperature & analysisGood steelmaking practice=> less casting problems =>better quality.Continous supervision of the mould area.Always keep the casters in top condition.

Mould conditionsSegment/roll alignmentSecondary cooling