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8/2/2019 Thesis Amajit
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Development of Computer Aided Heat Treatment
Planning System for Quenching & Tempering(CHT-q/t)
and Industrial Application
of CHT-bfand CHT-cfM.S Thesis Defense presentation
By
Amarjit Kumar Singh
Advisor: Prof. Yiming (Kevin) Rong
Prof. Diran Apelian Thesis Committee
Prof. R .D. Sisson. Jr, Thesis Committee
Prof. M. A. Demetriou, Graduate Committee
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Outline
Introduction to Heat treatment process
Industrial need of a simulation software
System design of CHT- q/t Database design
Enmeshment of Box shape workpiece
Mechanical properties prediction after quenching
Case study with CHT- q/t Industrial application of CHT- bfand CHT- cf
Summary
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Introduction to heat treatment
Heat Treatment may be defined as heating and cooling operations applied tometals and alloys in solid state so as to obtain the desired properties.
The main types of heat treatment applied in practice are
Annealing
Normalization
Hardening and
Tempering
Some of the objectives of heat treatment are summarized as follows:
Improvement in ductility
Relieving internal stresses
Refinement of grain size Increasing hardness or tensile strength
Improvement in machinability
Improvement in toughness
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Industrial need of a heat treating software
Furnaces are widely used for the heat treatment of mass production parts.So to optimize the heat treating process is of great significance.
The present simulation softwares, unable to integrate the part load and
furnace model with the heat treating process.
Foundation of CHT- q/t
CHT-bfand CHT-cfas the foundation of CHT- q/tfor several database andheating module
QuenchPAD for the quenchant database.
Challenges for development of CHT- q/t
CHT-q/tneeds a complete database, most function modules are databaseoriented.
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Definition of CHT- q/t
CHT-q/tis a software tool to predict the temperature profile of load in
batch as well as continuous furnace during heating, quenching and
tempering of steel, then to predict the mechanical properties as Quenched
& Tempered and finally to optimize the heat treatment process design.
Part information
Quenchantinformation
Temperature vs timeof all parts
Properties in load
Fuel flow rate-time
profile
Heat-time profileof each part
Heat transfercalculation
Load pattern
Input
Output
Furnace information
Dynamic cooling result
Phase
transformation
Property prediction
Database
Workpiece Material
Furnace
AtmosphereFuel
Workpiece geo.
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Function flow chart
Describes the functionmodules, database and
output of CHT- q/t
Module 2Heating
Module 5Tempering
Heating below austenizing temperature
Output 3Mechanical Properties
after Quenching
Output 5
Mechanical Propertiesafter Tempering
DB1Material & TTT profile DB
Output 1Heat term &
temperatures
Module 4Phase transformation prediction
(Austenite to pearlite / bainite / martensite)Comparing cooling curve with TTT diagram to
determine microstructure
Mapping of microstructure to properties
DB4Quenchant DB
Module 1Workpiece classification & enmeshment
Workpiece shape classificationEnmeshment by Biot no.
Output 2Cooling curve of eachworkpiece and inside
the workpiece
Output 4Heat term &temperatures
Module 6Property prediction by empirical equations
DB2Furnace DB
Heat transfer for gas quenching in same furnaceused in heating
Heat transfer for oil quenching in tank(load with fixture, single workpiece without fixture)
Heat transfer for gas quenching in differentfurnace
Initial condition
Cooling
Workpiece Furnace Load pattern Thermal schedule
Module 3
DB3
Atmosphere DB
DB6
Tempering propertiesDB
DB5Quenching properties
DB
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Database design
CHT-q/tneeds extensive database to increase its applicability, as most of themodules strongly depend on database.
The TTT and quenchant database are the new addition.
Material and properties It comprises of workpiece as well as furnace materials.
Considers non-linearity of properties
Addition of TTT diagrams for steels
Workpiece shape 13 basic shapes
Furnace Batch & Continuous furnace for heating
Dual chamber furnace, vacuum furnace, quenchant tank for cooling
Atmosphere Fuels
Quenchants Frequently used gas as well as liquid quenchants
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TTT database development
In CHT-q/tsteels are classified as
Carbon steel
Alloy steel
Tool steel
Stainless steel
Steps for the conversion of the TTT diagrams in
tabular format Convert in digital format
Pick the start and finish curves at temperature duration of 20 deg
The value range from Austenitic start to martensitic start
Store Ms and Mfvalues as well
Source: TTT diagrams taken from Atlas of Time-Temperature Diagrams forIrons and Steels
http://nick-gd.chat.ru/index2.htm
0
200
400
600
800
1000
1200
1400
1600
1 10 100 1000 10000 100000
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TTT Database as shown in CHT- q/t
TTT Database as shown in CHT- q/t
User has the option to add or edit the TTT database as well
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Quenchant database development for gas quenchant
Relationship between gas pressure and the heat
transfer coefficient at 500 degree C and 15m/s
Reference:Torsten holm, Soren
segerberg, Gasquenching
branches out,
advanced materials
and processes, 1996.
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Quenchant database development for liquid quenchant
H
eattransfercoefficient,W/m2K
0
1000
2000
3000
4000
5000
6000
0 200 400 600 800
Convection stage
Boiling
sage
Vapor
blanket
stage
TA-B TB-C
Temperature,
Boiling
stage
TA-BTB-C
The quenchant database considers the variation of convective heat transfer coefficient in
all the three stages i.e. film boiling, bubble boiling and convection stages during liquid
quenching
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Classification of workpiece
3-step
shaft
2-step
shaft
coneBase
Hollow
cone
Hollow
cylinder
2-stacked
brick
TorusSphereConeCylinderBox
Shapes
Class VClass IVClass IIIClass IIClass IClass
Class I
The enmeshment was one dimensional for CHT- bfand CHT- cfThe desired output of the hardness value at all the internal locations of part led
to the development of 3-dimensional enmeshment.
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3-Dimensional enmeshment
Classification of workpiece by Biot number
Case 1: Lumped heat capacity model
Case 2: Exact model
Lumped heat capacity modelInput Conditions:
The dimensions of the box (D1, D2, & D3).
The initial temperatures of the part.
Temperature of the quenchant gas.
Where, Ta is the ambient temperature
Ti is the initial temperature of part
F0 (Fourier number) is and
Thus we can get the final temperature T, by using the above equations
[ ]0exp FBTT
TTi
ai
a=
20
.
cL
tF
=
pC
k
=
1.iB
1.>iB
Conductivity and specific heat as a function of temperature
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Bi > .1, exact solution to be used
Input:
Dimensions of the box (D1, D2, & D3).
Specify the origin as shown in the figure.
Input the values n, l ,m
The initial temperatures of the part.
The time step
Ambient or quenchant temperature.n
Dx 1=
l
Dy 2=
m
Dz 3=
Internal nodes
i j k1 (1 to L-1) (1 to m-1)2 (1 to L-1) (1 to m-1)
(n-1) (1 to L-1) (1 to m-1)
Boundary nodes
i j k0 (1 to L-1) 0, m1 (0 to L) 0, m n-1 (0 to L) 0, mn (1 to L-1) 0, m
i j k0, n (1 to L-1) 00, n (0 to L) 1
0,n (0 to L) m-10, n (0 to L-1) m
i j k0, n (1 to L-1) 00, n (0 to L) 1
0,n (0 to L) m-10, n (0 to L-1) m
Corner nodes: (0, 0, 0) (n, 0, 0) (0, L, 0) (n, L, 0) (0, 0, m) (n, 0, m) (0, L, m) (n, L, m)
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Microstructure evolution and property prediction
Properties to be determined
Hardness
Ultimate Tensile Strength
Yield Strength
Approach: Analytical approach for asquenched. Hardness value for allthe nodes to get hardness
distribution.
For other properties equations used,as a function of hardness. Theaverage value of hardness used todetermine other properties.
Database approach for as tempered.
Module 2Heating
Module 5Tempering
Heating below austenizing temperature
Output 3Mechanical Properties
after Quenching
Output 5Mechanical Properties
after Tempering
DB1
Material & TTT profile DB
Output 1Heat term &
temperatures
Module 4Phase transformation prediction
(Austenite to pearlite / bainite / martensite)Comparing cooling curve with TTT diagram to
determine microstructure
Mapping of microstructure to properties
DB4Quenchant DB
Module 1Workpiece classification & enmeshment
Workpiece shape classificationEnmeshment by Biot no.
Output 2Cooling curve of eachworkpiece and inside
the workpiece
Output 4Heat term &temperatures
Module 6Property prediction by empirical equations
DB2
Furnace DB
Heat transfer for gas quenching in same furnace
used in heating
Heat transfer for oil quenching in tank(load with fixture, single workpiece without fixture)
Heat transfer for gas quenching in differentfurnace
Initial condition
Cooling
Workpiece Furnace Load pattern Thermal schedule
Module 3
DB3Atmosphere DB
DB6
Tempering propertiesDB
DB5Quenching properties
DB
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Hardness
Microstructure after quenching
( )
( ) ( )[ ]TtTtww
nfs
fs
/log
1ln/1lnlog =
The kinetics of the growth of ferrite and pearlite are described using the
Avrami-Johnson-Mehl equation
where,
w : volume fraction of austenite transformed
b,n : coefficient and exponent of the austenite transformation kinetics,
t : timets : start timetf : finish time
= 0.01
= 0.99
( )( )Tt
wb
s
s=
1ln
sw
fw
( )nsttbw = .exp1
( ) ( )( )( )TMwww sBPM = .011.exp1*1
Reference: V. C. Prantil, M. L. Callabresi and J. F. Lathrop, SimulatingDistortion and Residual Stresses in Carburized Thin Strips, vol. 125, April 2003
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Hardness Calculation
A continuous cooling curve is
divided into constant temperature
steps with appropriate times . It is
assumed that the horizontal partsof this step function cause a
transformation comparable to the
transformation occurring at the
individual temperatures in theisothermal TTT-diagram. By an
iteration of the transformation
steps the final microstructure is
derived.
Tempera
tureT
Time t Time log t
step function
real courseof cooling
M
B
P
A
HV
HV
HV
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Regression Analysis
Hardness=f(C%, Martensite%)
The equations of the form:
H= ax2 +bx+c,x--- C%
The equation at 50% Martensite
y = -19.0476 x^2 + 64x + 20.1448
The equation at 80% Martensitey = 7.14286 x^2 + 50.6429x + 25.6529
Similarly, generating the HRC value for all the martensitic percentage points
Reference:http://people.hofstra.edu/faculty/Stefan_Waner/RealWorld/newgraph/regressi
onframes.html
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Ultimate tensile strengthUTS=a*HB+b
Brinell hardness is used
Aim is to find constants a and b.
Value of constants for stainless steel
Validation for low alloy steel (5140) having hardness of 167 HB.
UTS calculated by the mentioned equation comes to be 572.278 MpaAnd the UTS of a specimen having hardness 167 HB should be 573 Mpa
Reference: Mechanical properties of Work Materials, Edmund Isakov
Validation source:http://www.efunda.com/materials/alloys/alloy_home/steels.cfm
U.T.S = 508 HB - 3900(156-595) HBAISI 400-seriesMartensitic
U.T.S = 430 HB + 6530(140-190) HBAISI 400-seriesFerritic
U.T.S = 534 HB - 16280(190-370) HBAISI 300-seriesAustenitic
U.T.S = 457 HB + 16910(140-180) HBAISI 300-seriesAustenitic
U.T.S = 606 HB - 31600(250-400) HBAISI Type 201Austenitic
Ultimate tensile strengthHardness RangeDesignation and GradeClass
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Hardness Conversion tablesConversion of HRC to HB
HB = 17.602 HRC - 403.86661
HB = 19.038 HRC - 489.46056
HB = 15.962 HRC - 318.75551
HB = 12.473 HRC - 142.65046
HB = 10.025 HRC - 30.84541
HB = 8.872 HRC + 16.04036HB = 8.379 HRC + 33.73531
HB = 6.984 HRC + 76.13026
HB = 5.329 HRC + 119.62520
tofrom
to Brinell Hardness (HB)
Numbers
(HRC)
Equations to convert Rockwell hardness
(HRC)
Rockwell
Hardness
Conversion of HV to HB
HB = 0.940 HV - 0.2670500
HB = 0.909 HV + 15.1499400
HB = 0.944 HV +1.2399300
HB = 0.922 HV + 7.3299250
HB = 0.954 HV - 0.7249200
HB = 0.949 HV + 0.9199150
HB = 0.959 HV - 0.814985
tofrom
into Brinell Hardness (HB)Number (HV)
Equations to convert Vickers
hardness (HV)
Vickers
Hardness
Reference: Mechanical properties of Work Materials, Edmund Isakov
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Calculation of Yield Strength
The materials are classified into three categories, plain carbon, low alloy and
alloy steel.
For plain carbon steel kis between 0.6 to 0.65, for low alloy steel kis 0.65 to
0.75, and alloy steel kis 0.84 to 0.86.
The value of k has been further refined and added in the database for each
grade of steel.
k = Yield strength / U.T.S
bs k =
Reference:
http://www.efunda.com/materials/alloys/alloy_home/steels.cfm
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Implementation
Case Study 1 at American Heat Treating, CT
Material: Alloy Steel 4340Weight: 0.3 lbsFurnace: VFS Vacuum Furnace
Load : 5 baskets arranged load
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Case Study 1 at American Heat Treating, CT
Quench Gas Atmosphere Nitrogen
Quench Pressure 2 bar
Blower HP 160
40200Nitrogen (2bar)
Quenching
501950VacuumSoaking
1201750VacuumSoaking
1801000VacuumSoaking
From room
temp.
70-1000VacuumHeating
Time (mins)Temperature
(F)
Atmosphere
Content
Process
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Comparison of calculated and measured results
0
500
1000
1500
2000
2500
0 100 200 300 400 500
TC1(top)
TC2
TC3TC4
TC5
TC6
TC7
TC8
TC9
TC10
TC11
TC12(BOT)
CALC_S
CALC_F
Case Study 1 at American Heat Treating, CT
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Case Study 2 at Bodycote, Worcester, MA
Workpiece Stainless steelQuench Gas Atmosphere Nitrogen
Quench Pressure 2 bar
Blower HP 200
Furnace Abar Vacuum Furace
2001900VacuumSoaking
from roomtemp.
70-1900VacuumHeating
200200Nitrogen (2 bar)Quenching
Time (mins)Temperature
(F)
Atmosphere
Content
Process
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Case Study 2 at Bodycote, Worcester, MA Measured & Calculated results
0
500
1000
1500
2000
2500
0 100 200 300 400 500 600
Time (mins)
Temperature(F)
Meas. slow
Meas. fast
Calc. furnace
Set Point
Calc. fast
Calc. fast
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Case Study 2 at Bodycote, Worcester, MA
Dynamic cooling results
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Summary and future work
Discusses the function and domain of CHT- q/t
CHT- q/tdesigned to meet industrial need, close contact with industrieskept to review their needs and implement the idea.
The basic advantages lies in short computation time, easy to use and the
ability to integrate the part load and furnace model with the complete heattreatment process.
Database development (especially TTT and quenchant database)
Development and validation of property prediction module
Validation of the new interface as well as cooling module in industry.
Future work More case studies required to validate the system
Enhance database for TTT diagram and quenchant Analytical approach to find convective heat transfer coefficient
Analytical approach to find properties after tempering
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Industrial Applications of CHT- bf
Case studies performed at Bodycote ThermalProcessing, Worcester
Objective To study the effects of change in the load quantity and giving
recommendations for the thermal schedule redesign.
To study the effect of change in load arrangement and determination ofoptimal load pattern from the calculated temperature values.
To determine the pre-heat required to reach the set point temperature andhence to determine cycle time.
Scheduling of jobs in furnace after determining exact cycle time.
To study the effect of part orientation on the quality and distortion andhence to determine best suited load orientation.
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Pit Furnace
Alloy, 1000lbsOthers
Alloy, 100lbsSupports
Graphite, 50lbsHeating
elements
Furnace Accessories data
(weight and material)
0Rate of
cooling water
35Weight
1140 R.P.MSpeed
4.5Height
14Diameter
2Horse power
303Material
[ x] Yes [ ] NoRecirculation Fan
(one fan at top)
[ ] Yes [ x ] NoVacuum Furnace
NoExcess of preheated air (%)
No preheatAir preheated temperature
AirAtmosphere content
120 kw or 409416.58 BTU/hrConnected heat input
1000Minimum Operating Temperature
2500 FMaximum Operating Temperature
45 x 60Work space (LengthWidth Height) or
(diameter Height)
5 x 8External size(LengthWidth Height) or
(diameter Height)
ElectricHeating type(E.g. direct/indirect fired, electric)
VerticalBody Shape
(E.g. vertical, Horizontal)
Pit furnace, 416Furnace name
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Case study 1 at Pit furnace
Workpiece Information
2Work piece weight
1137Work piece Material
R. H. HandlesWork piece Name
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Load Pattern
362Total weight of workpiece in fixture, lbs
181Total quantity of workpiece in fixture
ArrangedLoad pattern, Fixture configuration
35, 25Fixture size (diameter , height) inch
300 lbsFixture weight
SolidSide wall, bottom (solid/net like)RoundFixture shape (rectangular/round)
BasketFixture type (basket/plate)
Arrangement of load pattern
11
Ring
1019Ring 5
14Ring 920Ring 4
16Ring 821Ring 3
17Ring 722Ring 2
18Ring 623Ring (Row)1
QuantityRowQuantityRow
Quantity in each ring
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Comparison of result (soaking time: 305 min)
Temperature-Time chart
0
200
400
600
800
10001200
1400
1600
1800
0 100 200 300 400
Time (min)
Temp(F) Part (slow)
Part (fast)
Furnace
Conclusion: Part Temperature remains almost constant after 180 mins. The
optimum cycle time prior to heat treating can be determined.
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Comparison of result (Reduced soaking time:
180 min)
Temperature-Time chart
0
200
400
600
800
1000
1200
1400
1600
1800
0 50 100 150 200
Time (min)
Temp(F) Part (slow)
Part (fast)
furnace
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Case study 2
Two types of part(same material)
present in the load
1. Qty = 300 2. Qty = 903
Wt. = 41 Wt. = 45Thus average workpiece wt =
0.0715
Work piece weight
17-4 stainless steelWork piece Material
Hitchiner part no. 87296 & 87292Work piece Name
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Load pattern
(41 + 45)/2 = 43
Total weight of workpiece in fixture,
lbs
(300 + 903)/2 =
601Total quantity of workpiece in fixture
RandomLoad pattern, Fixture configuration
35, 25Fixture size (diameter , height) inch
300 lbsFixture weight
SolidSide wall, bottom (solid/net like)
RoundFixture shape (rectangular/round)
BasketFixture type (basket/plate)
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Comparison of Result
Actual result
0
500
1000
1500
2000
2500
0 50 100 150 200 250
Time (min)
Temp
(F) Temp (furnace)
Temp (slow)
Temp (fast)
Conclusion: Great opportunity to reduce the cycle time
All 405F
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All case furnace
2 G.P.MRate of cooling
water
200Weight
1800 R.P.MSpeed
14.5 inchesHeight
10 inchesDiameter
5Horse power
330Material
[x ] Yes [ ] No (one fan at top)Recirculation Fan
900Opening area (inch2)
[ ] Yes [ x ] NoVacuum Furnace
15Excess of preheated air (%)
850Air preheated temperature (F)
Endothermic (RX) with enriching gas, dilution
air and ammonia additions
Atmosphere content
1000000, 60000 Btu/hrConnected heat input
Natural gasFuel (combustion air)
1400Minimum Operating
Temperature
1800Maximum Heating
30-48-30Work space (WidthLength
Height) or (diameter
Height)
5.5 4.7 4.8 ftExternal size(LengthWidth
Height) or (diameter Height)
Indirect gas firedHeating type
(E.g. direct/indirect fired,
electric)
HorizontalBody Shape
(E.g. vertical, Horizontal)
All case, 405Furnace name
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Case study on all case furnace (with connected
heat input 600,000 Btu/hr)
0.2312 lbsWork piece weight
8620Work piece Material
Hitchiner 243860Work piece Name
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Load Pattern
140.4 lbs
Total weight of workpiece in fixture,
lbs
607Total quantity of workpiece in fixture
1 x 2 x 5
Rows Columns Layers of fixtures
in furnace
RandomLoad pattern, Fixture configuration
29, 23, 4
Fixture size (Length, width, height)
inch
45 lbsFixture weight
Net likeSide wall, bottom (solid/net like)
RectangularFixture shape (rectangular/round)
BasketFixture type (basket/plate)
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Result
Load takes around 65 minutes to
reach the set point temperature,
although the time allotted to reach
the set point temperature is 30
minutes.
In all case furnace, 10 fixtures are
used for the part load and generally
the parts are randomly placed in thefixture, leaving no room to change
the part load design.
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Result by CHT-bf (same load in furnace with higher
heat input i.e increasing the connected heat input to 1million Btu/hr) The time required by the load to reach
set point temperature reduced from 65
to 40 minutes, as we increased the
connected heat input from 600,000Btu/hr to 1000000 Btu/hr, thus saving
around 25 minutes.
Conclusion: The cycle time can be
reduced.
Conclusion about All case furnace:
Connected heat input is the most
important parameter for the All-case
furnaces. We can determine suitable allcase furnace for a specific load by
CHT-bf
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Application, Advantages and limitation of CHT- bf
Determination of pre-heat and cycle time
Helps in deciding appropriate furnace
Designing optimum load and its arrangement
Determination of required heat input of the furnace Low computation time make it highly applicable in industry
User friendly interface and stability further increases its applicability
Limitation
Scheduling more than one type of parts of different geometry andmaterial, we have to take average dimension and a closely resembling
material. This may affect the result.
Needs improvement for random load pattern
Part load may require some assumptions
Only applicable for heating process
Needs a furnace efficiency parameter
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Industrial Application of CHT- cf
Case studies performed at Bodycote ThermalProcessing, Waterbury, CT
Objective
To study the effects of change in the load quantity and givingrecommendations for the thermal schedule redesign.
To study the effect of change in load arrangement, determination ofoptimal load pattern from the calculated temperature values.
To study the effect of part orientation on the quality and distortion andhence to determine best suited load orientation.
To study the effect of belt speed and gross productivity on the thermalprofile of parts and hence determine optimum belt speed and loadcapacity to maximize productivity.
[ ] i [ ]bB d Sh
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Mesh Belt Furnace
0051600Air505250004
0011600Air727000003
0001600Air728750002
000500Air1363000001
Through
metal
area
(in2)
Wall
Insulatio
n height(in)
Fan
Hors
epowe
r (HP)
Zone
temperat
ure(F)
Atmos
phere
content
Len
gth
(in)
Connecte
d heat
input(Btu/hr
)
Z
o
ne
90Furnace efficiency % (based on furnace age)
[ ] Yes [x ] NoVacuum Furnace
15Excess of preheated air (%)900Air preheated temperature (F)
Natural gasFuel
0Opening area of the end zone (in2)
324Opening area of the entrance zone (in2)
[x] internal [ ] externalBelt or conveyor return0.27Moving belt/conveyor unit weight (lbs/in2)
54Moving belt/conveyor width (in)
56 x 56Work space (Width Height)
Or (diameter ) (in)
90 x 96External size(Width Height)
Or (diameter ) (in)
[ ]Direct [x]indirect fired
[ ]electric
Heating type
[ ]pipe [x]boxBody Shape
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Case study 1
0.04 lbsWeight
1020 carbon steelMaterial
XHD005 screwName
0.25 inchWorkpiece width
0.25 inchWorkpiece length
0.25 inchHeight of layers
0.156 inchWorkpiece height
54 inchActual load width
600 lbs/hrGross productivity
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Result by CHT-cf & Measured result
Measured result
0
200
400
600
800
1000
12001400
1600
1800
0 20 40 60 80
Time (min)
Temp(F)
Channel 5 (Left)
Channel 1 (Right)
Channel 3 (center)
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C d 2 (d i diff l d
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Case study 2 (demonstrating different load
patterns)
0.02Work piece weight (lbs)1020 carbon steelWork piece Material
14004 standard screwWork piece Name
0.125Workpiece height
2Workpiece width
2Workpiece length
0.375Height of layers (in)
54Actual load width (in)
600Gross productivity
(lbs/hr)
R d l d
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Random load
Arranged load
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Arranged load
Manual load arrangement
Arranged load clubbing 15 parts as 1.
Weight, part load pattern changed accordingly
Improvement in result
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Improvement in result
Uniformity of thermal profile in load
Better quality achieved (confirmed by the quality department)
Application and advantages of CHT cf
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Application and advantages of CHT- cf
The affect of part load arrangement can be studied using CHT-cf, prior torunning the actual load. As shown in the case studies uniformity oftemperature can be achieved by choosing arranged load pattern.
Orientation of parts: We can judge the part orientation, which givesuniformity in temperature
The affect of belt speed on the thermal profile of parts can be studied,and the optimum belt speed (i.e cycle time ) can be determined.
Furnace Planning: CHT-cfcan help us in determining the importantparameters required for the furnace, e.g connected heat input required for
each zones, which can help in deciding the number of burners requiredfor each zones.
Limitation of CHT cf
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Limitation of CHT-cf
In the Atmosphere content, only atmosphere name can be mentioned. Nooption to quantify the atmosphere content.
While simulating the part load by CHT-cf, distortion of parts are notconsidered, while in actual industrial practice the cycle time, productionrate and load pattern arrangement are mostly considered keeping in viewthe final quality and distortion.
Need to make the program stable and user friendly. Sometimes it givessome extra profiles in the temperature-time chart.
Summary
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Summary
Several case studies validated with experimental results (using thermocouple)
Accuracy of the temperature profiles predicted by CHT-bfand CHT-cf
Judgment and approximation required in defining part load
Described the methods to troubleshoot CHT-bfand CHT-cf
Discussed in detail all the features
i.e, database management
Case studies and the experience
helped in development ofCHT- q/tas well
Motivation to work closely
with industries
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Thanks for your attention
QUESTIONS ?