+ All Categories
Home > Documents > HEAT TREATMENT OF FORGINGS

HEAT TREATMENT OF FORGINGS

Date post: 22-Oct-2021
Category:
Upload: others
View: 8 times
Download: 1 times
Share this document with a friend
16
HEAT TREATMENT OF FORGINGS M. K. SARKAR Asstt. Divisional Manager, Tata Steel INTRODUCTION Ferrous materials are widely used for the manufacture of components for the engineering applications. This is because of the fact that these materials can have wide range of mechanical properties. According to requirements one can select a particular grade of iron and steel and by suitable processes shapes can be given and then by heat treatment the required physical properties can be imparted. Application and use of steel is much more wide than that of iron is well known, because of its improved characteristic as regards hot and cold deformation. A steel is usually defined as an alloy of iron and carbon with carbon content between a few hundreth of a percent upto about 2% byweight. Other alloying elements can amount to 5.0% by weight in low alloy steels and in high alloy steels more than 10% by weight such as tool steels and stainless steels etc. Steels can exhibit a wide variety of properties depending upon composition as well as phases and micro-constituents present, which in turn depend on mechanical work during defon 1 ration, such as forging, rolling and final heat-treatment. The table indicates the improvemen t in physical properties as a result of heat treatment of a plain carbon steel hi ving carbon content of 0.35% and Manganese content of 0.70%. Physical properties As Forged As Heat treatment Tensile strength (Tons/Sq.in.) 37.0 43.0 Yield strength (Tons/Sq.in.) 20.0 27.0 % Elongation 23.0 27.0 Charpy V notch impact (Joules) 14.0 54.0 Hardness (BHN) 165 190 F-1
Transcript
Page 1: HEAT TREATMENT OF FORGINGS

HEAT TREATMENT OF FORGINGS

M. K. SARKAR Asstt. Divisional Manager, Tata Steel

INTRODUCTION

Ferrous materials are widely used for the manufacture of components

for the engineering applications. This is because of the fact that these

materials can have wide range of mechanical properties. According to

requirements one can select a particular grade of iron and steel and by

suitable processes shapes can be given and then by heat treatment the

required physical properties can be imparted. Application and use of steel

is much more wide than that of iron is well known, because of its improved

characteristic as regards hot and cold deformation.

A steel is usually defined as an alloy of iron and carbon with carbon

content between a few hundreth of a percent upto about 2% byweight. Other

alloying elements can amount to 5.0% by weight in low alloy steels and in

high alloy steels more than 10% by weight such as tool steels and stainless

steels etc. Steels can exhibit a wide variety of properties depending upon

composition as well as phases and micro-constituents present, which in turn

depend on mechanical work during defon 1 ration, such as forging, rolling and

final heat-treatment.

The table indicates the improvemen t in physical properties as a result

of heat treatment of a plain carbon steel hi ving carbon content of 0.35% and

Manganese content of 0.70%.

Physical properties As Forged As Heat treatment

Tensile strength (Tons/Sq.in.) 37.0 43.0

Yield strength (Tons/Sq.in.) 20.0 27.0

% Elongation 23.0 27.0

Charpy V notch impact (Joules) 14.0 54.0

Hardness (BHN) 165 190

F-1

Page 2: HEAT TREATMENT OF FORGINGS

BASIC OF HEAT TREATMENT

Heat-treatment is an operation involving the heating of the solid

metal to a definite temperature and to allow solid solution of different

phases and chemical compounds at that temperature, followed by

cooling at suitable rates in order to obtain certain physical properties

which are associated with changes in the nature, form, size and

distribution of microconstituents.

To understand the above statement one should know the structure

of 'plain steels' and 'allotrophy of iron'

The essential difference between ordinary steel and pure iron is the

amount of carbon in the former, which reduces the ductility, but

increases the strength and the susceptibility to hardening when rapidly

cooled from elevated temperature. On account of various microstruc-

tures which may be obtained by different heat treatments. The appear-

ance of structure of pure iron is typical, it is built up of a number of

crystals of the same composition given the name 'Ferrite' and is very soft.

The addition of carbon to the pure iron results in a considerable

difference in the structure which now consists of two constituents one is

pure iron i.e. "Ferrite' appears as white under microscope and the dark

parts representing the constituents containing the carbon. The carbon

is present as a compound of iron and carbon (6.67%) called "Cementite",

Fe3C. This is a hard and brittle constituent.

On microexamination these dark parts will be seen to consist of

two components occurring as wavy or parallel plates alternately dark and

light. The two phases are ferrite and cementite which form a eutectoid

mixture containing 0.87% carbon and known as 'Pearlite". The highest

strength is obtained when the structure consists only pearlite. The

presence of free cementite masses increases the hardness but reduces

the strength.

F-2

Page 3: HEAT TREATMENT OF FORGINGS

Fig-1 - is showing mechanical properties vs microconstituents

dependent on % carbon content in plain carbon steels

Iron-Carbon Phase Diagram

The diagram which depicts the temperature at which phase

changes occur duringvery slow cooling or heating, and in relation to the

carbon content, is called the iron-carbon phase diagram. This diagram

is the basis for a correct understanding of all heat-treatment operations,

(Fig.2 ).

Carbon is an element that stabilizes austenite by increasing the

range of austenite formation of steel. The maximum solubility of carbon

in austenite is about 2.06% at 1147°C. The percentage carbon capable

of going into solution in ferrite increases from zero at 910°C to a

maximum of 0.02% at 720°C. On further cooling at room temperature

this decreases to 0.008%. As the carbon content increases the transfor-

mation of austenite into ferrite decreases. This reaches a minimum value

of 0.8% carbon at 723°C which is called eutectoid composition. Steels are

classified with reference to this composition. Those with less than 0.8%

carbon are called hypoeutectoid steel and those with more are called

hypereutectoid steels.

REASONS FOR HEAT-TREATMENT OF FORGINGS

Forgings are commonly associated with banded grain structure,

as well as large grain size or mixed large and small grain size dependent

on forging practice. Alloy steel forgings are subjected to a conditioning

treatment before final heat-treatment to obtain best possible physical

properties and to maximise the life cycle under severe service conditions.

Hypereutectoid alloy steels are associated with carbide network

after hot working. Elimination of carbide network and thus producing a

structure that is more susceptible to 100% spheroidisation, calls for a

simple heat-treatment. The spheroidised structure provides improved

machinability and more uniform response to hardening.

F-3

Page 4: HEAT TREATMENT OF FORGINGS

Alloy carburising steel forgings are usually subjected to high

temperature normalising prior to carburising to minimise distortion and

to improve machinability.

Considering the above mentioned reasons it is imperative that the

forgings are subjected to heat-treatment prior to final machining. The

forgings are subjected to either Annealing or Normalising or both

depending on the grade of steel and the forging practice. In case of high

alloy tool steels it is recommended that reduction in size should be done

in multistages and should be annealed in between stages or reductions.

Annealing

Annealing is a generic term denoting a treatment that consists of

heating to and holding at suitable temperature followed by cooling at an

appropriate rate, primarily for softening of metallic materials. Generally,

in plain carbon steels annealing produces a ferrite-pearlite microstruc-

ture. Steels may be annealed to facilitate cold working, or machining, to

improve mechanical or electrical properties, or to promote dimensional

stability.

The "Fe-C" binary phase diagram can be used to better understand

annealing processes. Although no annealing process ever achieves true

equilibrium conditions, it can closely parallel these conditions. In

defining the various types of annealing, the transformation tempera-

tures or critical temperatures are usually used. These temperatures can

be calculated using the actual chemical composition of the steel. The

following equations will give an approximate critical temperature for a

hypoeutectoid steel:

AC1(°C) = 723 - 20.7 (%Mn) - 16.9 (%Bi) + 29.1(%Si) - 16.9(%Cr)

Std. deviation = + 11.5°C

AC3(°C) = 910 - 203 (%C) - 15.2 (%Ni)+44.7 (%Si)+104(%V)+31.5 (0/0Mo)

Std. deviation = + 16.7°C

F-4

Page 5: HEAT TREATMENT OF FORGINGS

"Guidelines for annealing"

The following seven rules may be used as guidelines for develop-

ment of successful and efficient annealing schedules :

1. The more homogeneous the structure of the as austenitized steel

the more completely lamellar will be the structure of the annealed

steel. Conversely, the more heterogeneous the structure of the as

austenitized steel, the more nearly spheroidal will be the annealed

carbide structure.

2. The softest condition in the steel is usually developed by

austenitizing at a temperature less than 55°C above Al and

transforming at temperature less than 55°C below A1.

3. Because very long time may be required for complete transforma-

tion at temperatures less than 55°C below Al allow most of the

transformation to take place at the higher temperature, where a

soft product formed, and finish the transformation at a lower

temperature, when the time required for completion of transfor-

mation is short,.

4. After the steel has been austentized, cool to the transformation

temperature as rapidly as feasible in order to minimise the total

duration of the annealing operation.

5. After the steel has been completely transformed, at a temperature

that produces the desired microstructure and hardness, cool to

room temperature as rapidly as feasible to decrease further the

total time of annealing.

6. To ensure a minimum of lamellar pearlite in the structure of

annealed 0.70 to 0.90% C tool steels and other low alloy medium

carbon steels, preheat for several hours at a temperature about

28°C below the lower critical temperature (Al) before austentizing

and transforming, as usual.

F-5

Page 6: HEAT TREATMENT OF FORGINGS

7. To obtain minimum hardness in annealed hypereutectoid alloy

tool steels, heat at the austenitizing temperature for a long time

(about 10 to 15 hrs.) then transform as usual.

These rules are applied most effectively when the critical tempera-

tures and transformation characteristic of the steel have been estab-

lished and when transformation by isothermal treatment is feasible.

"Different types of annealing are applied for different purposes" :

Full Annealing

It consists of austenitzation of the steel followed by slow

cooling. For hypoeutectoid steel, it consists of austenitizing the steel

at 10-30°C above the AC3 line and holding it at this temperature for

a desired length of time, followed by slow furnace cooling. This leads

to the formation of a fine ground austenite structure. The subse-

quent slow cooling enables the austenite to decompose at low degree

of supercooling so as to form pearlite and ferrite. In case of hypereu-

tectoid steel heated above AC1 to spheroidize the proeutectoid ce-

mentite. Therefore it is the general practice to use spheroidized

annealing. In case of heating above Acm temperature and cooled

slowly results in formation of proeutectoid cementite at the grain

boundries. Retarded cooling facilities ferrite precipitation as a sepa-

rate cluster. This might result in soft spots during hardening and

render the steel brittle to forming and service stresses, Fig.3 is

showing full annealing temperature.

Spheroidized Annealing

This is done by heating the steel just above or slightly below AC1

temperature for a prolonged time, followed by a slow cooling in order

to soften the steel as much as possible. It is adopted to spheroidize

the carbides of lamellar pearlite or secondary cementite.

F-6

Page 7: HEAT TREATMENT OF FORGINGS

Commonly four methods are practiced for this treatment :

First Method - The steel is heated nearer to AC1 temperature

and held at that temperature for a long time for the formation of

coarse globular cementite, the temperature should be as close to AC1

as possible.

Second Method - The steel is heated slightly above AC1 temperature

and held for a prolonged time followed by slow cooling at a rate of lo - 20°C

per hour upto 550 - 600°C and then cool in still air.

Third Method - It is heating the steel slightly above AC1 and

holding for a predetermined time and then cooling to just below AC1

temperature and holding for prolongod time and subsequently cool-

ing to the room temperature.

Fourth Method - Spheroidizing is done by repeatedly heating

and cooling just above and below AC1 temperature. During heating

above AC1 temperature only the small sized grains of cementite will

dissolve in the austenite, but there is insufficient time for the larger cementite grains to dissolve. In the subsequent cooling cycle, the

molecules of cementite are deposited mainly on the cementite grains

that are not dissolved in the austenite. Hence a coagulation process

occurs. This method taken less time compared to previous methods but difficult to perform.

Isothermal Annealing

This is derived from the exact knowledge of temperature - time

diagrams. This treatment consists of austenitizing the steel at the full

annealing temperature and then cooling rapidly to appropriate tem-

perature below Art by 50 - 60°C. This temperature is held for a

predetermined time enabling the complete austenite decomposition

to take place for producing a structure having optimum machinabil-

ity. After the transformation is complete, the steel is cooled in a

furnace, or air cooled or rapidly cooled.

F-7

Page 8: HEAT TREATMENT OF FORGINGS

Normalising

Overheated forgings and very large forgings are normalised to

refine the grain structure, to improve machinability, to relieve inter-

nal stresses and to improve mechanical properties.

Normalising consists of heating the steel above the critical

temperature AC3 or Acm and holding at this temperature for a short

time depending on the grade of steel to achieve homogenization of

austenite, hypoeutectoid steels are heated to 30 - 40°C above the Ac3

temperature and held at this temperature for 20 - 40 mins. depending

on the chemistry. Exceeding the indicated temperature range might

attribute to excessive austenite grain growth. Grain growth may

occur due to higher holding time. After desirable holding the material

cooled in air the resultant microstructure are composed of fine

pearlite with ferrite in hypoeutectoid steels. The newly formed grain

boundries do not correspond to the old ones. Hypereutectoid steels

are heated to 30 - 40°C above Acm temperature with a short holding

just sufficient to complete phase transformation and then cool in air.

Here alongwith grain refinement, dissolution of carbide network do

take place. Microstructure corresponds to fine grained pearlite with

cementite. This is more suitable for spheroidization. Alloy carburising

steels are usually normalized at higher temperatures than the

carburising temperature to minimise distortion in carburizing and to

improve machinability.

To refine the grains and to obtain required hardness normalising

and tempering is a preferred treatment for forgings of low-alloy heat

resistant steels. (C-0.45%, Cr-1.0%, Mo-0.5% and V-0.3%) AISI -

4137 & AISI 4140.

F-8

Page 9: HEAT TREATMENT OF FORGINGS

Multiple Normalising - This is done to obtain complete solution of

all lower temperature constituents in austenite by the use of high initial

normalising temperature (e.g. - 925°C) and to refine final pearlite grain

size by the use of a second normalising treatment at a temperature

closer to Ac3 temp. (e.g. - 815°C) without destroying the beneficial effects

of the initial normalising treatment. This is normally applied to carbon

and low alloy steels of large dimensions where extremely high forging

temperatures have been used (e.g. Loco axle forging) made of carbon

steels. Forgings made of a low carbon steel (o.18%) with 1% Mn

intended for low temperature service are double normalised to meet

subzero impact requirements.

F-9

Page 10: HEAT TREATMENT OF FORGINGS

Mechanical properties of steels as a function of - composition and structure

Id

The Structure, Properties and Heat Treatment 01 Metals

20

to

w

Ferrite SO

.olegill ■••■•■•■•■ . . .• ............

Pill"

_...............1 merit'',

0.8

s

2

(b) •

tAaNtev,S■

Page 11: HEAT TREATMENT OF FORGINGS

1700 •

1600

1500

• 1400 134)3'

1300

1154• .m z -

)148' 1100

1200

1000

900

800

700..

100

400

300

200

100

Tem

p era

ture

. C

/rant

Figure 9,4 Show:-; the lee-C; equilibrium .diakramibr carbon col

tents up to 76 •.: Ste ► lH art alloys of iron, carbon, and other elemepi that contain less than 2% cab on —most frequently .114 or less:Theryfor

- • •••• •

470) Low C <0.2x = ItronS . Grey gn:401; ert:i

14Jiii re cemer.ri:re +ferritV e C High C <2%

Fe - • 2.0 2.5' 3.0 . 3 5 4.0 4.5 Weight Percentage Carbon.

Fig. 0. The Fe-C* equilibrium diF:gram up .to 7°A! carbOn. Solid; lines indicate Fe-Fe3C diagram; dashed lines indicate

0

St-ads

Page 12: HEAT TREATMENT OF FORGINGS

gott ED ThiN.

1100

1000

alb

700

0

• 0.5 1.0 1.5 2.17

Ca ,bon vontint in •••14•4 ptIcunii

Patton 01 tho Fe-C diagrart with temperature ranges for protium annealing, 'ecrystallizatlee enneatIng, Stress relieving. anc: :pheraidiring indicated. Courtesy of M.D. Geib, Colorado School e!M111113, Gulden

1441

700

0.5 10

Clow:. (mom in *0104 purciall

. Portion of thu claurzi» with temperature rangua fur full annealing, notinalizing, hot working, t.nd homogenizing Indicated. Courtesy of M.D. Geib, Color:Wu School ul Mines, Gulden

•F 'C

2012 1003

1,32

1052

1472

292

I 112

932

152

10:0

1100

120 0

1300

F. _ 2912

2/44

2552

2372

r . "•k1,114i..:p 2192

2012

1032

1052

14/2

1702

1112

recryatalliaation al stresses 411111111PTrs

remove o n erstresses ■ ductility, toughness ▪ equiaxed'ployednal ferritO * no 'phase transformation 11 temp : below L.C.T. (Al) •46,0-7':,0-C

P 111M11111

▪ heat above 3 - check grain coarsen 11 . .furnace.1,bOk cool

hyper eutectoici ; coarse Pearlite • cementite name* a electrical tihe e ts

hypereutectoid fine P Cementite

• high carbon steels • globu ar carbide In ferrlit) 111E401Ilne

Page 13: HEAT TREATMENT OF FORGINGS

3

Annealing temperature 144.44

Effect of annealing

1 temperature on Properties of cold•worked metal

C .

Recovery iflecry:tallitation

Grain growth

Clain suucnne

,

Annealing temperate ra

Nor mellsed emboli stool

fully

► ile:111(M C111 bon steel

Elnot.pateJ--•••• ferrite t i

"

CO COW stillna

p•oolitt,

10

Page 14: HEAT TREATMENT OF FORGINGS

l'earliI•

Nadirs t- BalnIts

°Gina* • •

T 1 A4E TEA--(17-wer.

--7—/211-Nsfroz44-1.7/oAl

800et i "AU'S rier r

Eutectoid .emperattira

2 S' r...--- .

700 V" . •

I-

Austenile

500 -

13 400

300

AuslanIte

ZOO

600

• 1

— "so

100

Martansiie

10 100 to3 io4 10' in Seconds

\vsteriire Th( C. c.)

-> 723°C

Oi 43/C si-eei T/A4C TEMPER/4702F- TRANSF0/2/2447/0,0

47

■4"

A ee , Mprzremr/ 6514

Cc,ARSE PrAgLIT6' 38R4

FINE Priatez/

mARTENS/Te p 54gcArzu1_

Page 15: HEAT TREATMENT OF FORGINGS

INOI•

CI C

0 r• l• .1•••

'I'

• - 11 NI ■ 11111 1-1.'

""le ...LL° ;+ la :3 (1) et rt

715. ft° e ID

V.!. 2: i3

"11 .1 • • - (D

c3•• ta

(Ek :3' e

et .„4 73

-1 T. DI ca 0 -1 1:D. ■i—• (1) 4.44

C) • CL 1-1 " (7.1

CD 10- --I ."1 -,- rn ..9" :3; •• a), 414.4!

COg.. got)

.13 e.

rn ri► f-E Z

:0 =1

co • J' eq.

=r -71

:73

c:

co r+

K., :9: (0 :c cr !1):. ID. '3 ca ix tt c) co,_ . IA , —I z5"

— 41. (D .3 —' i•D. •3* ‘ cr ,. . .3 — CL ... ()

.- n. c) --.. al ill . !

x :?.. -1'; 0. ..3 .0 • ri = it' ii, C/ 43' •-••• . ,

ii-r 74: ... 03 cci .o. :3 la I.< () . 01: 4) ir: 0 . 4.

Ct t: 7t) trIL 'n Axt ..., 0 tc ...3 tin ..4., "r1 ?7. •-4" :U. • op ' - iD (Co

*45. ....In 1..7: 1 (0 C. eel' 7.1 1 (0 CI- .. (CO — , ea,. =." 17)

C. IT

al irp —1 4) at* rt

.--, •

ai.. :0( ,

CL 0,

•-r-

Page 16: HEAT TREATMENT OF FORGINGS

4;*

Atisrenroin 1) Grain Size a prior au; fijnite g.s.

• ASTM G.Size no.(N). n 2"

ant/tent coats& p.m Jr

' ., . / ...,,

2, 06Q . hor,Qogenous aus

I .5 / . , r / r / 99% this3

... __,..lrftlarant tine grain 764 .... •..,... ../._-____-- to al raslat dua to 0.5 %—atta.

PPI Al-----

time

ill* tu ,..‘ r• 4.1 !,,:' !i

• .. ,•1 ..A N. •

; \ii,....., .) :, .. ,. b , 0 . : . ,.‘ • .41

- • ;1:4'1,14 4. f*:k '''''.... / 'fil.;-.11:1, .,*:-I.)......*4-'.. i'4, i•.'.!.,,c • -IN"..' ' 'A'..71 4,•1 • ' " '. •.;, • 24.. 8-' -,it • ;Y.. ,...A

ler F.,; ‘At Gogfititt Grain increase .

low yield strength • low tougnrPFss

g hardenabilit) high et • 74

4.

4/ . / . ,,./ ,

(18%C

• lntergranular fracture-+ • cl)arse ppt e

• coarse plate martensite

(1) • ,

•■• .

■•••:1

e!" 474,

04, . r

8 sec Z •

• • 15 sec

. Formation of austenite (light patches) (ton pcariite as a function of thee. (Ref 7.10)

(c)

t4

(0) Martensitic microstructures with prior noskolle pain sizes of

(a) ASTM No. 1; (b) ASTM No. 3; (c) ASTM No. 5; (c1) ASTM No. 7; and (o) ASTM No. 9. These microsinrchnes were preparvif by lit:1111y teniperina ,still in .1 firltuchlurit. lru.nc aid solution its .11culiul. Mognificallori, IOU thawn here di JO.:'9. Mel 7.10)


Recommended