22
FEA 3.1 INT milling fluid ap fluid ap identifie wear an dry mil 3.2 DEV SYS photogr electric axis an provisio ASIBILIT TRODUCTI Based on th of hardene pplication pa pplication p ed that will nd cutting fo ling and con VELOPME STEM A special fl raph of the f It consists drive. The d the degree on is used to TY STUDI F ION he literature d AISI 434 arameters th parameters, a bringforth orce using T nventional w ENT OF MI luid applicat luid applicat Fig. 3.1 S of a P-4 fu fuel pump h e of rotation o control the CHA IES ON H FLUID AP e survey it w 0 steel with hat affects th a set of lev better cuttin Taguchi tech wet milling. INIMAL PU tion system w tor is shown Schematic view uel pump (B has a plunge n of the plun rate of cuttin 46 APTER 3 HARD MIL PPLICAT was decided h minimal fl he cutting p vels of fluid ng performan hnique and t ULSED JET was develop n in Fig. 3.2. w of fluid appl Bosch make er with helic nger determi ng fluid deli LLING W TION d to conduc luid applicat performance d application nce in terms the results a T FLUID AP ped for this p lication system ) coupled to al groove wh ines the rate ivered per st WITH MIN t a feasibili tion and to . After iden n parameter s of surface are to be com PPLICATIO purpose (Fig m o an infinit hich can rot e of fluid de troke accurat NIMAL ity study on identify the ntification of rs are to be finish, flank mpared with ON g. 3.1). The ely variable tate about its elivery. This tely. n e f e k h e e s s

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Page 1: CHA PTER 3shodhganga.inflibnet.ac.in/bitstream/10603/10120/9/09_chapter3.pdf · el pump (B as a plunge of the plun ... commercially available mineral oil and the formulation contained

 

FEA

3.1 INT

milling

fluid ap

fluid ap

identifie

wear an

dry mil

3.2 DEV

SYS

photogr

electric

axis an

provisio

ASIBILIT

TRODUCTI

Based on th

of hardene

pplication pa

pplication p

ed that will

nd cutting fo

ling and con

VELOPME

STEM

A special fl

raph of the f

It consists

drive. The

d the degree

on is used to

TY STUDI

F

ION

he literature

d AISI 434

arameters th

parameters, a

bringforth

orce using T

nventional w

ENT OF MI

luid applicat

fluid applicat

Fig. 3.1 S

of a P-4 fu

fuel pump h

e of rotation

o control the

CHAIES ON H

FLUID AP

e survey it w

0 steel with

hat affects th

a set of lev

better cuttin

Taguchi tech

wet milling.

INIMAL PU

tion system w

tor is shown

Schematic view

uel pump (B

has a plunge

n of the plun

rate of cuttin

46 

APTER 3HARD MIL

PPLICAT

was decided

h minimal fl

he cutting p

vels of fluid

ng performan

hnique and t

ULSED JET

was develop

n in Fig. 3.2.

w of fluid appl

Bosch make

er with helic

nger determi

ng fluid deli

LLING W

TION

d to conduc

luid applicat

performance

d application

nce in terms

the results a

T FLUID AP

ped for this p

lication system

) coupled to

al groove wh

ines the rate

ivered per st

WITH MIN

t a feasibili

tion and to

. After iden

n parameter

s of surface

are to be com

PPLICATIO

purpose (Fig

m

o an infinit

hich can rot

e of fluid de

troke accurat

NIMAL

ity study on

identify the

ntification of

rs are to be

finish, flank

mpared with

ON

g. 3.1). The

ely variable

tate about its

elivery. This

tely.

n

e

f

e

k

h

e

e

s

s

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47  

Fig. 3.2 Photograph of fluid applicator

1. Fluid tank 2. Delivery tube, 3. Variable speed controller 4. Fluid pump 5. Four outlets 6. DC Motor

An injector nozzle of single hole type with a specification DN0SD151 with a spray

angle of 0° was used as the fluid injector in this investigation. Fig. 3.3 presents the

photograph of the fluid injector.

Fig. 3.3 Photograph of fluid injector

1. Fluid inlet 2. Fluid delivery nozzle 3. Screw for adjusting fluid delivery pressure

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reciproc

The del

fluid no

cutting

pressure

in Fig. 3

Fig. 3.4 sho

cates as the

livery pressu

ozzle pressu

fluid into th

e at the injec

1.

The fluid co

3.4, the velo

ows the line

DC motor r

ure at the fl

ure tester as

he nozzle. A

ctor.

Nozzle 2. P

oming out o

ocity of whic

Fig.3.4 Line sk

e sketch of

rotates and d

luid injector

shown in Fi

pressure ga

Fig 3.5 Pressure gauge

f the injecto

ch depends u

48 

ketch of the flu

the fluid je

delivers cutt

can be set

ig 3.5. It ha

auge fixed at

Nozzle testere 3. Fluid tank

or consists o

upon the pre

uid jet

et. The plun

ting fluid thr

at any prede

as a hand op

t the top of t

k 4. Handle of

f myriads of

ssure set at t

nger of the

rough the flu

efined value

perated plun

the device w

f the plunger

f tiny drople

the fluid inje

fluid pump

uid injector.

e by using a

nger to force

will show the

ets as shown

ector nozzle.

p

.

a

e

e

n

.

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49  

Higher the pressure at the injector, higher will be the velocity of the individual particles.

The test rig facilitated independent variation of pressure at fluid injector (P), frequency of

pulsing (F) and the rate of fluid application (Q). The system can deliver cutting fluid

through four outlets simultaneously so that cutting fluid could be applied to more than one

location or more than one machine tool at the same time. The frequency of pulsing can be

varied infinitely through a DC variable speed motor with a control system designed for

this purpose.

The fluid applicator delivers cutting fluid at a rate of one pulse per revolution of

the DC motor. This facility enables application of very small quantity of cutting fluid per

pulse. If Q is the rate of fluid application in ml/min and F is the frequency of pulsing in

pulses/min, fluid applied per pulse is given by Q/F. For example if Q is 1 ml/min and F is

1000 pulses/min and the pressure at the fluid nozzle is set at 100 bar, then fluid delivered

per pulse is equal to 1/1000 = 0.001 ml while the velocity of the individual fluid particles

will be approximately equal to about 70 m/sec (Philip et al., 2000; Heywood, 1996). Thus

by varying the frequency of pulsing, the rate of fluid delivered per pulse can be controlled.

Pulsing jet aids in fluid minimization without compromising the velocity of individual

particles as the pressure at the fluid injector remains constant at the set value. It is reported

that the frictional forces between two sliding surfaces can be reduced by rapidly

fluctuating the width of the lubricant filled gap separating them (Uzi Landman, 1998).

When the pulsing jet is used, the width of the lubricant filled gap between the tool rake

face and the chip fluctuates with a frequency equal to the frequency of pulsing of the fluid

jet. Hence a pulsing jet of cutting fluid was used in this investigation to exploit the

expected reduction in the frictional forces between tool and chip.

Special fixtures (Fig. 3.6) were designed so that the injector nozzle could be

located in any desired position without interfering with the tool or work during metal

cutting operation.

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50  

       

Fig. 3.6 Fluid application at the backside of the chip 1. Fixture 2. Tool holder 3. Insert

3.3 SELECTION OF CUTTING FLUID

Since the quantity of cutting fluid delivered per pulse is extremely small, a

specially formulated cutting fluid was employed in this investigation. The base was a

commercially available mineral oil and the formulation contained other ingredients such as

friction modifiers, emulsifying agents, coupling agents and anti-corrosion agents

(Varadarajan et al., 2002b). It acted as an oil in water emulsion. Table 3.1 shows the

various constituents present in the cutting fluid formulated.

Table 3.1 Composition of the cutting fluid

S No. Name of the constituent Percentage

1 Petroleum Sulfonate (Molecular Weight=490 to 520) 15%

2 Ethylene Glycol 1% 3 Oleic Acid 3% 4 Triethaol Amine 3%

5 Alcohol Ethoxylate 2% - 6%

6 Mineral Oil (Paraffinic) the rest

Petroleum Sulphonate acts as a multifunctional additive. It can act as an

emulsifier, a rust inhibitor, a surfactant and as an EP agent. The polar nature of the

Sulphonate end of the molecule functions as a typical anionic surfactant. The tail of the

Sulphonate is made up of a hydrocarbon chain which has no charge. Sulphonates act on

the surface of oil droplets by binding at the tail. The head of the Sulphonate has a polar

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51  

charge, allowing the head to bond to water droplets. Thus, the Sulphonate can hold oil and

water apart so that they can co-exist and form an emulsion.

Ethylene glycol resists freezing due to its low freezing point and acts as a coupling

agent to increase the stability of the emulsion. The use of ethylene glycol not only

depresses the freezing point but also elevates the boiling point such that the operating

range for the heat transfer fluid is broadened on both ends of the temperature scale. The

increase in boiling temperature is due to pure ethylene glycol having a much higher

boiling point and lower vapor pressure than pure water.

Oleic acid is an unsaturated fatty acid which is used as an emulsifying or

solubilizing agent in aerosol products. Besides serving as an agent for improving the

lubricity of the cutting fluid (agent for lowering the friction coefficient – friction

modifier), this compound forms an effective agent for enhancing permeability.

In water soluble cutting fluids, Triethaol Amine is used to provide the alkalinity

needed to protect against rusting and it acts as an anti-oxidant. It also controls the

evaporation rate of water in cutting fluid.

Alcohol Ethoxylate is a nonionic surfactant created by adding ethylene oxide

groups to a long chain (high molecular weight) alcohol. Alcohol ethoxylates possess

greater resistance to water hardness than many other surfactants. It also acts as a secondary

emulsifier which enhances the emulsification capability of the sulfonate. It is formulated

from selected aliphatic hydrocarbons and alcohol ethoxylates known for its

biodegradability. It is approved as a product which is readily biodegradable falls into the

most biodegradable classification as defined by EPA.

Mineral oils are hydrocarbons obtained from the petrol refining of crude oil. Their

properties depend on the chain length, structure and refining level. This formulation was

developed and used successfully by varadarajan et al. (2002b) during their investigation on

turning of hardened AISI4340 steel. The same formulation is being tried in the present

investigation also.

3.4 SELECTION OF WORK MATERIAL

AISI4340 steel was selected as a work material which is widely used in die

making, automobile and allied industries. Its applications include structural use such as

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aircraft

connect

as rotor

strength

conside

the Tab

were us

this inv

3.5 SEL

TT8020

engine m

ting rods, ge

r shafts, disc

It is a throu

h and fatigue

This grade

ering its wide

ble 3.2.

Plates of 12

sed for this i

vestigation.

LECTION O

Coated carb

0 of TaeguT

mounts, gene

ear shafts, cr

s and welde

ugh hardenab

e strength. It

of steel is c

e range of ap

Table 3.

25mm length

nvestigation

F

OF CUTTIN

bide cutting

Tec which h

eral enginee

rank shafts,

d tubing app

ble low allo

t is less costl

considered a

pplication in

2 Chemical c

Element

C

Cr

Mn

Mo

Ni

P

Si

S

Fe

h, 75mm bre

n. Fig. 3.7 pr

ig. 3.7 Photogr

NG TOOL

g tools wit

has helical h

52 

ering applic

landing gea

plications (V

oy steel and

ly compared

as the work m

n the industry

composition of

0.38

0.7

0.6

0.2

1.6

0.0

0.1

0.0

Ba

eadth and 20

resents the p

raph of the wor

th the spec

higher positiv

cations suc

ar componen

Varadarajan e

is known fo

d to high allo

material in t

y. It has a c

f work material

%

8 – 0.43

7 – 0.9

6 – 0.8

2 – 0.3

65 – 2.0

35 max

15 – 0.3

04 max

alance

mm thickne

photograph o

rkpiece

ification AX

ve cutting e

h as prope

nts, heavy fo

et al., 2002a)

for its toughn

oy steels.

the present i

composition

l

ess hardened

of the workp

XMT 0903

edges as in F

eller shafts,

orgings such

).

ness, tensile

nvestigation

as shown in

d to 45 HRC

piece used in

PER-EML

Fig. 3.8 and

,

h

e

n

n

C

n

L

d

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Fig. 3.9

of the in

AXM

investig

respecti

the rec

technica

9 was used in

nsert.

Designation

T 0903 PER-E

A tool holde

gation. The

ively (Fig. 3

commendatio

al/material s

n the investi

F

T

D

EML 9.4

er with the s

length and

3.11). The c

ons of M/s

support for th

igation. Tab

Fig. 3.8 Photo

Fig. 3.9 Differe

Table. 3.3 Dim

D d₁

499 6.19

specification

d diameter o

cutting tool

TaeguTec

his research

53 

ble 3.3 gives

ograph of the i

ent views of the

mensions of the

Dim

a

97 1.245

n TE90AX 22

of the tool

inserts and t

India (P) L

work.

the dimensi

nsert

e insert

e insert

mension (m)

t

3.607

20-09-L (Fig

holder are

the tool hold

Limited who

ions of vario

R

0.508

g. 3.10) was

170 mm a

der were sel

o were exte

ous elements

ap

8.890

s used in this

and 20 mm

lected as per

ending their

s

s

m

r

r

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of type

the pho

Experiment

FN1U. The

tograph of th

1. Milling m5. Tool force

Fig

Fig.

s were carri

e clamping a

he experime

machine 2. Mie dynamometer

g. 3.10 Photog

3.11 Schemati

ed out in a c

area of the m

ental setup.

Fig 3.12 Exinimal fluid apr (Kistler type)

54 

graph of the too

ic view of the t

column and

machine is 90

xperimental setpplicator, 3. Flu 6. Dynamom

ol holder

tool holder

knee type v

00 mm × 23

tup uid supply lineeter display 7

vertical milli

0 mm. Fig.

e 4. Fluid injec7. Charge ampl

ing machine

3.12 shows

ctor lifier

e

s

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55  

3.6 MEASUREMENT OF PROCESS PARAMETERS

Cutting force was measured using a Kistler dynamometer of type 9257B

(Fig. 3.13). It consists of a piezoelectric dynamometer (Fig 3.14) and a multichannel

charge amplifier (Type: 5070A) as well as a data acquisition and analysis

system (DynoWare). This multicomponent dynamometer facilitates dynamic and

quasi-static measurement of the three orthogonal components of cutting force.

Fig.3.13 Kistler - data analysis and display system

Fig.3.14 Kistler dynamometer (type 9257B)

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(Fig. 3.

count o

Surface fini

15).

Flank wear

f 0.005 mm.

ish was me

Fig.3

was measu

.

Fig.3.16 Too

easured usin

3.15 Surface r

red using to

ol makers micr

56 

ng TR100 P

roughness teste

ool makers m

roscope (Metze

Portable Sur

er (TR100)

microscope

er- megastar 80

rface Rough

(Fig. 3.16)

031)

hness Tester

with a least

r

t

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57  

Surface morphology of the worn tool was carried out using Scanning Electron

Microscope of type JSM-6390 (Fig 3.17) with a magnification range of 5X to 300,000X.

The closer view of the worn tool on the display of Scanning Electron Microscope is shown

in Fig. 3.18.

Fig.3.17 Scanning electron microscope (JSM-6390)

Fig.3.18 A closer view of surface morphology of worn tool as the display

All measurements were repeated two times, and the average of these two

measurements was taken as the final value of tool wear, surface roughness, and cutting

force.

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58  

3.7 PRELIMINARY CUTTING EXPERIMENTS

Preliminary experiments were conducted using a single jet configuration

(Fig. 3.19) to find out the viability of fluid minimization scheme for hard milling and to

arrive at a set of fluid application parameters that can bring forth minimum surface

roughness, minimal flank wear and minimum cutting force. The experimental conditions

at which the preliminary cutting experiments were conducted are shown in table 3.4.

Fig. 3.19 Directions of cutting fluid application using single jet configuration

Table 3.4 Experimental conditions

Machine tool Vertical milling machine (FN1U)

Work material AISI4340 steel

Cutting insert AXMT 0903 PER-EML

Tool holder TE90AX 220-09-L

Tool Geometry Length – 9.499 mm, width – 6.197 mm, thickness - 3.607 mm, nose radius – 0.508 mm

Cutting speed 45 m/min

Feed 0.25 mm/tooth

Depth of cut 0.4 mm

Type of cutting fluid Specially formulated mineral oil based cutting fluid.

Environment Cutting fluid application through minimal fluid application

An eight run experiment was designed based on Taguchi technique (Lochner and

Matar, 1990) and the design matrix is shown in Table. 3.5.

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4

injector

fluid ap

cutting

Fig. 3.

Table 3

R

The experim

r (P), freque

pplication (D

fluid was ke

Table 3.6

Inpu

Pressure at f

Frequency of

Rate of fluid Direction o

.20 presents

Fig.

3.5 Design mat

Run No.

1 2 3 4 5 6 7 8

ments were c

ency of puls

D) were varie

ept at 10% o

Input paramet

ut parameter

fluid injector P

f pulsing (Pulse

application (mof fluid applica

a block diag

. 3.20 Block di

trix for eight-ruF

1 1 1 1 1 2 2 2 2

carried out w

sing (F), rat

ed at two lev

oil and the re

ters and their l

P(Bar)

es/min)

ml/min) ation Back

gram of the i

iagram represen

59 

un, two-level eFACTOR COLU

2 1 1 2 2 1 1 2 2

with two rep

e of fluid ap

vels as show

st water.

evels during pr

Level 1

50 (P1)

500 (F1)

5 (Q1) k side of chip (

input and ou

ntation of inpu

experiment withUMNS

3 1 2 1 2 1 2 1 2

plications. T

pplication (Q

wn in Table 3

reliminary cutt

(D1) Tool-w

utput parame

ut and output pa

h four factors

7 1 2 2 1 2 1 1 2

The pressure

Q) and the

3.6. The com

ting experimen

Level 2

100(P2)

750 (F2)

15 (Q2) work interface (

eters.

 

arameters

e at the fluid

direction of

mposition of

nts

(D2)

d

f

f

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in Table

single j

Fig

Fig. 3.1

tool-wo

directio

respecti

The respons

e 3.7

 

Table 3

Fig. 3.21 sh

et configura

g. 3.21 Schem

The two dir

19 namely fl

ork interface

on of fluid a

ively.

se table for

3.7 Response ta

hows the sche

ation.

atic view of di

rections of fl

luid applicat

e. Fig. 3.2

application a

eight-run, tw

able for eight-r

ematic view

rections of cut

luid applicat

tion at the ba

22(a) and Fi

at the back

60 

wo-level exp

run, two-level e

w of direction

tting fluid appl

tion employe

ack side of t

ig. 3.22(b)

side of the

periment wit

experiment wit

ns of cutting

ication using s

ed in this inv

the chip and

shows the

chip and at

th four facto

th four factors

fluid applic

ingle jet config

vestigation a

d fluid applic

schematic v

the tool-wo

ors is shown

ation during

guration.

are shown in

cation at the

view of the

ork interface

n

g

n

e

e

e

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(Thepso

depth o

compos

2002b).

Fig. 3.2

Fig. 3

Cutting par

onthi et al., 2

of cut were m

sition of cut

. .

22(a). Schema

.22(b). Schema(tool rotates

rameters we

2009; Rahm

maintained a

tting fluid w

atic view of flui(tool occupie

atic view of flus through 180˚

ere selected

man et al., 2

at 45 m/min,

was maintai

61 

id application aes the location a

uid applicationand occupies t

based on e

002). Acco

, 0.25 mm/to

ined at 10%

at the back sidat B)

n at the tool-wothe location at

earlier resea

ordingly the

ooth and 0.4

% oil in wa

e of the chip

ork interface

A)

arch work i

cutting spee

4 mm respec

ater (Varadar

in this field

ed, feed and

ctively. The

rajan et al.,

d

d

e

,

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3.7.1 R

attainab

flank w

parame

individu

analysis

ANOVA

cutting

at the fl

followe

applicat

Results of th

Fig. 3.23(a)

ble surface f

wear is availa

ters on the

ual fluid ap

s of variance

A summary

force. From

luid injector

ed by direc

tion.

Fig. 3.23(a)(P – Pressu

Fig. 3.23(P – Pressu

he prelimin

) presents th

finish. The r

able in Fig. 3

cutting forc

pplication p

e (ANOVA)

for the diffe

m the ANOV

forms the m

ction of flu

Relative signiure at fluid injec

3(b) Relative sure at fluid injec

nary exper

he relative s

relative sign

3.23(b) and

ce is presen

parameters o

) using Qual

erent input p

VA results (T

most significa

uid applicati

ificance of fluidctor, F – Frequ D – Direction

ignificance of ctor, F – Frequ D – Direction

62 

riments

significance

nificance of

the relative

nted in Fig.

on cutting

litek-4 softw

parameters on

Table 3.8(a)

ant paramete

ion, frequen

d application puency of pulsinn of fluid applic

fluid applicatiouency of pulsinn of fluid applic

 

of fluid app

the fluid ap

significance

3.23(c). Th

performance

ware. Table 3

n surface rou

) – 3.8(c)), it

er influencin

ncy of puls

parameters on sng, Q – Rate ofcation)

on parameters ng, Q – Rate ofcation)

plication pa

pplication pa

e of the fluid

he relative i

e was estim

3.8(a) – 3.8(

ughness, flan

t is evident t

ng the output

sing and ra

 

surface roughnf fluid applicati

 

on flank wear f fluid applicati

arameters on

arameters on

d application

influence of

mated using

(c) show the

nk wear and

that pressure

t parameters

ate of fluid

ness ion

ion

n

n

n

f

g

e

d

e

s

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Fig. 3.23(c) Relative significance of fluid application parameters on cutting force (P – Pressure at fluid injector, F – Frequency of pulsing, Q – Rate of fluid application

D – Direction of fluid application)

Table. 3.8(a) ANOVA summary for influence of fluid application parameters on surface roughness

Col#/ Factor

DOF (f)

Sum of sqrs (Ss)

Variance (V)

F – Ratio (F)

Pure sum (S′)

Percent P (%)

Pressure (bar) 1 0.601 0.601 40.929 0.587 59.141 Frequency (pulses/min)

1 0.056 0.056 3.862 0.042 4.24

Rate of fluid (ml/min)

1 0.007 0.007 .489 0 0

Direction 1 0.282 0.282 19.233 0.268 27.006 Other/Error 3 0.043 0.014 9.613

Total 7 0.992 100.00%

Table. 3.8(b) ANOVA summary for influence of fluid application parameters on flank wear Col#/ Factor

DOF (f)

Sum of sqrs (Ss)

Variance (V)

F – Ratio (F)

Pure sum (S′)

Percent P (%)

Pressure (bar) 1 0.003 0.003 104.583 0.003 58.338 Frequency (pulses/min)

1 0 0 10.533 0 5.369

Rate of fluid (ml/min)

1 0 0 0.843 0 0

Direction 1 0.001 0.001 58.593 0.001 32.437 Other/Error 3 -0.001 -0.001 3.853

Total 7 0.005 100.00%

Table. 3.8(c) ANOVA summary for influence of fluid application parameters on cutting force Col#/ Factor

DOF (f)

Sum of sqrs (Ss)

Variance (V)

F – Ratio (F)

Pure sum (S′)

Percent P (%)

Pressure (bar) 1 43725.331 43725.331 80.7 43183.505 64.026 Frequency (pulses/min)

1 2265.834 2265.834 4.181 1724.009 2.556

Rate of fluid (ml/min)

1 443.89 443.89 0.819 0 0

Direction 1 19385.597 19385.597 35.778 18843.771 27.938

Other/Error 3 1625.476 541.825 5.48

Total 7 67446.13 100.00%

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The results of the analysis which led to a set of levels of fluid application

parameters to minimize surface roughness, flank wear and cutting force are summarized in

Table. 3.9.

Table 3.9 Summary of fluid application parameters for optimum performance during preliminary experiments

Sl. No.

Output parameters Objective

Pressure at the fluid injector

(bar)

Frequency of pulsing

(pulses/min)

Rate of cutting fluid

(ml/min)

Direction of fluid

application

Projected values

1. Surface roughness (µm)

To minimize surface roughness 100(P2) 500(F1) 5(Q1) Tool-work

interface(D1) 0.623

2. Tool wear (mm)

To minimize tool wear 100(P2) 500(F1) 5(Q1) Tool-work

interface(D1) 0.025

3. Cutting force (N)

To minimize cutting force 100(P2) 500(F1) 5(Q1) Tool-work

interface(D1) 148.161

From the summary of results it was clear that fluid application parameters namely

pressure at fluid injector, frequency of pulsing and rate of fluid application have their own

influence on cutting performance. The set up for conventional wet milling is shown in

Fig. 3.24.

Fig. 3.24 Conventional wet milling setup

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65  

Confirmatory experiments were conducted to check the validity of the projected

values of surface roughness (Ra), Flank wear (Vb) and cutting force (F). During the

confirmatory experiments the cutting parameters such as cutting speed, feed and depth of

cut were maintained at 45 m/min, 0.25 mm/tooth and 0.4 mm respectively. The

composition of cutting fluid was maintained at 10% oil in water and the fluid application

parameters were maintained constant as in Table 3.9. The results of the confirmatory

experiments are shown in Table. 3.10. The experimental results matched well with the

projections.

Table 3.10 Results of the confirmatory experiments

Sl. No.

Output parameters Projected values Experimental

values

Percentage error (%)

1. Surface roughness (µm) 0.623 0.644 3.26

2. Tool wear (mm) 0.025 0.028 10.71

3. Cutting force (N) 148.161 168.56 12.10

Cutting experiments were conducted to compare the performance during dry

milling, conventional wet milling and milling with minimal fluid application with cutting

speed, feed and depth of cut maintained at 45 m/min, 0.25 mm/tooth and 0.4 mm

respectively. The fluid application parameters were maintained constant as in Table 3.9.

The results are presented in Table 3.11 and shown graphically through Fig. 3.25(a),

Fig.3.25(b) and Fig.3.25(c).

Table 3.11 Comparison of performance during dry, wet and milling with minimal fluid application

Sl. No. Cutting condition

Surface roughness (μm)

Flank wear (mm)

Cutting force (N)

1. Dry milling 1.671 0.131 483.61

2. Wet milling 1.193 0.059 239.56

3.

Milling with minimal fluid application (Optimized) 0.644 0.028 168.56

 

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66  

 

Fig. 3.25(a) Comparison of surface roughness during dry milling, wet milling and milling with minimal fluid application using single jet in optimized condition

 

 

Fig. 3.25(b) Comparison of flank wear during dry milling, wet milling and milling with minimal fluid application using single jet in optimized condition

  Fig. 3.25(c) Comparison of cutting force during dry milling, wet milling and milling with minimal

fluid application using single jet in optimized condition

The results show a definite advantage for milling with high velocity pulsed jet fluid

application when compared to conventional wet milling and dry milling.

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67  

3.8 Summary

The preliminary experiments clearly indicated that the fluid application parameters

such as pressure at the fluid injector, frequency of pulsing, rate of fluid application

and direction of fluid application do influence the cutting performance.

Comparison of surface roughness, flank wear and cutting force revealed that better

cutting performance can be achieved by hard milling with minimal cutting fluid

application.

During the preliminary experiments cutting parameters such as cutting speed, feed

and depth of cut were selected based on earlier research work in this field.

A systematic procedure must be laid out to arrive at a better combination of cutting

parameters.

Experiments are to be designed to explore the possibility of arriving at a set of

fluid application parameters (with a particular thrust to the direction of fluid

application and the number of jets used) to achieve better cutting performance.

The preliminary investigations revealed that the jet configuration that facilitates

fluid application at the tool-work interface has got an edge over the one that

facilitates fluid application at the tool-chip interface and both these directions can

promote improvement in cutting performance. Attempts must be made to arrive at

a jet configuration which can facilitate fluid application at both these directions.

Finally the operating as well as the fluid application parameters are to be fine tuned

to make them more suitable for industrial applications.

A model is to be established to simulate hard milling with minimal fluid

application and an attempt must be made to develop a performance enhancer that

can further improve the cutting performance.