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International Journal of Mechanical Engineering and Technology (IJMET)
Volume 8, Issue 3, March 2017, pp. 34–41 Article ID: IJMET_08_03_004
Available online at http://www.iaeme.com/IJMET/issues.asp?JType=IJMET&VType=8&IType=3
ISSN Print: 0976-6340 and ISSN Online: 0976-6359
© IAEME Publication Scopus Indexed
EXPERIMENTAL INVESTIGATION OF EFFECT
OF HEAT TREATMENT ON NOSE RADIUS OF
INSERT AND TEMPERATURE AT CUTTING
AREA IN TURNING OF TITANIUM (GRADE 2)
Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy
UG Final Year Student, Department of Mechanical Engineering,
Vidya Jyothi Institute of Technology, Hyderabad, India
Dr. V.V. Satyanarayana
Professor, Department of Mechanical Engineering,
Vidya Jyothi Institute of Technology, Hyderabad, India
ABSTRACT
Titanium and Titanium alloys are utilized in many aerospace applications due to a
combination of properties such as high strength at elevated temperatures and
relatively low density. However, these materials are problematic to machine and are
therefore referred to as difficult-to-cut materials. Compared to most materials, the
chip–tool interface temperatures during machining are extremely high, even at lower
cutting speeds, and tend to concentrate close to the cutting edge. These alloys when
machined results in the reduced tool life and effects the surface roughness of the
material. In this article to overcome the reduction in the tool life and development of
the temperature at the cutting area the titanium is heat treated. The temperature at the
cutting area in the turning is measured using Non-Contact Infrared Digital
Thermometer and the nose radius of the tool insert is measured using profile
projector.
Key words: Profile Projector, Tool Insert Nose Radius, Titanium, Heat Treatment.
Cite this Article: Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala
Saketh Reddy and Dr. V.V. Satyanarayana, Experimental Investigation of Effect of
Heat Treatment on Nose Radius of Insert and Temperature at Cutting Area in Turning
of Titanium (Grade 2). International Journal of Mechanical Engineering and
Technolog, 8(3), 2017, pp. 34–41.
http://www.iaeme.com/IJMET/issues.asp?JType=IJMET&VType=8&IType=3
1. INTRODUCTION
Titanium and its alloys are considered as important engineering materials for industrial
applications because of good strength to weight ratio, superior corrosion resistance and high
temperature applicability. Titanium alloys have been widely used in the aerospace and aircraft
industry due to their ability to maintain their high strength at elevated temperature, and high
Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy and
Dr. V.V. Satyanarayana
http://www.iaeme.com/IJMET/index.asp 35 editor@iaeme.com
resistance for corrosion. They are also being used increasingly in chemical process,
automotive, biomedical and nuclear industry.[1] The machinability of titanium alloys is very
poor when compared to both general steels and stainless steels, which imposes particular
demands on the cutting tools employed for machining , makes titanium alloys has a topic of
great interest for industrial production and scientific research worldwide. During machining,
conventional tools wear away rapidly because the poor thermal conductivity of titanium
alloys results in higher temperature closer to the cutting edge and there exists strong adhesion
between the tool and workpiece material.[2]
With advances in cutting tool materials, many difficult-to-machine materials can now be
machined at higher metal removal rates. None of these tool materials, however, seems to be
effective in machining titanium because of their chemical affinities with titanium. [3] New
development in tool coating also does not help titanium machining. Coating has a
lower thermal conductivity than the tungsten carbide insert, which prevents heat dissipation
from extremely concentrated high stress and high temperature at the cutting point. Titanium
carbide and titanium nitride coatings are not suitable for machining titanium alloys because of
their chemical affinities. In the present investigation, turning of titanium alloy is carried out
on both heat treated and non-heat treated rod and results showed an improvement of tool life
and reduction of temperature at cutting area for heat treated rod when compared with the Non-
heat treated rod.[4]
2. HEAT TREATMENT OF TITANIUM AND ITSALLOYS
Titanium and titanium alloys are heat treated for several reasons:
 To reduce residual stresses developed during fabrication (stress relieving)
 To produce the most acceptable combination of ductility, machinability, and dimensional and
structural stability, especially in alpha-beta alloys (annealing)
 To increase strength by solution treating and aging
 To optimize special properties, such as fracture toughness, fatigue strength, and high-
temperature creep Strength[5]
Stress relieving and annealing may be used to prevent preferential chemical attack in some
corrosive environments, to prevent distortion, and to condition the metal for subsequent
forming and fabricating operations. Hot isostatic pressing, a specialized heat treatment
process, can help narrow the fatigue property scatter band and raise the minimum fatigue life
of cast components. [6]
3. EXPERIMENTAL DETAILS
3.1. Material Employed
In this investigation commercially available titanium Grade 2 is undertaken. The mechanical
properties and chemical composition of the material are given in Table 1 and Table 2 [7]
respectively. The material in rod form of 20 mm diameter and 120 mm length is used for the
heat treatment, machining and further
Experimental Investigation of Effect of Heat Treatment on Nose Radius of Insert and Temperature
at Cutting Area in Turning of Titanium (Grade 2)
http://www.iaeme.com/IJMET/index.asp 36 editor@iaeme.com
Table 1 Mechanical Properties of Titanium Grade 2
Table 2 Chemical Specification of Titanium Grade 2
3.2. Heat Treatment
The process annealing is carried out for one out of the two rods in the melting furnace at the
conditions as specified in the Table 3
Table 3 Conditions for Heat Treatment
Temperature 450 o
C
Time 180 Mins
Type of cooling Furnace Cooling
Property Value
Yield Strength 275 Mpa
Ultimate Tensile Strength 345 Mpa
Elongation % >20 %
Reduction of Area % >30%
Chemical Value
Carbon, C < 0.08 %
Iron, Fe < 0.3 %
Oxygen, O < 0.25 %
Nitrogen, N < 0.03 %
Hydrogen, H < 0.015 %
Titanium, Ti Balance
Figure 1 (a) Heat Treatment
Furnace Outer view
Figure 1 (b) Heat Treatment
Furnace Inner view
Figure 1 (c) Heat Treated Titanium
Rod
Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy and
Dr. V.V. Satyanarayana
http://www.iaeme.com/IJMET/index.asp 37 editor@iaeme.com
3.3. Specifications of Turning Tool Holder and Insert Used in experiments
Sandvik coromant USA made external turning tool holder is used for the machining
throughout the experiment. The tool holder is shown in figure 2 and the specifications of the
tool holder is shown in the Table 4[8,9]
Figure 2 Tool Holder
Table 4 Tool Holder Specifications
Tool holder name MTJNR 2020K 16
Breakdown of tool holder name according to ISO nomenclature
Letter Convection Explanation
M Insert clamping method Top + hole clamping
T Insert type Triangle
J Holder style 27o
Auxiliary cutting edge
N Insert clearance angle 0˚
R Hand of tool Right
20 Shank height 20 mm
20 Shank width 20 mm
K Holder length 125 mm
16 Length of insert cutting edge 16 mm
The Sumitomo made triangle coated carbide insert EN10Z is used in the tool holder
throughout the experiment. The insert is shown in Figure 3 and specifications are shown in
Table 5[10]
Figure 3 EH10Z Triangle Insert
Experimental Investigation of Effect of Heat Treatment on Nose Radius of Insert and Temperature
at Cutting Area in Turning of Titanium (Grade 2)
http://www.iaeme.com/IJMET/index.asp 38 editor@iaeme.com
Table 5 Insert Specifications
Insert name EH10Z TNGG 160302 R ST
Breakdown Insert name according to ISO nomenclature
Letter Convection Explanation
T Shape Triangle
N Clearance Angle 0˚
G Tolerance on Size
Inscribed Circle Thickness Height
± 0.025 mm ± 0.025 mm ± 0.13 mm
G Insert Cross Section Type C Sink 70o
- 90o
16 Cutting Edge Length 27 mm
03 Thickness 3.18 mm
02 Nose Radius 0.2 mm
R-ST Chip breaker Geometry -
3.4. Measurement of Temperature at cutting Area
The temperature at the cutting area is measured with the help of infrared thermometer while
machining. The device is shown in Figure 4
Figure 4 Infrared Thermometer
3.5. Hardness Testing
The hardness test is carried out for the both rods i.e, Heat Treated Rod and the Non Heat
Treated on the Brinell Hardness Testing Machine. [11] Testing Details:
Test Procedure : IS 1500: 2005
Type of Hardness : BHN
Indentor : 2.5 mm
Load Applied : 187.5 Kgs
Location : Surface
Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy and
Dr. V.V. Satyanarayana
http://www.iaeme.com/IJMET/index.asp 39 editor@iaeme.com
4. RESULTS AND DISCUSSION
4.1. Hardness Testing
The Table 6 shows the comparison of hardness between Heat Treated and Non Heat Treated
Rod
Table 6 BHN Values
Heat Treated Rod
( BHN )
Non-Heated Rod
(BHN)
Impression 1 210 206
Impression 2 206 212
Impression 3 210 212
Average 208.66 210
4.2. Machining Test
The orthogonal cutting trials were carried out on HMT make High precision Lathe NH 22
(Figure 5) [12], which has a 7 kW motor power and the spindle rotation speed ranges from
40-2040 rpm in forward and 60-1430 rpm in reverse. In this Investigation the parameters
depth of cut and Speed are varied [13]. The other parameters like feed, coolant discharge rate ,
length of cut are kept constant .The machining is done to the both the rods i.e, heat Treated
and Non heat treated with the same input parameters and the temperature at the cutting area is
noted for each trial. The tool insert is changed after the machining of the Non heat treated rod
which helps to compare the change in the nose radius of the tool insert with the help of the
Profile Projector (Figure 6) The details of the experiment are shown in the Table 7.
Figure 5 HMT Lathe NH 22
Figure 6 Profile Projector
Experimental Investigation of Effect of Heat Treatment on Nose Radius of Insert and Temperature
at Cutting Area in Turning of Titanium (Grade 2)
http://www.iaeme.com/IJMET/index.asp 40 editor@iaeme.com
Table 7 Experimental Input parameters and temperatures measured
It is recorded low temperature at the tool chip interface with heated material for all the
machining parameters compared to non heated material. The reduction in temperature is high
at low speeds and depth of cut compared to high speeds and depth of cut. This is attributed
due to softening of material with heat treatment and increased easy sheering operation in
machining. Similarly the wear rate of the tool at nose in the machining of heat treated rod is
very low compared to Non heated rod machining .The results are in tandem with the
machining of ferrous materials.
Table 8 Nose Radius of the Inserts before and After Machining
The nose radius of the tool insert is measured before and after machining of both heat
treated and non heat treated rods. The Table 8 shows the details of the tool with machining
parameters
5. CONCLUSION
The present paper has investigated the effect of heat treatment of the material to be machined
with the tool insert nose radius and temperature at the cutting area. The major results can be
summarized as follows:
 The temperature at the cutting area is lower when machining the Heat treated Rod compared
to the machining of Non heat treated Rod
 Tool insert nose radius had increased when machined Non Heated Rod when compared to the
Heat Treated Rod
6. ACKNOWLEDGEMENT
The authors express their thanks to Head of the Mechanical Engineering Department,
Principal, Director and Correspondent of Vidya Jyothi Institute of Technology, Aziz Nagar,
Hyderabad for the help and support extended towards this work
Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy and
Dr. V.V. Satyanarayana
http://www.iaeme.com/IJMET/index.asp 41 editor@iaeme.com
REFERENCES
[1] Ramesh S, Karunamoorthy L, Palanikumar K. Fuzzy modeling and analysis of machining
parameters in machining titanium alloy. Mater Manuf Process. 2008; 23:439–47.
[2] Ibrahim GA. Tool wear mechanism in continuous cutting of difficult –to- cut material
under dry machining. Adv Mater Res. 2010; 126–8:195–201.
[3] Ozel T. Investigations on the effects of multi layered coated inserts in machining Ti-6Al-
4V alloy with experiments and finite element stimulations. CIRP Annuals –
Manufacturing Technology. 2010; 59:77–82.
[4] Aitha Shravan, Samatham Madhukar, Bootla Akhil, Dr. A. A. Sri Rama Krishna , "
Experimental and Numerical Analysis of Metal Removal Rate and Surface Finish on Al-
Ti Alloy", International Journal of Scientific Research in Science, Engineering and
Technology(IJSRSET), Print ISSN : 2395-1990, Online ISSN : 2394-4099, Volume 3
Issue 1, pp.407-411, January-February 2017. URL :
http://ijsrset.com/IJSRSET1731104.php
[5] Arbizu IP, Perez CJL. Surface roughness prediction by factorial design of experiments in
turning process. Journal of Materials processing Technology. 2003; 143–4:390–6.
[6] Ibrahim GA. The effect of dry machining on surface integrity of titanium alloy Ti-6Al-4V
ELI. Journal of applied science. 2009; 9(1):121–7.
[7] Krishna Sastry KV, Seshagiri Rao V, Palanikumar K, Dhanalakshmi R, Kuravi A .
Assessment of process parameters influencing delamination factor on the drilling of
CFRC composite material with TiN coated carbide tool. Indian journal of science and
technology. 2014; 7(2):142–50.
[8] S. Madhukar, A. Shravan, P. Vidyanand Sai and Dr. V.V. Satyanarayana (2016), A
Critical Review on Cryogenic Machining of Titanium Alloy (Ti-6Al-4V). International
Journal of Mechanical Engineering and Technology, 7(5), pp. 38-45
[9] Valarmathi TN, Palanikumar K, Sekar S. Parametric analysis on delamination in drilling
of wood composite panels. Indian journal of science and technology. 2013; 6(4):4347–56.
[10] Dhar N R P S, Chattopadhyay A B 2002 Journal of Materials Processing Technology 118
9-35
[11] Chen W 2000 International journal of machine tools and manufacture 4 0 455-66
[12] Thakur D, Ramamoorthy B, Vijayaraghavan L 2009 Materials & Design 30 1718-25
[13] Samatham Madhukar , Paaka Vidyanand Sai , Sumith Kumar and Dasari Jagath Prakash
(2016) , Experimental Investigation on Effect of Heat Treatment on Mechanical Properties
of Titanium Alloy (Ti-6Al-4V) ,International Journal of Current Engineering and
Technology, Vol.7, No.1 (Feb 2017) , pp-238-242
[14] Sreehari V.S, Vivin Muthanna, Pramodh.G and Sumit Chhetri, Effect of Heat Treatment
and Natural Agening on Microstructure and Mechanical Properties of A356 Reinforced
with Boron Carbide Composites. International Journal of Mechanical Engineering and
Technology, 7(4), 2016, pp. 61–74.

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DESIGN CONSIDERATIONS OF RADOMES: A REVIEW

  • 1. http://www.iaeme.com/IJMET/index.asp 34 editor@iaeme.com International Journal of Mechanical Engineering and Technology (IJMET) Volume 8, Issue 3, March 2017, pp. 34–41 Article ID: IJMET_08_03_004 Available online at http://www.iaeme.com/IJMET/issues.asp?JType=IJMET&VType=8&IType=3 ISSN Print: 0976-6340 and ISSN Online: 0976-6359 © IAEME Publication Scopus Indexed EXPERIMENTAL INVESTIGATION OF EFFECT OF HEAT TREATMENT ON NOSE RADIUS OF INSERT AND TEMPERATURE AT CUTTING AREA IN TURNING OF TITANIUM (GRADE 2) Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy UG Final Year Student, Department of Mechanical Engineering, Vidya Jyothi Institute of Technology, Hyderabad, India Dr. V.V. Satyanarayana Professor, Department of Mechanical Engineering, Vidya Jyothi Institute of Technology, Hyderabad, India ABSTRACT Titanium and Titanium alloys are utilized in many aerospace applications due to a combination of properties such as high strength at elevated temperatures and relatively low density. However, these materials are problematic to machine and are therefore referred to as difficult-to-cut materials. Compared to most materials, the chip–tool interface temperatures during machining are extremely high, even at lower cutting speeds, and tend to concentrate close to the cutting edge. These alloys when machined results in the reduced tool life and effects the surface roughness of the material. In this article to overcome the reduction in the tool life and development of the temperature at the cutting area the titanium is heat treated. The temperature at the cutting area in the turning is measured using Non-Contact Infrared Digital Thermometer and the nose radius of the tool insert is measured using profile projector. Key words: Profile Projector, Tool Insert Nose Radius, Titanium, Heat Treatment. Cite this Article: Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy and Dr. V.V. Satyanarayana, Experimental Investigation of Effect of Heat Treatment on Nose Radius of Insert and Temperature at Cutting Area in Turning of Titanium (Grade 2). International Journal of Mechanical Engineering and Technolog, 8(3), 2017, pp. 34–41. http://www.iaeme.com/IJMET/issues.asp?JType=IJMET&VType=8&IType=3 1. INTRODUCTION Titanium and its alloys are considered as important engineering materials for industrial applications because of good strength to weight ratio, superior corrosion resistance and high temperature applicability. Titanium alloys have been widely used in the aerospace and aircraft industry due to their ability to maintain their high strength at elevated temperature, and high
  • 2. Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy and Dr. V.V. Satyanarayana http://www.iaeme.com/IJMET/index.asp 35 editor@iaeme.com resistance for corrosion. They are also being used increasingly in chemical process, automotive, biomedical and nuclear industry.[1] The machinability of titanium alloys is very poor when compared to both general steels and stainless steels, which imposes particular demands on the cutting tools employed for machining , makes titanium alloys has a topic of great interest for industrial production and scientific research worldwide. During machining, conventional tools wear away rapidly because the poor thermal conductivity of titanium alloys results in higher temperature closer to the cutting edge and there exists strong adhesion between the tool and workpiece material.[2] With advances in cutting tool materials, many difficult-to-machine materials can now be machined at higher metal removal rates. None of these tool materials, however, seems to be effective in machining titanium because of their chemical affinities with titanium. [3] New development in tool coating also does not help titanium machining. Coating has a lower thermal conductivity than the tungsten carbide insert, which prevents heat dissipation from extremely concentrated high stress and high temperature at the cutting point. Titanium carbide and titanium nitride coatings are not suitable for machining titanium alloys because of their chemical affinities. In the present investigation, turning of titanium alloy is carried out on both heat treated and non-heat treated rod and results showed an improvement of tool life and reduction of temperature at cutting area for heat treated rod when compared with the Non- heat treated rod.[4] 2. HEAT TREATMENT OF TITANIUM AND ITSALLOYS Titanium and titanium alloys are heat treated for several reasons:  To reduce residual stresses developed during fabrication (stress relieving)  To produce the most acceptable combination of ductility, machinability, and dimensional and structural stability, especially in alpha-beta alloys (annealing)  To increase strength by solution treating and aging  To optimize special properties, such as fracture toughness, fatigue strength, and high- temperature creep Strength[5] Stress relieving and annealing may be used to prevent preferential chemical attack in some corrosive environments, to prevent distortion, and to condition the metal for subsequent forming and fabricating operations. Hot isostatic pressing, a specialized heat treatment process, can help narrow the fatigue property scatter band and raise the minimum fatigue life of cast components. [6] 3. EXPERIMENTAL DETAILS 3.1. Material Employed In this investigation commercially available titanium Grade 2 is undertaken. The mechanical properties and chemical composition of the material are given in Table 1 and Table 2 [7] respectively. The material in rod form of 20 mm diameter and 120 mm length is used for the heat treatment, machining and further
  • 3. Experimental Investigation of Effect of Heat Treatment on Nose Radius of Insert and Temperature at Cutting Area in Turning of Titanium (Grade 2) http://www.iaeme.com/IJMET/index.asp 36 editor@iaeme.com Table 1 Mechanical Properties of Titanium Grade 2 Table 2 Chemical Specification of Titanium Grade 2 3.2. Heat Treatment The process annealing is carried out for one out of the two rods in the melting furnace at the conditions as specified in the Table 3 Table 3 Conditions for Heat Treatment Temperature 450 o C Time 180 Mins Type of cooling Furnace Cooling Property Value Yield Strength 275 Mpa Ultimate Tensile Strength 345 Mpa Elongation % >20 % Reduction of Area % >30% Chemical Value Carbon, C < 0.08 % Iron, Fe < 0.3 % Oxygen, O < 0.25 % Nitrogen, N < 0.03 % Hydrogen, H < 0.015 % Titanium, Ti Balance Figure 1 (a) Heat Treatment Furnace Outer view Figure 1 (b) Heat Treatment Furnace Inner view Figure 1 (c) Heat Treated Titanium Rod
  • 4. Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy and Dr. V.V. Satyanarayana http://www.iaeme.com/IJMET/index.asp 37 editor@iaeme.com 3.3. Specifications of Turning Tool Holder and Insert Used in experiments Sandvik coromant USA made external turning tool holder is used for the machining throughout the experiment. The tool holder is shown in figure 2 and the specifications of the tool holder is shown in the Table 4[8,9] Figure 2 Tool Holder Table 4 Tool Holder Specifications Tool holder name MTJNR 2020K 16 Breakdown of tool holder name according to ISO nomenclature Letter Convection Explanation M Insert clamping method Top + hole clamping T Insert type Triangle J Holder style 27o Auxiliary cutting edge N Insert clearance angle 0˚ R Hand of tool Right 20 Shank height 20 mm 20 Shank width 20 mm K Holder length 125 mm 16 Length of insert cutting edge 16 mm The Sumitomo made triangle coated carbide insert EN10Z is used in the tool holder throughout the experiment. The insert is shown in Figure 3 and specifications are shown in Table 5[10] Figure 3 EH10Z Triangle Insert
  • 5. Experimental Investigation of Effect of Heat Treatment on Nose Radius of Insert and Temperature at Cutting Area in Turning of Titanium (Grade 2) http://www.iaeme.com/IJMET/index.asp 38 editor@iaeme.com Table 5 Insert Specifications Insert name EH10Z TNGG 160302 R ST Breakdown Insert name according to ISO nomenclature Letter Convection Explanation T Shape Triangle N Clearance Angle 0˚ G Tolerance on Size Inscribed Circle Thickness Height ± 0.025 mm ± 0.025 mm ± 0.13 mm G Insert Cross Section Type C Sink 70o - 90o 16 Cutting Edge Length 27 mm 03 Thickness 3.18 mm 02 Nose Radius 0.2 mm R-ST Chip breaker Geometry - 3.4. Measurement of Temperature at cutting Area The temperature at the cutting area is measured with the help of infrared thermometer while machining. The device is shown in Figure 4 Figure 4 Infrared Thermometer 3.5. Hardness Testing The hardness test is carried out for the both rods i.e, Heat Treated Rod and the Non Heat Treated on the Brinell Hardness Testing Machine. [11] Testing Details: Test Procedure : IS 1500: 2005 Type of Hardness : BHN Indentor : 2.5 mm Load Applied : 187.5 Kgs Location : Surface
  • 6. Samatham Madhukar, Birudala Raga Harshith Reddy, Rontala Saketh Reddy and Dr. V.V. Satyanarayana http://www.iaeme.com/IJMET/index.asp 39 editor@iaeme.com 4. RESULTS AND DISCUSSION 4.1. Hardness Testing The Table 6 shows the comparison of hardness between Heat Treated and Non Heat Treated Rod Table 6 BHN Values Heat Treated Rod ( BHN ) Non-Heated Rod (BHN) Impression 1 210 206 Impression 2 206 212 Impression 3 210 212 Average 208.66 210 4.2. Machining Test The orthogonal cutting trials were carried out on HMT make High precision Lathe NH 22 (Figure 5) [12], which has a 7 kW motor power and the spindle rotation speed ranges from 40-2040 rpm in forward and 60-1430 rpm in reverse. In this Investigation the parameters depth of cut and Speed are varied [13]. The other parameters like feed, coolant discharge rate , length of cut are kept constant .The machining is done to the both the rods i.e, heat Treated and Non heat treated with the same input parameters and the temperature at the cutting area is noted for each trial. The tool insert is changed after the machining of the Non heat treated rod which helps to compare the change in the nose radius of the tool insert with the help of the Profile Projector (Figure 6) The details of the experiment are shown in the Table 7. Figure 5 HMT Lathe NH 22 Figure 6 Profile Projector
  • 7. Experimental Investigation of Effect of Heat Treatment on Nose Radius of Insert and Temperature at Cutting Area in Turning of Titanium (Grade 2) http://www.iaeme.com/IJMET/index.asp 40 editor@iaeme.com Table 7 Experimental Input parameters and temperatures measured It is recorded low temperature at the tool chip interface with heated material for all the machining parameters compared to non heated material. The reduction in temperature is high at low speeds and depth of cut compared to high speeds and depth of cut. This is attributed due to softening of material with heat treatment and increased easy sheering operation in machining. Similarly the wear rate of the tool at nose in the machining of heat treated rod is very low compared to Non heated rod machining .The results are in tandem with the machining of ferrous materials. Table 8 Nose Radius of the Inserts before and After Machining The nose radius of the tool insert is measured before and after machining of both heat treated and non heat treated rods. The Table 8 shows the details of the tool with machining parameters 5. CONCLUSION The present paper has investigated the effect of heat treatment of the material to be machined with the tool insert nose radius and temperature at the cutting area. The major results can be summarized as follows:  The temperature at the cutting area is lower when machining the Heat treated Rod compared to the machining of Non heat treated Rod  Tool insert nose radius had increased when machined Non Heated Rod when compared to the Heat Treated Rod 6. ACKNOWLEDGEMENT The authors express their thanks to Head of the Mechanical Engineering Department, Principal, Director and Correspondent of Vidya Jyothi Institute of Technology, Aziz Nagar, Hyderabad for the help and support extended towards this work
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