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    Production EngineeringContents

    Chapters Topic Page No.

    Section I Metal Cutting and Tool LifeChapter - 1 Theory of Metal Cutting & Tool Life

    Theory at a glance

    Previous Years Conventional Questions

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    11

    28

    39

    59

    Section II Metal FormingChapter - 2 Cold Working, Recrystallisation and Hot

    WorkingTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    67

    67

    70

    73

    Chapter - 3 RollingTheory at a glance

    Previous 20-Years GATE, IES & IAS QuestionsPrevious 20-Years GATE, IES & IAS Answers

    7575

    8892

    Chapter - 4 ForgingTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    9595

    110

    115

    Chapter - 5 Extrusion, Drawing and other

    ProcessesTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    117

    117

    128

    134Chapter - 6 Sheet Metal Operations

    Theory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    137137

    157

    165

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    Indias No. 1 Production Engineering

    IES Academy Contents

    ww.iesacademy.com Email: [email protected] Page-ii25, 1

    stFloor, Jia Sarai, Near IIT. New Delhi-16 Ph: 011-26537570, 9810958290

    Chapters Topic Page No.

    Chapter - 7 Powder MetallurgyTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    169169

    172

    176

    Section III Metal CastingChapter - 8 Metal Casting

    Theory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    177177

    197

    205

    Chapter - 9 Special Cast ing ProcessesTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    209209

    219

    226

    Section IV Welding / Fabrication ProcessesWelding / Fabrication ProcessTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    229229

    259

    271

    Section V Metal Cutting MachinesChapter - 10 Metal Cutt ing

    Theory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    275275

    283

    288

    Chapter - 11 Drill ingTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    291291

    294

    297

    Chapter - 12 BoringTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    299299

    303

    306

    Chapter - 13 Milling

    Theory at a glance

    307

    307

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    Indias No. 1 Production Engineering

    IES Academy Contents

    ww.iesacademy.com Email: [email protected] Page-iii25, 1

    stFloor, Jia Sarai, Near IIT. New Delhi-16 Ph: 011-26537570, 9810958290

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    317

    322

    Chapter - 14 Gear ManufacturingTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    325325

    332

    336

    Chapter - 15 Shaper/Planner/SlotterTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    337337

    340

    342

    Chapter - 16 Grinding & FinishingTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    343343

    351

    357

    Chapter - 17 NC; CNC; DNC; FMS; Automation andRoboticsTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    361

    361

    383

    390

    Chapter - 18 Unconventional MachiningTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    393393

    420

    424

    Section VI MetrologyChapter - 19 Jigs and Fixture

    Theory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers429429

    431

    433Chapter - 20 Fits and Tolerances

    Theory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    434434

    437

    441

    Chapter - 21 Measurement of Surface TexturePrevious 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    443443

    446Chapter - 22 Miscellaneous of Metrology

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    448448

    450Chapter - 23 Miscellaneous of Product ion Technology

    Previous 20-Years GATE, IES & IAS Questions

    452

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    Indias No. 1 Production Engineering

    IES Academy Contents

    ww.iesacademy.com Email: [email protected] Page-iv25, 1

    stFloor, Jia Sarai, Near IIT. New Delhi-16 Ph: 011-26537570, 9810958290

    Previous 20-Years GATE, IES & IAS Answers 452454

    Section VII Engineering MaterialsChapter 24 Basic Concepts (Structure of Solids)

    Theory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    459459

    460

    462

    Chapter 25 Hardness TestTheory at a glance

    Previous 20-Years GATE, IES & IAS QuestionsPrevious 20-Years GATE, IES & IAS Answers

    463463

    465466

    Chapter 26 Crystalline MaterialTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    467467

    476

    482Chapter 27 Plain Carbon Steel

    Theory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    484484

    485

    487

    Chapter 28 Iron Carbon Equilibrium diagramTheory at a glancePrevious 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    488488491

    494Chapter-29

    Cast IronTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    495495

    498

    501Chapter-30

    Al loying Element of Steel and alloy SteelTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    502502

    506

    509Chapter 31 High Speed Steel

    Theory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    511511

    511

    513

    Chapter 32 Cutting Tool MaterialsTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    514514

    518

    521Chapter 33 Heat Treatment of Metals

    Theory at a glance

    522

    522

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    Indias No. 1 Production Engineering

    IES Academy Contents

    ww.iesacademy.com Email: [email protected] Page-v25, 1

    stFloor, Jia Sarai, Near IIT. New Delhi-16 Ph: 011-26537570, 9810958290

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers529

    535Chapter-34

    PlasticsTheory at a glance

    Previous 20-Years GATE, IES & IAS QuestionsPrevious 20-Years GATE, IES & IAS Answers

    538538

    540

    546Chapter-35

    ElastomerTheory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    548548

    548

    551Chapter 36 Use of Materials

    Theory at a glance

    Previous 20-Years GATE, IES & IAS Questions

    Previous 20-Years GATE, IES & IAS Answers

    552552

    553

    556

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    Student note

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    Section IMetal Cutting and Tool Life

    Contents of this section

    Chapter 1 : Theory of Metal Cutt ing & Tool Life Classification of Manufacturing Process Machining Machine tool Geometry of single point turning too l ASA or ANSI system Nose radius Orthogonal rake system (ORS) Mechanism of chip formation Buil t up Edge (BUE) formation Shear angle Assumption in the Merchant theory Limitations of use of MCD Theory of Lee and Shaffer Metal Removal Rate (MRR) Tool Wear, Flank Wear, Crater wear Tool life criteria Wear Mechanism Abrasion wear, Adhesion wear, Diffusion wear Tool life Rake angle Machinability

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    www.iesacademy.com E-mail: [email protected] Page-1________________________________________________________________________

    25, 1st Floor, Jia Sarai, Near IIT Delhi. New Delhi-110016 Ph: (011)-26537570, (M) 9810958290

    1. Theory of Metal Cutting & Tool LifeTheory at a glance (For IES, GATE & PSUs)

    Classification of Manufacturing Process Shaping or forming Joining process Removal process Regenerative manufacturing

    Regenerative Manufacturing Production of solid products in layer by layer from raw materials in different forms. Regenerative manufacturing is the latest one which is generally accomplished very rapidly and

    quite accurately using CAD and CAM for Rapid prototyping and tooling.

    MachiningMachining is an essential process of finishing by which jobs are produced to the desired

    dimensions and surface finish by gradually removing the excess material from the preformed

    blank in the form of chips with the help of cutting tools moved past the work surface. Machining

    is a removal process.

    Machining aim to Fulfill its functional requirements Improve its performance Prolong its service.

    Drawback in Machining The major drawback of machining process is loss of material in the form of chips.

    Machine toolA machine tool is a non-portable power operated and reasonably valued device or system of

    device in which energy is expended to produce jobs of desired size, shape and surface finish by

    removing excess material from the preformed blanks in the form of chips with the help of

    cutting tools moved past the work surface.

    Q. Why even a battery operated pencil sharpener cannot be accepted as a machine tool?

    Ans. In spite of having all other major features of machine tools, the sharpener is of low value.

    Geometry of single point turning toolBoth material and geometry of the cutting tool play very important roles on their performances

    in achieving effectiveness, efficiency and overall economy of machining.

    Classification: (According to the number of major cutting edges (points) involved.)

    Single point: turning, shaping, planning, slotting tools et Double point: drilling tools Multipoint: Milling, broaching, hobbing tools etc.

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    Rack angle and clearance angle

    The surface along which the chip moves upward is called Rack surface of tool. The other surface which is relieved to avoid rubbing with the machined surface, is called Flank.

    Rake angle: () Angle of inclination of rake surface from referenceplane i.e. normal to horizontal machined surface.

    Clearance angle: ( ) Angle of inclination of clearance or flank surfacefrom the finished surface.

    Following figure depicts the nomenclature of different angle and surface in turning.

    Discussion on Rack angleRake angle is provided for case of chip flow and overall machining. Rake angle may be positive or

    negative or zero.

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    Advantage

    Positive rake: reduce cutting force and thus cutting power.

    Negative rake: to increase edge strength and life of the tool. The use of negative rake angle started

    with the employment of carbide cutting tools. When we use positive rake angle, the force on the tool is

    directed towards the cutting edge, tending to chip or break it, carbide being brittle lacks shock

    resistance and will fail if positive rake angles are used with it. Using negative rake angles, directs the

    force back into the body of the tool away from the cutting edge, which gives protection to the cutting

    edge. The use of negative rake angle increases the cutting force. But at higher cutting speeds, at which

    carbide cutting tools can be used, this increase in force is less than at normal cutting speeds.

    High cutting speeds are, therefore, always used with negative rake, which requires ample power of the

    machine tool.

    The use of positive rake angles is recommended under the following conditions

    Machining low strength material

    Low power machine Long shaft of small diameter Set up lacks strength and rigidity Low cutting speed

    The use of negative rake angles is recommended under the following conditions.

    Machining high strength alloy Heavy impact loads High speed cutting With rigid set- up.

    Zero rake: to simplify design and manufacturing of the form tools.

    Discussion on Clearance angleIt is provided to avoid rubbing of the tool (flank) with the machined surface which causes loss of energy

    and damages of both the tool and the job surface. Hence, clearance angle is a must be positive (30 150).

    System of description of tool geometryi.e. Designation of cutting tools

    (I) Machine reference system: ASA or ANSI

    ASA American Standard Association System.

    ANSI American National Standards Institute.

    (Geometry of a cutting tool refers mainly to its several angles)

    (II) Tool reference system: ORS and NRSORS Orthogonal rake system or (ISO old)

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    NRS Normal rake system or (ISO new)

    (The planes of reference and the co-ordinate axes used for expressing the tool).

    (III) Work reference system:WRS

    Fig. A Single point cutting tool

    ASA or ANSI systemIn this system the angles of tool face, that, is its slope, are defined in two orthogonal planes, one parallel

    to and the other perpendicular to, the axis of the cutting tool, both planes being perpendicular to the

    base of the tool.

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    back rack angle ( )b

    side rack angle ( )s

    End relief angle ( )e

    side relief angle ( )s End cutting edge angle (Ce) Side cutting edge angle (Cs)

    Note: Side cutting edge angle (CS) It is the angle which prevents interference as the enters the work materials. Larger this angle, the greater the component of force tending to separate the work and the tool. At its increased value it will have more of its length in action for a given depth of cut. At its increased value it produce thinner and wider chip that will distribute the cutting heat. Zero SCEA is desirable when machining casting and forging with hart and scaly skins, because

    the least amount of tool edge should be exposed to the des action & the skin.

    Nose radius It is curvature of the tool tip. It provides strengthening of the tool nose and better surface finish. A sharp point on the end of a tool is highly stressed, short lived and leaves a groove in the path

    of cut. There is an improvement in surface finish and permissible cutting speed as nose radius is

    increases from zero value.

    But too large a nose radius will induce chatter.

    Tool designation [VIMP]To remember easily follow the rule

    Side will come last rake, relief, cutting edge finish with nose radius

    b -

    s -

    e -

    s - Ce - Cs R

    Back rack angle ( )b -side rack angle ( )s -End relief angle ( )e -side relief angle ( )s -End cutting edgeangle (Ce)-Side cutting edge angle (Cs) - Nose Radius (R)

    Orthogonal rake system (ORS)i - -

    1 Ce - R

    Inclination angle (i) side rake ( ) side relief ( ) end relief ( 1 ) End cutting edge (Ce)

    Approach ( ) nose radius.

    Approach angle () = 90 - CS[Sometimes is called principal cutting edge angle (Orthogonal cutting)]

    For Pure orthogonal cutting, i = 0

    For Oblique cutting, i 0

    Inter conversion between ASA & ORStan = tans sin + tanb cos

    tanb= cos tan+ sin tan i

    tans= sin tan - cos tani

    Gives tani = - tanscos + tan

    bsin

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    Mechanism of chip formation

    Mechanism of chip formation in ductile material

    Fig. Piispanen model of card analogy to explain chip formation in machining ductile materials

    Fig. Primary and secondary deformation zones in the chip.

    Mechanism of chip formation in brittle materialCause of chip formation: Yielding in ductile material

    Brittle fracture brittle material

    Fig. Development and propagation of crack causing chip separation.

    Types of chip formation depends on Work material (ductile, brittle)

    Cutting tool geometry (rake angle, cutting angle etc.)

    Cutting velocity and feed rate.

    Types of cutting fluid and method of application.

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    Types of chip Continuous chip Discontinuous chip

    Continuous chip with BUE

    Conditions for forming different types of chipDiscontinuous chip

    of irregular size and shape : work material brittle (grey cast iron) or regular size and shape : work material ductile but hard and work hardenable

    - feed large

    - tool rake negative

    - cutting fluid absent or inadequate

    Continuous chipWithout BUE: work material ductile

    Cutting velocity high

    Feed- low

    Rake angle positive and high

    Cutting fluid both cooling and lubricating.

    With BUE: work material ductile

    Cutting velocity medium

    Feed medium

    Cutting fluid - absent or in adequate.

    Built up Edge (BUE) formationCauses: In machining ductile material with long chip tool contact length, lot of stress and

    temperature develops in the secondary deformation zone at the chip tool interface. Under such high

    stress and temperature in between two clean surfaces of metals, strong bending may locally take place

    due to adhesion similar to welding. Such bonding will be encouraged and accelerated if the chip tool

    materials have mutual affinity or solubility. The weld material starts forming as an embryo at the most

    favorable location and thus gradually grows. With the growth of the BUE, the force also gradually

    increased due to wedging action of the tool tip along with the BUE formed on it. Whenever the force

    exceeds the bending force of the BUE, the BUE is broken or sheared off and taken away by the flowing

    chip. Then again starts forming and gray. This BUE changes its size during the cutting operation. It

    first increases, then decreases, and then again increases. Low cutting speed also contributes to the

    formation of BUE.

    Effects of BUE formation

    Harmful effect It unfavourably changes the rake angle at the tool tip causing increase if cutting force i.e.

    power consumption.

    Repeated formation and dislodgement of the BUE causes fluctuation in cutting forces andthus induce vibration.

    Poor surface finish.

    Good effect BUE protects the cutting edge of the tool i. e. increases tool life.

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    Reduction or Elimination of BUE Increase

    Cutting speed Rake angle Ambient work piece temperature.

    Reduce Feed Depth of cut

    UseCutting fluid

    Change cutting tool material (as cermets).

    Shear angle ()

    ( )c c

    c

    Vt sin 1

    t V cos

    lr

    l

    = = = = =

    andrcos

    tan

    1 sinr

    =

    Where r 1< r is chip thickness ratio, or chip compression factor or cutting ratio

    is chip reduction factor

    is shear angle

    is rake angle

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    ( ) ( )

    ( )

    c

    t ABsin sinr

    t ABcos cos

    r cos cos + r sin sin sin

    or r cos r tan sin tan

    or tan 1 rsin r cos

    rcosor tan

    1 rsin

    = = =

    =

    + =

    =

    =

    Form continuity equations

    c c

    cc

    c

    lbt l bt , l length of cut

    l tor r l length of chip

    l t

    = =

    = = =

    =

    = =

    c

    c c

    c

    c

    workpiece velocity V and chipvelocity V

    V bt V bt

    Vt

    or rt V

    For orthogonal cutting; 21

    e

    = =

    From this expression we will get

    (The value of can be reduced by)

    using tool having large positive rake Reduce friction by using lubricant.

    Cutting shear strain ()

    ( )

    ( )

    cot tan

    cos

    sin cos

    = +

    =

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    ( )

    S PM PN NM PN NM

    Y ON ON ON ONcot +tan

    + = = = = +

    =

    ( )

    ( )( )

    ( ) ( )( )

    ( )( )

    ( )

    NOM = 90 - (90 - ) - =

    sincos

    sin cos

    cos cos sin sin

    sin cos

    cos

    sin cos

    cos

    sin cos

    +

    + =

    + =

    =

    ESE-2004: Derive the expression for velocities in metalcutting.

    Velocities(i) The velocity of the tool relative to the work piece (V) called the cutting speed.

    (ii) The velocity of the chip relative to the work, Vs called the shear velocity.

    (iii) The velocity of the chip up the face of the tool Vc, called chip velocity.

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    ( ) ( ){ }c sV V V

    sin sin 90 sin 90 = =

    ( )

    ( )

    c

    c

    s

    V t sinr

    V t cos

    V cosand

    V cos

    = = =

    =

    Shear Strain rate: (Note: it is not shear strain it is rate of shear strain i.e. flow)

    ( )s

    s

    Vd

    dt thickness of shear zone t

    = =

    Determination of Un-deformed chip thickness: (VIMP)

    For single point cutting tool

    sin

    sin

    t f

    db

    =

    =

    Where t =Uncut chip thickness

    f = feed

    = 90 Cs= approach angle

    Cs= side cutting edge angle

    [Use above formula if not provided by examiner]

    Force relations: (For 2D orthogonal cutting only)When a cut is made the forces acting on the metal chips are:

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    1. Force Fs, is the resistance to shear of the metal in forming the chip. It acts along the shear plane.

    2. Force Fn, normal to the shear plane.

    3. Force N at the tool chip interface acting normal to the cutting face of the tool.

    4. Force F is the frictional resistance of the tool acting on the chip.

    Now if R is the resultant force of F & N and R is the resultant force of Fs and Fn for equilibrium R&R must be equal in magnitude an opposite in direction and collinear.

    Fc and Ft:The two orthogonal components (horizontal and vertical) Fc and Ft of the resultant force R can be

    measure by using a dynamometer.

    The horizontal component is the cutting force (Fc)

    and the vertical component is the thrust force (Ft)

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    And the power consumed during the process is cF V The force relations is as follows (VIMP)

    c t

    c t

    n c t

    s c t

    F = F sin F cosN F cos F sin

    F F sin F cos

    F F cos F sin

    +=

    = +

    =

    =F

    and = tanN

    [Where is the co efficient of friction, is friction angle]

    ( )

    ( )

    s

    2

    s c t

    s

    s

    Further study

    btShear plane area A

    sin

    F F sin cos F sinShear stress

    A bt

    =

    = =

    All these forces can be represented with the help of a circle known as the Merchant force circle.

    Fig. Merchant force circle Diagram (MCD)

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    Assumption in the Merchant theory The work material behaves like an ideal plastic. The theory involves minimum energy principal.

    As, s and are assumed to be constant, independent of .

    Limitations of use of MCD MCD is valid only for orthogonal cutting. By the ratio F/N, the MCD gives apparent (not actual) co-efficient of friction. It is based on single shear plane theory.

    From merchant Force circleFs = R cos ( ) +

    Fc = R cos ( )

    ( ) ( ) ( ) ( )c

    s cFor F .cos F sec coscos

    = + = +

    ( )sbt

    Shear plane area A b width of cutsin

    t = uncut chip thickness

    = =

    ( )( ) ( )

    ( ) ( )

    css

    s

    c

    F sec cosFAverage shear stress

    btA

    sin

    F sec cos sin

    bt

    + = =

    + =

    ( )

    ( ) ( )

    ( ) ( )

    sFor maximum shear stress 0 as & is constant for a case

    cos cos sin sin 0

    or tan cot tan 90

    or =4 2 2

    =

    + + =

    + = =

    +

    =4 2 2

    +

    But experimental fact reveals that varies greatly with and is not independent of . Considering

    this Merchant gives modified formula

    ( )

    = +

    =

    s so s s

    ns

    s

    1

    k where, is the normal stress on shear plane.

    F

    A

    and then 2 + - =cot k

    Theory of Lee and Shaffer

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    +

    They applied the theory of plasticity for an ideal-rigid-plastic material.

    They also assumed that deformation occured on a thin-shear plane.

    They derive.

    =4

    Compare turning with orthogonal cutting

    Fz = (Fc) = tangential component, main or major component, or power component, Force along the

    velocity vector largest in magnitude.

    Fy = radial or transverse component.

    Fx = axial component, feed force, Least in magnitude.

    Fxy = force along orthogonal plane2 2F +Fx y= = (Ft)

    Fx < Fy < FzNote Fc > FtWhen you solve problem take care so that above law should not be violated. Some examiner give

    question for that we have to take Ft = Fx in that case also above rule should not be violated.

    Some empirical formula (No need to remember)

    Fc = Fz = s1

    bf tan 1r

    +

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    t xy s

    1F F bf tan 1

    = =

    =

    =

    =

    0.6

    s u

    u

    0.74. .

    elongation

    1=cutting strain = tan

    r

    ultimate tensile stre

    %

    ngth

    Metal Removal Rate (MRR)Metal removal rate (MRR) = Ac.V= b t V

    Where

    Ac = cross-section area of uncut chip

    V = cutting speed =DN

    60

    Cutting power: E = Fc.V Fc = cutting force

    V = cutting speed =DN

    60

    Total energy (E) = shearing energy (Es) + Frictional Energy (Ef)

    (FcV) (FsVs) (F.Vc)

    Specific energy (e) =E

    MRR

    Total specific energy (e) = Specific shear energy (es) + specific friction energy (ef)or c s s c

    F .V F V FV

    btv btv btv= +

    ( )s c

    c

    V Vcos tNow and = r =

    V cos V t

    =

    ( )c s

    c

    F F cos F

    bt bt cos bt

    = +

    Tool Wear(a) Flank Wear(b) Crater Wear

    (c) Chipping off of the cutting edge.

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    Flank Wear: (Wear land)

    Reason Abrasion by hard particles and inclusions in the work piece. Shearing of the micro welds between tool and work material. Abrasion by fragments of built-up-edge ploughing against the clearance face of the tool. At low speed flank wear predominates. If MRR increased flank wear increased.

    Effect

    Flank wear directly affect the component dimensions produced. Flank wear is usually the most common determinant of tool life.

    StagesFlank Wear occurs in three stages of varying wear rates

    Primary wear

    The region where the sharp cutting edge is quickly broken down and a finite wear land is established.

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    Secondary wearThe region where the wear progresses at a uniform rate.

    Tertiary wear

    The region where wear progresses at a gradually increasing rate.

    In the tertiary region the wear of the cutting tool has become sensitive to increased tooltemperature due to high wear land.

    Re-grinding is recommended before they enter this region.

    Tool l ife cri teria ISO(A certain width of flank wear (VB) is the most common criterion)

    Uniform wear: 0.3 mm averaged over all past Localized wear: 0.5 mm on any individual past

    Crater wear Crater wear is more common in cutting ductile materials which produce continuous chips. Crater wear occurs on the rake face due to contact between the chip and the tool and the

    temperature depended diffusion and chemical wear mechanism are predominant in crater wear

    formation.

    At very high speed crater wear predominates For crater wear temperature is main culprit and tool defuse into the chip material & tool

    temperature is maximum at some distance from the tool tip that so why crater wear start at

    some distance from tip.

    The maximum crater depth exhibits an approximate linear increase with time. It increases with MRR.

    An increase in crater wear has little or no influence on cutting forces, work piece tolerance orsurface finish.

    Wear Mechanism1. Abrasion wear

    2. Adhesion wear

    3. Diffusion wear

    4. Chemical or oxidation wear

    Abrasion wear If a hard particle cuts or groves one of the rubbing surfaces then abrasive wear will occur.

    Coating the cutting edge or surface treatment for high hardness is a method for reducingabrasive wear.

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    Adhesion wear In the absence of lubricants surface may rub to each other and adhere to each other at the point

    of contact.

    The shearing and breaking of these interfacial junctions can lead to plucking of a piece ofmaterial out of one or both the surfaces.

    BUE may break away with a small portion of the tool. Use lubricant or coat surface with non-sticky hard coating reduce adhesive wear.

    Diffusion wear Solid state diffusion occurs when atoms in a metallic crystal move from a region of high atomic

    concentration to one of low concentration.

    Temperature exponentially increases the rate of diffusion.

    Chemical or oxidation wear Chemical wear occurs if rubbing surfaces are attacked by the environment to form a removable

    surface film. Generally oxide and hydroxide films will be formed in the presence of air.

    The fundamental causes of excessive tool wear when using cutting fluids at high velocity ischemical wear.

    Tool wear mechanismLow speed High speed Very high speed

    Mechanical properties

    Abrasion Micro fracture

    Fatigue Flow induced crack

    Nucleation and

    growth

    Chemical diffusion and

    convection

    Chemical diffusion

    Chipping off or fine cracks developing at the cutting edge

    Causes:

    Tool material is too brittle Weak design of tool, such as high positive rake angle As a result of crack that is already in the tool Excessive static or shock loading of the tool.

    Question: Why are ceramics normally provided as inserts for tools, and not as entire tools?

    Answer: Ceramics are brittle materials and cannot provide the structural strength required for a tool.

    Question: List the important properties of cutting tool materials and explain why each is important.

    Answer:

    Hardness at high temperatures - this provides longer life of the cutting tool and allowshigher cutting speeds.

    Toughness - to provide the structural strength needed to resist impacts and cutting forces Wear resistance - to prolong usage before replacement doesnt chemically react - another wear

    factor Formable/manufacturable - can be manufactured in a useful geometry

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    Tool life

    CriteriaTool life criteria can be defined as a predetermined numerical value of any type of tool deterioration

    which can be measured.

    Some of the ways Actual cutting time to failure. Volume of metal removed. Number of parts produced. Cutting speed for a given time Length of work machined.

    Taylors equation (based on Flank Wear)Causes

    Sliding of the tool along the machined surface Temperature rise

    nVT C= Where, V = cutting speed (m/min)

    T = Time (min)

    n = exponent depends on tool material

    C = constant based on tool and work material and cutting condition.

    =n nV T V T C =

    1 1 2 2

    Take log on both sides

    log V1 + n log T1 = log V2 + n log T2

    or n = 1 2

    2 1

    log V log V

    log T log T

    The following values may be take for n

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    n = 0.1 to 0.15 for HSS tool

    = 0.2 to 0.4 for carbide tool [IAS-99; IES-2006]

    = 0.4 to 0.6 for ceramic tool [NTPC-2003]

    Extended or Modified Taylors equation. . .

    n n nV T f d = C Where: d = depth of cut

    f = feed rate

    or T =1 2

    1/n

    1/n 1/n1/n

    C

    V .f .d

    1 2

    1 1 1

    n n n> >

    i.e Cutting speed has the greater effect followed by feed and depth of cut respectively.

    Cutting speed used for different materialHSS (min) < Cast alloy < Carbide < Cemented carbide < Cermets < Ceramics or sintered oxide (max)

    Effect of tool geometry on tool life

    Rake angle If rake angle is large, smaller will be cutting angle and larger will be the shear angle. This will

    reduce force and power of cut i.e. tool life. But increasing the rake angle reduces the mass of metal behind the cutting edge resulting in

    poor transfer of heat i. e. tool life.

    Therefore optimum value of= 140

    .

    Clearance angle If clearance angle it reduces flank wear but weaken the cutting edge, so best compromise is 80

    for HSS and 50 for carbide tool.

    Effect of work piece on tool material With hard micro-constituents in the matrix gives poor tool life. With larger grain size tool life is better.

    Chip EquivalentEngagedcutting edgelengthChipEquivalent(q)

    Planareaof cut=

    It is used for controlling the tool temperature.

    The side cutting edge angle alters the length of the

    engaged cutting edge without affecting the area of

    cut. As a result, the chip equivalent changed.

    When the side cutting edge angle is increased, the

    chip equivalent as well as the area of chip-tool

    contact is increased, without significantly

    changing the cutting forces.

    Increase in nose radius also increases the value of the chip equivalent and improve tool life.

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    Economics of metal cutt ing

    Remember the following formula

    =no oV T Ct

    o c c t m

    m

    c t m

    t

    c

    m

    C 1 nWhere T T if T ,C &C given

    C n

    1 nT if C &C notgiven

    n

    C 1 nif T is not given for problem.

    C n

    = +

    =

    =

    Units: Tc min (Tool changing time)

    Ct Rs./ servicing or replacement (Tooling cost)Cm Rs/min (Machining cost)

    V m/min (Cutting speed)

    Tooling cost (Ct) = tool regrind cost + tool depreciation per service/ replacement

    Machining cost (Cm) = labour cost + over head cost per min

    Unit volume of metal removal

    Time to machine a unit volume of metal 1C1

    d.f.V V= = [C

    1is cost.]

    Cost of machining per unit volume = Cm 1C

    V----- (i)

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    Number of tool replacement in 1C

    V=

    1

    1

    CCV times =

    T VT

    ( )

    1-n

    n1 t t 11

    t 1/n 1/n

    1-n

    nt 1m 1

    1/n

    n

    m

    t

    C .C C C VC

    Tooling cost = .CVT CC.V

    V

    C +C VC CTotal cost Y

    V C

    dY0 gives

    dV

    C nV = C.

    C n-1

    = =

    = +

    =

    VIMP Note In metal cutting operation the cutting speed for a minimum cost per piece and for maximum

    production rate (or minimum production time) gives a different cost and production rate.

    So the optimum cutting speed for the minimum cost of machining may not maximum profit. The minimum cost criteria will give a lower production rate, while the maximum production

    rate criteria will result in higher cost per piece.

    So we have to optimum these and will use no o

    V T = C

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    MachinabilityMachinability can be tentatively defined as ability of being machined and more reasonably as ease of

    machining.

    Such ease of machining or machining characters of any tool-work pair is to be judged by:

    Magnitude of the cutting forces Tool wear or tool life Surface finish Magnitude of cutting temperature Chip forms.

    Machinability will be considered desirably high when cutting forces, temperature, surfaces roughness

    and tool wear are less, tool life is long and chips are ideally uniform and short enabling short chip-tool

    contact length and less friction.

    The addition of certain materials live sulphur, lead and tellurium to non-ferrous and steel improvesmachinability. Sulphur is added to steel only if there is sufficient manganese in it. Sulphur forms

    manganese sulphide which exists as an isolated phase and act as internal lubrication and chip breaker.

    If insufficient manganese is there a low melting iron sulphide will formed around the around the

    austenite grain boundary. Such steel is very weak and brittle.

    Surface roughness

    Ideal surface

    ( )

    a

    a

    Sum of absolute values of all the area above and below the mean lineR

    Sampling length

    h

    4

    fpeak to-valley roughness (h) = [IAS-1999;GATE-2005]tan SCEA + cot ECEA

    h fR

    4 4 tan SCEA + cotECEA

    =

    =

    = =

    Practical Surface (has nose radius)

    2fh=

    8R

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    2h f

    1h

    R

    change of feed rate is more important than a change in the nose radius

    and depth of cut has no effect on surface geometry.

    Cutting fluid

    Purposes of application of cutting fluid in machiningand grinding

    Cooling of the job and the tool to reduce the detrimental effects of cutting temperature on the joband the tool.

    Lubrication at the chiptool interface. Cleaning the machining zone by washing away the chip . Protection of the embryonic finished surface a thin layer of the cutting fluid sticks to the

    machined surface and thus prevents its harmful contamination by the gases like

    , , ,SO O H S 2 2 2

    NxOy present in the atmosphere.

    The main aim of application of cutting fluid is to improve machinability through reduction of cutting

    forces and temperature, improvement by surface integrity and enhancement of tool life.

    Types of cutting fluids and their application Cutting fluids are employed in liquid form. Occasionally cutting fluids employed in gaseous form.

    Only for lubricating purpose, often solid lubricants are also employed in machining andgrinding.

    The cutting fluids, which are commonly used, are:

    Air blast or compressed air onlyMachining of some materials like grey cast iron become inconvenient or difficult if any cutting fluid is

    employed in liquid form. In such case only air blast is recommended for cooling and cleaning.

    WaterFor its good wetting and spreading properties and very high specific heat, water is considered as the

    best coolant and hence employed where cooling is most urgent.

    Soluble oilWater acts as the best coolant but does not lubricate. Besides, use of only water may impair the

    machine-fixture-tool-work system by rusting So oil containing some emulsifying agent and additive like

    EPA, together called cutting compound, is mixed with water in a suitable ratio ( 1 ~ 2 in 20 ~ 50). This

    milk like white emulsion, called soluble oil, is very common and widely used in machining and grinding.

    Cutting oilsCutting oils are generally compounds of mineral oil to which are added desired type and amount of

    vegetable, animal or marine oils for improving spreading, wetting and lubricating properties. As and

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    when required some EP additive is also mixed to reduce friction, adhesion and BUE formation in heavy

    cuts.

    Chemical f luidsThese are occasionally used fluids which are water based where some organic and or inorganicmaterials are dissolved in water to enable desired cutting fluid action.

    There are two types of such cutting fluid;

    Chemically inactive type high cooling, anti-rusting and wetting but less lubricating Active (surface) type moderate cooling and lubricating.

    Solid or semi-solid lubricantPaste, waxes, soaps, graphite, Moly-disulphide (MoS2) may also often be used, either applied directly to

    the work piece or as an impregnant in the tool to reduce friction and thus cutting forces, temperature

    and tool wear.

    Cryogenic cutt ing fluidExtremely cold (cryogenic) fluids (often in the form of gases) like liquid CO or N

    2 2are used in some

    special cases for effective cooling without creating much environmental pollution and health hazards.

    Selection of Cutting FluidThe benefits of application of cutting fluid largely depends upon proper selection of the type of the

    cutting fluid depending upon the work material, tool material and the machining condition. As for

    example, for high speed machining of not-difficult-to-machine materials greater cooling type fluids are

    preferred and for low speed machining of both conventional and difficult to machine materials greater

    lubricating type fluid is preferred. Selection of cutting fluids for machining some common engineering

    materials and operations are presented as follows:

    Grey cast iron Generally dry for its self lubricating property Air blast for cooling and flushing chips Soluble oil for cooling and flushing chips in high speed machining and grinding

    Steels If machined by HSS tools, soluble oil (1: 20 ~30) for low carbon and alloy steels and neat oil with

    EPA for heavy cuts

    If machined by carbide tools thinner soluble oil for low strength steel, thicker soluble oil ( 1: 10 ~

    20) for stronger steels and staright sulphurised oil for heavy and low speed cuts and EP cuttingoil for high alloy steel.

    Often steels are machined dry by carbide tools for preventing thermal shocks.

    Aluminium and its alloys Preferably machined dry Light but oily soluble oil Straight neat oil or kerosene oil for stringent cuts

    Copper and its alloys Water based fluids are generally used

    Oil with or without inactive EPA for tougher grades of Cu-alloy

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    Stainless steels High performance soluble oil or neat oil with high concentration with chlorinated EP

    additive.

    The brittle ceramics and cermets should be used either under dry condition or light neat oilin case of fine finishing. Grinding at high speed needs cooling (1: 50 ~ 100) soluble oil. For finish grinding of metals

    and alloys low viscosity neat oil is also used

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    Previous Years Conventional QuestionsConv.-1. During turning a carbon steel rod of 160 mm diameter by a carbide tool of

    geometry; 0, 0, 10, 8, 15, 75, 0 (mm) at speed of 400 rpm, feed of 0.32 mm/rev and 4.0mm depth of cut, the following observation were made. [ESE-2003]

    Tangential component of the cutting force, Pz = 1200 N

    Axial component of the cutting force, Px = 800 N

    Chip thickness (after cut), =2

    0.8mm.

    For the above machining condition determine the values of

    (i) Friction force, F and normal force, N acting at the chip tool interface.

    (ii) Yield shears strength of the work material under this machining condition.

    (iii) Cutting power consumption in kW.

    Solution:

    GivenD = 160 mm Fc = 1200 N = (Pz)

    0 xt xy

    0

    c

    P0 F P 800N

    sin

    75

    N 400rpm t 0.8mm

    f 0.32mm / rev

    d 4mm

    = = = =

    =

    = =

    =

    =

    ( )

    = = =

    = = =

    = =

    =

    c

    0

    t = fsin =0.3091mm

    d 4b 4.1411 mm

    sin sin75t 0.3091

    r 0.3864t 0.8

    rcostan r 1= r

    1 rsin

    or =tan r 21.125

    c t c t

    c t c t

    c

    0

    F = F sin F cos ;N F cos F sin

    F 0 F 1 800N F 1 F 0

    F 1200N

    F 800

    = 0.67N 1200

    tan 33.69

    + =

    = + = =

    = =

    = = = =

    s c ts

    s

    2

    c t

    2

    F F cos F sin

    btA

    sin

    F sin cos F sin

    bt

    1200 sin21.125cos21.125 800 sin 21.125

    0.3091 4.1411

    256.7MPa

    = =

    =

    =

    =

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    c

    c

    Power (P) = F V

    DN= F kW

    60

    1200 0.16 400= kW =4.021kW

    60 1000

    Conv.-2. While turning a C-15 steel rod of 160 mm diameter at 315 rpm, 2.5 mm depth of cutand feed of 0.16 mm/rev by a tool of geometry 00, 100, 80, 90,150, 750, 0(mm), the

    following observations were made. [GATE 1995]

    Tangential component of the cutting force = 500 N

    Axial component of the cutting force = 200 N

    Chip thickness = 0.48 mm

    Draw schematically the Merchants circle diagram for the cutting force in the

    present case.

    Solution:

    0

    0

    c

    c

    0

    Given : =10 t f sin 0.15455mm

    t75 r 0.32197

    t

    r cost 0.48mm tan = 0.33586

    1 r sin

    f = 0.16 mm/rev or =18.565

    = =

    = = =

    = =

    c

    t

    c t

    c t

    1

    F 500N

    F 200N

    F = F sin F cos 500sin10 200cos10 284N

    N F cos F sin 500cos10 200sin10 457.67N

    F 2840.62

    N 457.67

    tan 32

    =

    =

    + = + =

    = = =

    = = =

    = =

    n c t

    s c t

    F F sin F cos 500sin18.565 628cos18.565

    F F cos F sin 500cos18.565 628sin18.565

    = + = +

    = = +

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    Conv.-3. The following data from the orthogonal cutting test is available. Rake angle = 100,

    chip thickness ratio = 0.35, uncut chip thickness = 0.51, width of cut = 3 mm, yield

    stress of work material = 285 N/mm2, mean friction co-efficient on tool force = 0.65,

    [ESE -2000]

    Determine

    (i) Cutting force (Fc)

    (ii) Radial force (Ft)

    (iii) Normal force (N) on tool and

    (iv) Shear force on the tool (Fs ).

    Solution:

    Given: =10, r = 0.35, t = 0.51 mm, b = 3mm,s

    = 285 N/mm2.

    ss s s s s

    s

    0

    F btor F A

    A sin

    10

    r cos 0.35cos10r = 0.35; tan = 20.151 rsin 1 0.35sin10

    = = =

    =

    = =

    s

    0.51 3F 285 N = 1265.8 N

    sin20.15

    =

    ( ) ( )

    s

    0

    1 0

    From triangle ABC

    F R

    Sin B sin90Here B = 180 - 90-( ) 90

    Orsin B cos

    and tan tan 0.65 33

    =

    = +

    = +

    = = =

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    ( ) ( )s

    0

    F 1265.8Therefore,R = 1735N

    cos cos 33 20.15 10

    from triangle ADB

    F R

    sin sin90

    F Rsin =1735 sin 33 =944.95

    F 944.95N= 1453.8N

    0.65

    = = + +

    ==

    = =

    ( )

    ( ) ( )

    t

    0

    t

    2 2

    c t

    from ABE

    F R

    sin sin90

    or F Rsin 1735sin 33 10 678 N

    And F R F 1597N

    =

    = = =

    = =

    c

    t

    s

    Ans : (i) Cutting force (F ) 1597N(ii) Radial force (F ) 678N

    (iii) Normal force on the tool (N) = 1453.8 N

    (iv) Shear force (F ) 1265.8N

    ==

    =

    Conv.-4. Mild steel is being machined at a cutting speed of 200 m/min with a tool rake angle

    of 10. The width of cut and uncut thickness are 2 mm and 0.2 mm respectively. If

    the average value of co-efficient of friction between the tool and the chip is 0.5

    and the shear stress of the work material is 400 N/mm2, [ESE-2005]

    Determine (i) shear angle and

    (ii) Cutting and thrust component of the machine on force.

    Solution:

    Given: rake angle ( ) =100

    Width of cut (b) = 2 mm

    Uncut chip thickness (t) = 0.2 mm

    Coefficient of friction ( ) = 0.5

    Shear stress s = 400 N/mm2

    (i) We know that for maximum shear stress

    4 2 2

    = +

    Where = shear angle and = angle of friction therefore ( )1 1tan tan 0.5 26.6 = = =

    010 26.645 36.72 2

    = + =

    (ii) We know that F = Fc sin+ Ft cos

    N = Fc cos- Ft sin

    Fn = Fc sin + Ft cos

    Fs = Fc cos - Ft sin

    c t

    c t

    c t

    c t

    F tan FFand =

    N F F tan

    F tan10 F0.5 (i)

    F F tan10

    + =

    +=

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    ( )

    s

    s ss

    s

    btShear plane area (A )

    sin

    F F sinand Average shear stress

    A bt

    =

    = =

    ( )

    2c t

    s

    2

    c t

    c t

    F sin cos F sin

    bt

    F sin36.7cos36.7 F sin36.7or 400 = (ii)

    2 0.2

    solving (i) &(ii) we get

    F 420N &F 125N

    =

    = =

    [Note: Using Merchant force circle diagram you may solve this problem.]

    Conv.-5. In an orthogonal cutting process, the following observations were made:

    Depth of cut = 0.25 mm; width of cut = 4 mm, chip thickness ratio = 0.45 cutting

    velocity = 40 m/ min cutting force parallel to the cutting vector = 1150 N cutting

    force component normal to cutting velocity vector = 140 N, rake angle =18o.

    Determine resultant cutting force. Shear plane angle, friction angle and force

    component parallel to shear plane. [ESE 1992]

    Solution:2 2

    2 2

    t

    c

    0

    Resultant cutting force (R) = Fc Ft

    1150 140 1158.5N

    F 140tan A =

    F 1150

    A = 6.94 with parallel to cutting vector

    +

    = + =

    =

    ( ) 0

    r cos 0.45cos18tan = 0.49710

    1 rsin 1 0.45sin18

    shear plane angle 26.43

    = =

    =

    ( )c t

    c t

    Friction angleF F sin F cos

    1150sin18 140cos18 488.52N

    N = F cos F sin

    1150 cos18 140sin18 1050.45 N

    = +

    = + =

    = =

    0

    F 488.52

    N 1050.45

    tan ; 24.94

    = =

    = =

    s c tF F cos F sin

    1150cos26.43 140sin2643

    967.5N

    =

    =

    =

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    cPower F V

    401150 W

    60

    766.67W

    =

    =

    =

    Conv. -6. During turning process with 7- - 6 6 8 30 1 (mm) ASA tool the undeformedchip thickness of 2.0 mm and width of cut of 2.5 mm were used. The side rake

    angle of the tool was a chosen that the machining operation could be

    approximated to be orthogonal cutting. The tangential cutting force and thrust

    force were 1177 N and 560 N respectively. Calculate: [IAS-2003]

    (i) The side rake angle

    (ii) Co-efficient of friction at the rake face

    (iii) The dynamic shear strength of the work material [30 marks]

    Solution:

    Given:o

    s90 C 90 30 60 = = =

    i 0 fororthogonalcutting= o

    bback rake angle( ) 7 =

    sside rake angle( ) ?

    Orthogonal rake angle ( ) ?

    =

    =

    We know that

    s b

    b

    s

    o o

    s

    tan tan sin tan cos

    and tan cos tan sin tan i

    Therefore

    tan tan sin60 tan7cos60 (i)

    and tan7 cos60tan sin60tan0 (ii)

    Solving we get

    12 and 13.8

    = +

    = +

    = +

    = +

    = =

    Again givent c

    F 560N and F 1177N= =

    c t

    c t

    F F sin F cos

    1177sin13.8 560cos13.8 824.6N

    N F cos F sin 1009.4N

    = +

    = + =

    = =

    o

    F 824.60.81688

    N 1009.4

    tan 39.245

    = = =

    = =

    and 4 2 2

    13.8 39.24545 32.28

    2 2

    = +

    = + =

    s c ts

    s

    2

    c t

    2

    F F cos F sin

    btA

    sin

    F cos sin F sin

    bt

    1177cos32.28sin32.28 560sin 32.28

    2.5x0.2

    74.43MPa

    = =

    =

    =

    =

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    (ii) if velocity increased by 25% with f, d constant

    0.13

    0.6 0.3 0.6 0.3

    2

    C 36.5T

    V f d 50 0.25 2

    T=10.78 min

    = =

    (iii) If feed increased by 25% with V & d constant

    0.13

    0.6 0.3

    36.5T

    40 (0.3125) 2

    T=21.42 min

    =

    (iv) if depth of cut increased by 25% with V & f constant

    0.13

    0.6 0.3

    36.5T

    40 (.25) (2.5)

    T 35.85 min

    =

    =

    Conv. -9. Determine the optimum cutting speed for an operation on a Lathe machine using

    the following information: [IES 2009]Tool change time: 3 min

    Tool regrinds time: 3 min

    Machine running cost Re.0.50 per min

    Depreciation of tool regrinds Rs. 5.0

    The constants in the tool life equation are 60 and 0.2

    Solution

    Given: Tool changing time (Tc) = 3 min

    Tooling cost (Ct) = tool regrind cost + tool depreciation per service/ replacement

    = 3 min x Rs. 0.5 / min + Rs. 5.0

    = Rs. 6.5 / regrind

    Machining cost (Cm) = labour cost + over head cost per min = Rs. 0.5 / min

    n = 0.2 and C = 60

    Then optimum cutting time, to c c t mm

    C 1 nT T As T ,C &C given

    C n

    = +

    o

    6.5 1 0.2T 3 64min

    0.5 0.2

    = + =

    Therefore, Optimum cutting speed, VOn

    o o

    o n 0.2

    o

    V T C

    C 60or V 26m / min

    T (64)

    =

    = = =

    Conv.-10. In a certain machining operation with a cutting speed of 50 m/min, tool life of 45

    minutes was observed. When the cutting speed was increased to 100 m/min, thetool life decreased to 10 min. Estimate the cutting speed for maximum

    productivity if tool change time is 2 minutes. [ESE-2001]

    Solutions:

    1 1

    2 2

    Given:

    V 50m / min T 45min

    T 10min V 100m / min

    = =

    = =

    =

    =

    n

    1 1

    2 2

    n

    V T1

    V T

    50 45or 1

    100 10

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    =

    =

    = =

    nor 4.5 2

    or n ln 4.5 In2

    ln2or n 0.46085

    ln 4.5

    ( )

    n1 1

    0.46085

    Again V T C

    C 50 45 288.97

    =

    = =

    ( )

    +

    = + =

    to c

    m

    For optimum tool life

    C 1-nT = T

    C n

    1 0.460852 0 2.34min

    0.46085

    ( )

    n

    0 0

    0 n 0.46085

    0

    optimum velocity, V T C

    C 288.97or V 195m / min

    T 2.34

    =

    = = =

    Conv. -11. The following data was obtained from the tool-life cutting test of H.S.S. tool

    material, used to cut die steel: [ESE]

    Cutting speed,

    m/min

    49.74 49.23

    48.67 45.76 42.58

    Tool life, min 2.94 3.90 4.77

    9.87

    28.27

    Determine Taylors tool life equation.

    Solution:

    ( )2 2

    y = ax+b

    x y - N xya =

    x N x

    nVT = C.

    logeV + nlogeT = logeC

    or logeV = - nlogeT + logeC

    let y = ax+b where y = logeV

    a = -n

    x = logeT

    b = logeC

    N x y x2 xy

    1

    2

    34

    5

    1.0784

    1.361

    1.56232.2895

    3.3418

    3.9068

    3.8965

    3.88513.8234

    3.7514

    1.1629

    1.8523

    2.44085.2418

    11.168

    4.2131

    5.3031

    6.06978.7537

    12.5364

    5 9.633 19.263 21.866 36.876

    N x y 2x xy

    ( )

    ( )

    2 2

    2

    x y - N xya =

    x N x

    9.633 19.263 5 36.8760.071391

    9.633 5 21.866

    = =

    n = -a = 0.0714

    y = a x + bN

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    b

    y - a xb =

    N

    19.263 0.071391 9.633

    5

    3.99014

    C = e 54.06

    + =

    ==

    Conv.-12. A lathe tool bit with a rake angle of 20o is cutting a section of pipe with an inner

    diameter of 6 and an outer diameter of 6.25. The cut has a depth of 0.010 and

    the chip has a thickness of 0.020. If the lathe is turning at 200 rpm, and the

    measured cutting forces are FC = 300 1b, and Ft = 1252 lb.

    (a) What assumption must you make.

    (b) Find the following values using a graphical or numerical solution: (Marks

    are only awarded for correct answers) Fs, FN, F, N, , , , Vc, Vf, Vs.(c) What is the minimum horsepower required for the machine?

    (d) Given that the tube is aluminum, use another method to find the requiredhorsepower.

    Solution.

    =20deg Fc = 3001bs Ft = 1251bs t1 = d = 0.010in

    RPM = 200 t2 = 0.02in D =6 6.25

    2

    +

    =6.125in

    (a) Reasonable assumptions are that we are performing orthogonal cutting. This means

    that we are cutting fully through the wall of the tube. We also want to assume that the

    effects of the different cutting speeds from the inside of the tube are negligible

    (b) 1c2

    tr = = 0.5

    t ( )

    1 1c

    c

    r cos= tan = tan 0.56676719 = 29.5deg

    1-rsin

    F = Ft cos - fc sin = 2201bs N = Fc cos - Ft sin = 2391bsFs = Fc cos - Ft sin = 2001bs Fn = Ft cos + Fc sin = 2571bs

    F0.92

    N = = ( )= = a tan 0.92 42.6 deg

    = = =C

    RPM D 200 (6.125)V 321rpm

    12 12

    ( )S321cos20

    V 306fpmcos 29.5 20

    = =

    ( )

    = =f

    321cos29.5V 160rpm

    cos 29.5 20

    (c)( )

    C CC

    300 321F VHP 2.9HP

    33000 33000= = = For an efficient machine with no idle

    horsepower.

    (d) Q = d(6.25-6) CV 12=0.010 (0.25)321(12) = 9.633in

    min

    C uHP HR Q 0.3(9.63) 2.9HP= = =

    Conv-13. We have set up a lathe and are doing an orthogonal cut. The feed rate of the lathe

    is 0.1 mm, and the chip thickness after the cut is 0.2 mm. The depth of the chip

    being cut is 5 mm. The surface cutting speed of the tool is 2 m/s. The tool has a

    rake angle of 10 deg. The tangential force is measured as 200 N, and the cutting

    force is 500 N.

    (a) Calculate the shear force and velocity.

    (b) Calculate the total energy produced in the cut,

    (c) Calculate the energy used to shear

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    (d) Explain the difference between the total and the shear energy.

    Solution.

    Given , t1 = 0.1mm = 10 Vc = 2m

    s

    C

    F 500N=

    tc = 0.2 mm depth = 5 mm Ft = 200 N

    Find the total power and shear power.

    ( )C C C

    1C

    2

    m 1HPW F V 500N 2 1000W 1.34HP

    s 746W

    t 0.1r 0.5

    t 0.2

    = = = =

    = = =

    1 c

    c

    r cos= tan = 28.3

    1-rsin

    D

    Fs = Fc cos - Ft sin =345 N

    Vs = ( )C

    V cos m2.07cos s

    =

    S S S

    1HPW F V 714W

    746W

    = =

    = 0.96 HP

    Finally the ratio between cutting power and the shear power

    S

    C

    W 0.960.71

    W 1.34= =

    Conv-14. We are going to estimate the effects of feed rate on tool life. Some simple

    calculations yield the Taylor tool life coefficients of n = 0.4 and a C = 400. Find the

    change in tool life (in %) when velocity drops by (a) 20% and (b) 40%.

    Solution.

    Given, n = 0.4 C = 400 for Taylors equation

    For a) fv = 0.8 b) fv = 0.6 what is tf ?

    VT = C therefore (fvV)( ftT) = C

    C = VT = (fvV)( ftT)

    1 =n

    v tf f

    (a) fv = 0.8 ft = 1.75 T is 75% higher

    (b) fv = 0.6 ft = 2.59 T is 259%higher

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    Objective Questions (IES, IAS, GATE)Previous year GATE Questions

    GATE-1. Plain milling of mild steel plate produces [GATE-1995]

    (a) Irregular shaped discontinuous chips

    (b) Regular shaped discontinuous chip

    (c) Continuous chips without built up edge

    (d) Joined chips

    GATE-2. Friction at the tool-chip interface can be reduced by [GATE-2009]

    (a) decreasing the rake angle (b) increasing the depth of cut

    (c) Decreasing the cutting speed (d) increasing the cutting speed

    GATE-3 A built-up-edge is formed while machining [GATE-2002]

    (a) Ductile materials at high speed

    (b) Ductile materials at low speed

    (c) Brittle materials at high speed

    (d) Brittle materials at low speed

    Determination of shear angleGATE-4. The values of shear angle and shear strain, respectively, are [GATE-2006]

    (a) 30.3 and 1.98 (b) 30.3 and 4.23 (c) 40.2 and 2.97 (d) 40.2 and 1.65

    GATE-5. Minimum shear strain in orthogonal turning with a cutting tool of zero rake angle

    is [GATE -2009]

    (a) 0.0 (b) 0.5 (c) 1.0 (d) 2.0

    GATE-6. In a single point turning tool, the side rake angle and orthogonal rake angle are

    equal. is the principal cutting edge angle and its range is 0 90o o . The chip

    flows in the orthogonal plane. The value of is closest to [GATE-2008](a) 00 (b)450 (c)600 (d) 900

    GATE-7. In orthogonal turning of a low carbon steel bar of diameter 150 mm with uncoated

    carbide tool, the cutting velocity is 90 m/min. The feed is 0.24 mm/rev and the

    depth of cut is 2 mm. The chip thickness obtained is 0.48 mm. If the orthogonalrake angle is zero and the principal cutting edge angle is 90, the shear angle is

    degree is [GATE-2007]

    (a) 20.56 (b) 26.56 (c) 30.56 (d) 36.56

    Data for Q. GATE- 8 & GATE- 9 are given below. Solve the problems and choose correct

    answers.

    A cylinder is turned on a lathe with orthogonal machining principle. Spindle rotates at 200 rpm.

    The axial feed rate is 0.25 mm per revolution. Depth of cut is 0.4 mm. The rake angle is 10. In

    the analysis it is found that the shear angle is 27.75.

    GATE-8. The thickness of the produced chip is [GATE-2003]

    (a) 0.511 mm (b) 0.528 mm (c) 0.818 mm (d) 0.846 mm

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    GATE-9. In the above problem, the coefficient of friction at the chip tool interface obtained

    using Earnest and Merchant theory is [GATE-2003]

    (a) 0.18 (b) 0.36 (c) 0.71 (d) 0.908

    GATE-10. The effect of rake angle on the mean friction angle in machining can be explained

    by [GATE-1993](a) Sliding (coulomb) model of friction (b) sticking and then siding model of friction

    (c) Sticking friction (d) sliding and then sticking model of friction

    GATE-11. During orthogonal cutting of mild steel with a 10 rake angle tool, the chip

    thickness ratio was obtained as 0.4. The shear angle (in degrees) evaluated from

    this data is [GATE-2001]

    (a) 6.53 (b) 20.22 (c) 22.94 (d) 50.00

    GATE-12. In an orthogonal machining operation, the chip thickness and the uncut thickness

    are equal to 0.45 mm. If the tool rake angle is 0, the shear plane angle is

    (a) 45 (b) 30 (c) 18 (d) 60 [GATE-1998]

    Force relationsGATE-13. In orthogonal turning of medium carbon steel. The specific machining energy is

    2.0 J/mm3. The cutting velocity, feed and depth of cut are 120 m/min, 0.2 mm/rev

    and 2 mm respectively. The main cutting force in N is [GATE-2007]

    (a) 40 (b) 80 (c) 400 (d) 800

    GATE-14. In orthogonal turning of low carbon steel pipe with principal cutting edge angle

    of 90, the main cutting force is 1000 N and the feed force is 800 N. The shear angle

    is 25 and orthogonal rake angle is zero. Employing Merchants theory, the ratio of

    friction force to normal force acting on the cutting tool is [GATE-2007]

    (a) 1.56 (b) 1.25 (c) 0.80 (d) 0.64

    Common Data for Questions GATE- 15, 16 & 17:In an orthogonal machining operation:

    Uncut thickness = 0.5 mm Cutting speed = 20 m/min Rake angle = 15

    Width of cut = 5 mm Chip thickness = 0.7 mm

    Thrust force = 200 N Cutting force = 1200 N

    Assume Merchant's theory.

    GATE-15. The coefficient of friction at the tool-chip interface is [GATE-2006]

    (a) 0.23 (b) 0.46 (c) 0.85 (d) 0.95

    GATE-16. The percentage of total energy dissipated due to friction at the tool-chip interfaceis [GATE-2006]

    (a) 30% (b) 42% (c) 58% (d) 70%

    GATE-17. In a typical metal cutting operation, using a cutting tool of positive rake = 10, it

    was observed that the shear angle was 20. The friction angle is [GATE-1997]

    (a) 45 (b) 30 (c) 60 (d) 40

    Statement for Linked Answers questions GATE-18 and GATE-19Orthogonal turning is performed on a cylindrical work piece with shear strength of 250

    MPa. The following conditions are used: cutting velocity is 180 m/min. feed is 0.20 mm/rev.

    depth of cut is 3 mm. chip thickness ratio = 0.5. The orthogonal rake angle is 7 o. Apply

    Merchant's theory for analysis.

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    GATE-18. The shear plane angle (in degree) and the shear force respectively are

    (a) 52: 320 N (b) 52: 400N (c) 28: 400N (d) 28:320N [GATE-2008]

    GATE-19. The cutting and frictional forces, respectively, are [GATE-2008]

    (a) 568N; 387N (b) 565N; 381N (c) 440N; 342N (d) 480N; 356N

    GATE-20. In an orthogonal cutting test on mild steel, the following data were obtained

    Cutting speed : 40 m/min [GATE-2004]

    Depth of cut : 0.3 mm

    Tool rake angle : + 5

    Chip thickness : 1.5 mm

    Cutting force : 900 N

    Thrust force : 450 N

    Using Merchant's analysis, the friction angle during the machining will be

    (a) 26.60 (b) 31.50 (c) 450 (d) 63.40

    Energy considerations is metal cuttingGATE-21.Cutting power consumption in turning can be significantly reduced by

    (a) Increasing rake angle of the tool [GATE-2008]

    (b) Increasing the cutting angles of the tool

    (c) Widening the nose radius of the tool

    (d) Increasing the clearance angle

    Tool wear and tool li feGATE-22. For tool A, Taylors tool life exponent (n) is 0.45 and constant (K) is 90. Similarly

    for tool B, n = 0.3 and K = 60. The cutting speed (in m/min) above which tool A will

    have a higher tool life than tool B is [GATE-2010]

    (a) 26.7 (b) 42.5 (c) 80.7 (d) 142.9

    Statement for Linked Answer Questions 23 and 24:In a machining experiment, tool life was found to vary with the cutting speed in the

    following manner:

    Cutting speed (m/min) Tool life (minutes)

    60 81

    90 36

    GATE-23. The exponent (n) and constant (k) of the Taylor's tool life equation are

    (a) n = 0.5 and k = 540 (b) n= 1 and k=4860 [GATE-2009]

    (c) n = -1 and k = 0.74 (d) n-0.5 and k=1.15

    GATE-24. What is the percentage increase in tool life when the cutting speed is halved?

    (a) 50% (b) 200% (c) 300% (d) 400% [GATE-2009]

    GATE-25. In a machining operation, doubling the cutting speed reduces the tool life to1

    8th

    of the original value. The exponent n in Taylor's tool life equation VTn = C, is

    1 1 1 1( ) ( ) ( ) ( )

    8 4 3 2a b c d [GATE-2004]

    GATE-26. A batch of 10 cutting tools could produce 500 components while working at 50 rpm

    with a tool feed of 0.25 mm/rev and depth of cut of 1 mm. A similar batch of 10

    tools of the same specification could produce 122 components while working at 80

    rpm with a feed of 0.25 mm/rev and 1 mm depth of cut. How many components can

    be produced with one cutting tool at 60 rpm?(a) 29 (b) 31 (c) 37 (d) 42 [GATE-2003]

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    GATE-27.Tool life of 10 hours is obtained when cutting with single point tool at 63 m/min. If

    Taylor's constant C = 257.35, tool life on doubling the velocity will be [GATE-1996]

    (a) 5 hours (b) 25.7 min (c) 38.3 min (d) unchanged

    GATE-28. In horizontal milling process. (up/down) milling provides better surface

    finish and.. (up-down) milling provides longer tool life. [GATE-1992]

    GATE-29. Consider the following statements about nose radius [GATE-1995]

    1. It improves tool life 2. It reduces the cutting force 3. It improves the surface finish.

    Select the correct answer using the codes given below:

    (a) 1 and 2 (b) 2 and 3 (c) 1 and 3 (d) 1, 2 and 3

    WearGATE-30. What is approximate percentage change is the life, t, of a tool with zero rake angle

    used in orthogonal cutting when its clearance angle, , is changed from 10o to 7o?

    (Hint: Flank wear rate is proportional to cot a) [GATE-1999]

    (a) 30 % increase (b) 30%, decrease (c) 70% increase (d) 70% decrease

    GATE-31. Both the Iive centre and the dead centre of centre lathes are hardened and

    lubricated for reducing friction and wear. [GATE-1995]

    Above statement is

    (a) True (b) False (c) Cant says (d) Insufficient data

    Economics of metal cuttingGATE-32. The figure below shows a graph which

    qualitatively relates cutting speed and

    cost per piece produced.

    The three curves 1, 2 and 3 respectively

    represent

    (d) Machining cost, non-productive cost,

    tool changing cost

    (b) Non-productive cost, machining cost,

    tool changing cost

    (c) Tool changing cost, machining cost,

    non-productive cost

    (h) Tool changing cost, non-productive

    cost, machining cost [GATE-2005]

    MachinabilityGATE-33. The main purpose of spheroidising treatment is to improve [GATE-2006]

    (a) Harden ability of low carbon steel (b) Mach inability of low carbon steels

    (c) Harden ability of high carbon steels (d) Mach inability of high carbon steels

    Different tool materialsGATE-34. To get good surface finish on a turned job, one should use a sharp tool with

    a ..feed and speed of rotation of the job. [GATE-1994]

    (a) Minimum, minimum (b) Minimum, maximum

    (c) Maximum, maximum (d) Maximum, minimum

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    Previous year IES QuestionsIES-1. Chip equivalent is increased by [IES-1996]

    (a) An increases in side-cutting edge angle of tool

    (b) An increase in nose radius and side cutting edge angle of tool(c) Increasing the plant area of cut

    (d) Increasing the depth of cut.

    IES-2. Assertion (A): For drilling cast iron, the tool is provided with a point angle

    smaller than that required for a ductile material. [IES-2006]

    Reason (R): Smaller point angle results in lower rake angle.

    (a) Both A and R are individually true and R is the correct explanation of A

    (b) Both A and R are individually true but R is not the correct explanation of A

    (c) A is true but R is false

    (d) A is false but R is true

    IES--3. Which of the following is a single point cutting tool? [IES-2006]

    (a) Hacksaw blade(b) Milling cutter

    (c) Grinding wheel

    (d) Parting tool

    IES-4. Consider the following statements with respect to the relief angle of cutting tool:

    1. This affects the direction of chip flow [IES-2004]

    2. This reduces excessive friction between the tool and work piece

    3. This affects tool life

    4. This allows better access of coolant to the tool work piece interface

    Which of the statements given above are correct?

    (a) 1 and 2 (b) 2 and 3 (c) 2 and 4 (d) 3 and 4

    IES-5. Consider the following statements: [IES-2002]

    The strength of a single point cutting tool depends upon

    1. Rake angle

    2. Clearanceangle

    3. Lip angle

    Which of these statements are correct?

    (a) 1 and 3 (b) 2 and 3 (c) 1 and 2 (d) 1, 2 and 3

    IES-6. For cutting of brass with single-point cutting tool on a lathe, tool should have

    (a) Negative rake angle (b) Positive rake angle [IES-2001]

    (c) Zero rake angle (d) Zero side relief angle

    IES-7. The angle between the face and the flank of the single point cutting tool is known as

    [IES-1995]

    (a) Rake angle (b) Clearance angle (c) Lip angle (d) Point angle.

    IES-8. Single point thread cutting tool should ideally have: [IES-1995]

    (a) Zero rake (b) Positive rake (c) Negative rake (d) Normal rake.

    Designation of cutting toolIES-9. Tool geometry of a single point cutting tool is specified by the following elements:

    1. Back rake angle [IES-1994]

    2. Side rake angle3. End cutting edge angle

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    4. Side cutting edge angle

    5. Side relief angle

    6. End relief angle

    7. Nose radius

    The correct sequence of these tool elements used for correctly specifying the tool

    geometry is(a) 1,2,3,6,5,4,7 (b) 1,2,6,5,3,4,7

    (c) 1,2,5,6,3,4,7 (d) 1, 2, 6, 3, 5, 4,7

    IES-10. The following tool signature is specified for a single-point cutting tool in American

    system: [IES-2009]

    10, 12, 8, 6, 15, 20, 3

    What does the angle 12 represent?

    (a) Side cutting-edge angle

    (b) Side rake angle

    (c) Back rake angle

    (d) Side clearance angle

    IES-11. In ASA System, if the tool nomenclature is 8-6-5-5-10-15-2-mm, then the side

    rake angle will be [IES-1993]

    (a) 5 (b) 6 (c) 8 (d) 10

    IES-12. Consider the following statements with respect to the effects of a large nose radius

    on the tool: [IES-2009]

    1. It deteriorates surface finish.

    2. It increases the possibility of chatter.

    3. It improves tool life.

    Which of the above sta