IAS Mains Mechanical Engineering 1986

Embed Size (px)

Citation preview

  • 8/20/2019 IAS Mains Mechanical Engineering 1986

    1/8

    l r ~ r ~ · ; : : : : ~ : : : : : : ~ · : : : : · ; ~ . : ~ : : : : · ; \ : : : : : : ~ · : : : : : : ~ : : : : : : · · : : : : : ; ~ ; : : : : : ~ ~ : : ; : - - ; : : : : m : : : ; - - ~ - - ~ · ~ ~ ~

    u ;,•,f

    II • r f ? r n ; 1 ' i r r n 1 r • ~ r i . r • ~ r i . r • ~ r i . r • ~ r i . ~ i ~ : ~ i e . ~ ~ ~ ' r ' i i ' ~ , ~ . ~ . ~ ~ i ~ i ~ i ' i > ; ~ t i r . i • i ' i i ~ i ' i i ~ i ' : ? r r n 1 ' i r r n 1 J :1•1

    l

     l

    i{

    lt fi.AJiii R ~ I

    l

     l

    i{

    lt

    Time Allowed: 3 Hours Maximum Marks: 300

    l

     l

    i{

    INSTRUCTIONS

    ll

    l

     l

    i{

    lt

    Candidates should attempt Question 1 and 5 which re compulsory and any ftlie

    lt

    remaining question sliecting at least ONE question from each Section. 0

    lt All question carry equal marks.

    l

     l

    i{

    l

    l,i

    J

    {

    lt

    SEC11 N A

    l

     l

    i{

    l

     l

    i{

    l

    ,i

    {

    lt I Answer any three of the following:

    D

    lt

    (a) Sketch and describe any mechanism which can give ex

    ac

    erated straight-Line motion.

    lt

    Give mathematical analysis involved.

    (b) What is CORIOLIS component of c c e l e r t i o

     

    ·, e an expression for evaluating it and

    lt

    explain how

    the

    direction is fixed. '

    (c) Discuss the effect of primary, second fot s an couples in a four cylinder in-line four-

    lt

    stroke engine with mathematical an · is. m are the above engine with three-cylinder in-

    lt line engine in respect ofb alancin .

    l

     l

    i{

    lt

    (d) From first principles e r i v e   sio for the frequency of free damped vibration of a

    lt

    single degree freedom with sc dar ping.

    l

     l

    i{

    lt

    Prove that the amplitude f su 1

    ve

    oscillations are in geometric progression for

    the

    above

    I

    ~

    I

    l

     l

    i{

    lt

    2. (a) A wetght W of

    ~

    s

    lllg

    from a rope wrapped round a drum of effective

    rad1us

    of 0 3

    lt

    metre wh1ch IS

    tl

    t shaft A Shaft A IS geared

    to

    shaft B which runs

    at

    6 times the speed

    l

     l

    i{

    and

    tha

    o 1s 5 kgf-m

    2

    Fmd the acceleration of wetght

    W,

    1f 1t 1s allowed to fall

    lt

    free

    he free body diagram of shaft A The configuration of the system 1s shown m

    lt

    l

    i{

    l

     l

    i{

    l

     l

    i{

    l

    l,i

    {

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    l

     l

    i{

    ,l

    £}

    :;

  • 8/20/2019 IAS Mains Mechanical Engineering 1986

    2/8

    ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ~ ·

    3.

    4.

    (b)

    (a)

    T f ~

    I

    - .

    :::j· · ·

    .

    ·

    I ;

    ?? ·llJ

    i.J. .

    {

    1 L

    ~

    ig.

    I

    A thm c1rcular

    d1sc

    1s fitted to a shaft

    as

    shown m F1g

    o+ the disc 1s 50

    kgf

    and

    d1ametert s 120

    em,

    Shaft rotates at

    300

    r p m m antt-clo · ctton when seen from the

    nght

    s1de

    \ }

    Fmd the effect

    of

    gyro

    scop1

    c couple

    on

    the shaft and be · ng reactions at

    A

    and

    B

    takmg

    the ~ f e t o f w ; ~ ~ h t

    of h e = ~ r

    ~ f l j

    . L .

    ··- ~ L - ·

    A L ~

    -·1 . - -   ~ · ~ ::-_-_. ==-· -: ' . 111

    _

    ...:- \ ~

    r'.t. ; . · · • \ \

    I

    Ar I,..>

    1 ~ 0 < . . - - 1 5 < m

     

    h g .2

    ·

    A

    single-cylinder

     

    G t i n

    pump is driven through gearing at 50 r.p .m.

    The

    resisting

    torque

    of

    pumpe m 6 assumed to follow a sine curve

    in half

    revolution with a

    maximum value f ~  

    g -mat 90°

    and 270°. Find the weight

    of

    the flywheel required to be

    mounted

    on

    a pu

    ~

    to keep the speed within

    I

    Y

    of

    the mean speed if the radius of

    gyration o the flywn eel is

    1.5

    metre,

    The

    effect

    of

    motor armature and gear-wheels is

    equ1v t

    flyw

    heel

    of 450 kgf

    with a radius

    of

    gyration

    of

    I metre on the pump shaft .

    (b) ic

    ear tram consists

    of

    a compound gear-wheel CD which gears wtth two mtemal

    (a)

    wH Is B Gear-wheel C has

    30

    teeth meshes wtth

    mtelnal

    wheel A, while D gears

    • ' temal wheel B ha111ng 85

    teeth Internal wheel

    B IS

    keyed

    to

    a shaft L

    The

    compound

    (1)

    What

    IS

    the speed

    of

    shaft L 1f shaft

    M

    makes

    1000 rpm

    and

    all

    the wheels have the

    same p1tch?

    (u) What

    IS

    the load torque

    on

    the shaft

    Land

    holding torque

    on

    wheel

    A

    1f 1nput torque

    (i)

    (ii)

    to shaft

    M

    is

    8

    kgf-m ?

    State the theorem

    of

    Castigliano.

    Using the above theorem find the horizontal displacement along the

    load

    line

    of

    the

    frame shown

    in

    Fig. 3, considering the deflection due to bending only.

    The

    moment

    of

    inertia is the same for all sections

    ................................................................................................................................................................................................................................................................................................................................................

    .

  • 8/20/2019 IAS Mains Mechanical Engineering 1986

    3/8

    T

    a

    Fir-

    f

    1

    t

    I

    ~ l ] l

    (b) A tyre is shrook on a wheel of

    12

    metres diameter. Asswning the wheel

    to

    be ri gi

    the internal diameter of the tyre, if after shrinking, the hoop stress

    in

    the tyre is

    a for the tyre is

    11.7

    x

    0 6

    per °C and E equal

    2

    x I

    0

    8

    kgflcm

    2

    .

    Find the least

    ~

    J

    to

    which the tyre must

    be

    heated above that of he wheel before

    it

    could be o

    SECnONB

    ~

    5. Answer briefly and precisely any three of the following (Each   not exceed

    200

    words):

    a) What do you ooderstand by the term 'Cutting Tool : m f ~ ' ? Mention different single

    point tool angles and their effect on machining

    h

     

    ofmetals.

    6.

    7

    8.

    (b) What are the princi pies on which forminf l o s are based? How does hydrostatic

    extrusion differ from conventional e x t r u s i   s Mention the salient points.

    c) With reference to quality control, w h   d e r s t a n d by the following ?

    (d)

    a)

    (b)

    c)

    (i) Standard deviation l

    (ii)

    (iii)

    machining methods and mention their areas

    of

    application.

    List out the ~ { Z ; · a in Merchant's theory in orthogonal cutting and draw the force

    diagram.

    Represent rapht • some of the typical relationships between speed, feed, depth of cut

    ce   g h n e s s while twning mild steel with sintered carbides and critically

    eir relationships.

    p nventi on

    a

    and high velocity forming methods. Discuss the effect of strain and

    an1fn velocity on forming methods

    c

    U are the advantages and disadvantages of having excess inventories ? What are the

    ntory policies for

    A,

    B and C class items ?

      l l ~

    Deduce an expression for economic order quantity and clearly state the assumptions made

    in

    the derivation.

    (c) The rate of use of a particular raw material from stores is 2 0 units/year. The cost of pi acing

    and receiving an order is Rs. 40. The cost of each unit is Rs. I00. The cost of carrying

    inventory in per cent per year is 0.16 and

    it

    depends on the average stock. Determine the

    EOQ. f the lead time is 3 months, calculatethereorderpoint.

    (a)

    (b)

    Show how

    to

    formulate the general linear programming problem of optimal decision -making.

    A small plant makes two types of aircraft parts. It buys castings that are machined, bored and

    polished. The shop capacity is shown in the table given:

  • 8/20/2019 IAS Mains Mechanical Engineering 1986

    4/8

     

    Castings for Part A cost Rs. 4 each for Part B cost Rs. 9 each; they sell for Rs. 8 and Rs. 18

    respectively. The three machines have running costs o

    Rs

    40

    Rs.

    28 and

    Rs.

    35 per hour.

    Assuming that any combination o Part A and Part B can be sold what pro duct mix

    maximizes the profit ?

    Machining capacity

    Boring capacity

    Polishing capacity

    ~

    Capacities

    Part

    50

    per hour

    56 per hour

    70 per hour

    Part

    80 per hour

    70 per hour

    50 per hour

    J

    Ja·

    '(j

  • 8/20/2019 IAS Mains Mechanical Engineering 1986

    5/8

    lr, ..

    ~ : ~ - - ; , : ~ - - ~ ; : : ; : : · · ; : ; ; ~

    ......-....

    1

    -· i

    .,i

    '

    li

    li

    'iit 1:it;;;1:? r i . n ~ r i . n ~ r i . n ~ r i . n ~ ~ j ~ ~ . ~ j ~ ~ ~ ~ ~ ~ ~ ~ i ~ r . ~ ~ ~ ~ ~ ~ · ~ i i ~ : i i f < ~ r ~ ~ r i i ~ ~ i i ~ ~ i i ~ ; , 1 : i t ; ; ; 1 : ? r t . ~ ~

    II

    ~ A P : R .

    i i

    Time Allowed: Three Hours Maximum marks: 300

    INSTRUCTIONS

    Candidates should attanpt Questions 1 and 5 which are compulsory and any T  

    il i

    e

    remaining questions selecting t least ON question from each Section

    The number

    of

    marks carried by each question is indicated at the md

    of

    the ·

    I

    SEC11 NA

    J

    Am_,

    my

    •=

    of

    0011

    Eooh

    .

    of

    ..

    ~

    ' e .

    ,

    200

    ~ r o .

    ' '

    a) Explain how the poor takeoff characteristics of turb t en ·nes can be improved by thrust

    augmentation.

    2

    0)

    b) Compare the normal pressure and ,

    Us

    of recipro eating, rotary positive

    displacement) and centrifugal c o m  

    i v e

    their relative advantages.

    20)

    c) A Pitot tube in a wind s tatic pressure reading of 40.7 kgflcm

    2

    and stagnation

    pressure reading of 98 kgfl

    2

    usp ected that the device used for stagnation temperature

    d)

    measurement 1s   ~ p rature of I0 0

    •c

    1s recorded If the acoustic vel oc1ty under

    the condi tlons

    1s

    eq)

    ...

    r

    m/s

    comment on the functlorung

    of

    temperature measunng

    dev1ce {>fj (

    2

    0)

    uss n t g e s and disadvantages of gas turbmes over the reciprocating IC

    engme +

    20)

    e the pressure m the vessel1t 1s connected to an extraction pump The volume flow rate

    2

     

    d vessel of volume 0 3 m

    3

    contams perfect gas at a pressure of I kgflcm

    2

    In order to

    e gas lea111ng the vessel1s constant at 0 014 m

    3

    /mm Assummg the temperature of the gas

    to reman

    constant, calculate-

     b)

    1)

    time taken on reduce to pressure m the vessel

    to

    0 35 kgflcm

    2

    ,

    u) magmtude and sense

    of

    heat transfer between the vessel and the surroundmg dunng

    the time.

    Derive any formula you use.

    30)

    kg/s of air at 20 o•c flowing through a pipe at I 00 m/s is mixed adiabatically with I kg/s of

    air at 100°C which is following through another pipe at 50 m/s. The resulting mixture flows

    at a pressure

    of

    4 kgflcm

    2

    in a pipe

    of

    I 0 em diameter. Determine the temperature and

    velocity

    of

    the mixture.

    £

    :;

  • 8/20/2019 IAS Mains Mechanical Engineering 1986

    6/8

    3. (a)

    (b)

    4

    (a)

    (b)

    (Assume that Cp 0.27 kcallkg-K and

    R 29.2 kg-mlkg/K)

    (30)

    A boiler has a volume of I 0 m

    3

    and contains water in liquid and vapour phases at 3 0 kg/cm

    2

    pressure. Initially the liquid phase occupies half the volume. Fluid may be allowed to escape

    from the boiler by two valves one at the top of the boiler and the other at the bottom. Heat is

    transferred to the boiler at such a rate that the temperature

    of

    the fluid remains constant. Find

    the amount of heat which must be transferred if 3 0 0 kg of fluid are allowed to escap via (i)

    upper valve (ii) lower valve. It may be assumed that no liquid particles are held in s ~

    in the vapour. '

    (30)

    A multistage gas turbine is to be designed with impulse stages and is to ~ an inlet

    pressure and temperature of 6 kgflcm

    2

    and 900 K

    r e s p e c t i v e l y

     

      s s u r e

    is I

    kgflcm

    2

    and 900 K respectively. The outlet pressure is I kgflcm

    2

    . isen pte efficiency of

    the turbine is likely to

    be

    8 5 . All stages are to have a nozzle outlet

    a 15°,

    equal

    in et,

    and outlet blade angles, a mean blade speed of 250 m  equal mlet and outlet gas

    velocities. Estimate the number of stages required. Assu

    e

    ~ kcallkg-K and

    y

    Any datanot given can be assumed sui table.

    1.333.

    J

    (30)

    Calculate the power required for two m f t e : s

    ~ l

    ammonia system that serves a 3

    0-

    tonne evaporator at -2 8.9°C. The syst a illrect contact cascade condenser, and the

    condenser temperature is 37.8 •c The o

    ~ v a l u e s

    or ammonia are available:

    Pressure kgf cm

    2

    4.13

    14.00

    -28.9

    0.56

    37.8

    48.9

    87.8

    Enthalpy lccallkg

    376.9

    386.6

    150

    424.4

    (2) Saturated Ammonia

    Saturation Press

    kgf cm

    2

    1.3772

    1.27

    1.3772

    Enthalpy krallkg Entropy{Vapour)

    lccallkg-K

    h

    336

    345

    351.6

    h

    119

    43.7

    86.2

    1.3772

    1.27

    1.171

    If instead of two-stage compression a single-stage is used calculate the power required. Also

    compare the COP of one-stage and two-stage systems.

    (35)

    A room

    7m

    x

    4m

    x

    4m

    is occupied by an air-water vapour mixture at 38°C. The atmospheric

    pressure is I kgflcm

    2

    and the relative humidity is 70 Determine the humidity ratio, dew

    point, mass of air and the mass of water vapour. If the mixture of air-water vapour is further

  • 8/20/2019 IAS Mains Mechanical Engineering 1986

    7/8

    5.

    cooled at constant pressure until the temperature is

    10•c,

    find the amount

    of

    water which

    condensed.

    Assume

    R

    - - - L .

    0.622

    and R r

    29.2

    kg-mlkg-K

    R.,p,..

    (25)

    SECnON

    Answer any three

    of

    the followmg four parts (answer to each part should not exceed 200

    a) 1)

    Show that for an

    1deal

    gas wtth constant heat capacities, the slope o 

    ~ f o r

    a

    revers1ble ad1abat1c pro cess 1s negative and that

    1t

    has larger absolute v u than the

    slope

    of

    a P-V curve for an Isotherm at the same value

    of

    P ant

    (I

    0)

    b)

    (c)

    d)

    (u)

    A thermometer

    1s

    mserted m a p1p

    e

    through which

    1s

    flowtng a y stream

    of

    gas

    at

    a temperature

    T1

    and velocity

    u1.

    Will the i n d i c a t e d

     

    be higher than, lower

    than or same as T

    1

    ?

    '

    (10)

    Explam the purpose of usmg regenerative   plant. Outline a method for

    optimum heater lo catlon How does a reheat.,rv tlve cycle differ from regenerative

    1)

    Prove that system energy 1s pert)

    (I

    0)

    (u) Prove that

    ds c

    d

    T

    ~

    (I

    0)

    formation of carbon depo s1ts and smoke m gas turbine

    om u s t l ~ chamber ?

    (I 0)

    6.

    Explam the term cntlcal msulatlon th1ckness A small electnc heating apphcatlon uses

    0 183

    em

    diameter wtre wtth 0 071 em thick msulatlon The thermal conduct:1111ty of the

    insulation is 0.1

    015

    kcal/m-hour

    •c

    and surface convection beat transfer coefficient is

    29.3

    kcal./m

    2

    -hour

    •c

    Calculate the critical thickness of the insulation and the effect of employing

    critical insulation thickness. Assume that the temperature difference between the surface of

    the -wire and surrounding air remains unchanged. Derive the formula used.

    (30)

    b)

    In a long tube

    of

    outer radius r

    0

    is insulated

    at

    its outer periphery. The tube is cooled at the

    inner radius r

    1

    . Uniform heat generation

    at the

    rate

    of

    q occurs within the solid walls

    of

    the

    tube.

  • 8/20/2019 IAS Mains Mechanical Engineering 1986

    8/8

    7 a)

    b)

    c)

    8. (a)

    b)

    (i) Find a general soluti on for temperature distribution

    in

    the tub

    e

    (The maximum

    permissible temperature at the insulated

    surf cer

    r

    0

    is T

    0

      .

    (ii) Heat removal rate.

    Assumptions, if any, be stated clear

    y.

    (30)

    For flow

    of

    a liquid metal through a circular tube, the velocity and temperature profiles at a

    particular axial location may be approximated

    as

    being uniform and parabolic respectively.

    What

    is

    the value

    of

    Nusselt number at this location

    ? 2 0)

    1)

    (ii)

    v 15.36 x 10-6m

    2

    /s,

    Pr 0.709

    (30)

    Show by d1menr st s

    th t

    for turbulent flow m rough p1p

    es

    the res1stance coeffic1ent

    f

    1s

    a funct1on o y ,

    Jd

    number and the ratio

    Rfk

    where

    R

    1s

    the p1pe radius and k

    1s

    the

    average he1ght o " ughness

    proJ

    ectlons on the wall

    of

    he

    p1p

    2 0)

    Den

       

    for spec1fic speed

    of

    a turbme m terms

    of 1ts

    speed

    N,

    output power P

     

    ectnc station the avatlable head 1s 6 0 m and

    1t 1s

    anticipated that

    32

    3 m

    3

    /s

    of

    t wtll be avatl able Franc1s turbmes

    of sp ec1fic

    speed

    of

    19

    0 ate to be mstalled and are to

    0 0 r p m wtth an overall efficiency

    of

    8 2% Detemune the maxtmum power avatlabl

    m the turbmes and the number reqwred

    2 0)

    Discuss the various mechanisms

    of

    heat transfer

    th t

    take place

    when

    a red

    hot

    steel is

    quenched

    in

    a brine sol uti

    on

    at atmospheric temperature till the steel attains the temperature

    of

    he brine solution. Sketch the same on a heat flux-temperature diagram. (20)