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    FTHEPLANEMOTION

    umberof conceptsofkinematicswhich,

    andofconsiderableusefulnessinmechanism

    dfromundergraduatecurricula.

    Euler-SavaryEquation

    6,radiiofcurvatureofthe pathsofmoving

    nceinkinematicanalysisofmechanisms.

    nceinsynthesis.Theonlymethoddiscussed

    path curvatureisbasedontheknowledgeof

    ionofthepointconcerned:p=v2/anor

    arly,asfarasmechanismsareconcerned,this

    ,becausehere,asinany constrainedmotion,

    whicharea geometricalpropertyofthesystem,

    eactualvelocitiesandaccelerations.The

    inthissection,offersa direct,purelygeo-

    blem.

    dandmovingpolodes,TT/and wm,which

    mentoftheplanem;OfandOmare thecentersof

    ttheirpoint ofcontacttheinstantvelocity

    yP;pnis thepolenormal,whichoriginatesat

    7 (seealsoFig.3-22);ptis thepoletangent,the

    btainedby turningpnthrough90 intheposi-

    e,sense.

    ,definedbythe rayangle08,measured

    andthedistancePS. Inthefollowing,dis-

    atedasdirectedlineelements,i.e.,takenas

    ositivesensebeingfromP tothemovingpoint.

    ayspositive.(Theoverbarwillbeusedto

    rquantityisdirected.)Thepositivesense

    toa givenrayisobtainedby turningtheposi-

    erclockwise.0sistheinstantaneouscenter

    S.

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    ICSOFPLANEMECHANISMS

    lrotationd

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    OFTHEPLANEMOTION

    nofa length,Eq.(c)becomes

    vailable,oreasilyobtainable,detailsofthe

    positionofthevelocitypole andtheangular

    epolenormal,specifiedby theangle 0,

    engthrf,arenotknown.Theobjectiveof the

    hedeterminationofthesetwoquantities,to

    tionofEq.(10-1).

    tion(10-1)showsthatpointssuch asSi,

    scribepathswhichdifferin shapeinthevicinity

    vation.Itis thereforereasonabletoassume

    yapointI, whichpasses,atthegiveninstant,

    path.Forsuchapoint,the radiusofcurva-

    stanceOi.>P arebothinfinite.Equation

    s,therefore,to

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    ICSOFPLANEMECHANISMS

    venray therereallyexistsone,andonlyone,

    elocusof allinflectionpointsina given

    em isacircleofdiameterdf, centeredonpn

    scircleis knownastheinflectioncircle.

    ctioncircleforthe kinematicsystemof

    erivationofEq.(10-2)isinteresting.

    (cos0,)i,+(aspjn

    /,= oand(a/.)n=0,so that

    /.)wm2

    omittedbecausediisin effectadirectedlength.

    thatd,-,as definedbyEq.(3-15),isidentical

    directproofofthisfactis givenbelow.

    efirstformoftheEuler-Savaryequation

    qs.(10-1)and(10-2),thus:

    eamenabletographictreatment,itis trans-

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    OFTHEPLANEMOTION

    oftheEuler-Savaryequation.Since(P>

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    CSOFPLANEMECHANISMS

    onnectI,with Y(line|),and YwithP

    lineparalleltoline |,intersectingtheauxil-

    awaline paralleltoline||,and obtainOsat

    withtherays.

    structionis provedbyconsideringtwosets

    angles SI,YandSPZ,

    e trianglesSOSZandSPY,

    meconstructionfora differentrelativedis-

    and/,.

    icalDeterminationofd,-

    centerofcurvature0sof itspathforma

    tdiand thedirectionofpncan bedetermined

    pointsandthecorrespondingray angleare

    onjugatepoints,ondifferentrays,arespecified.

    mpleofthis caseisillustratedin Fig.10-6.

    intsOm andOfforwhichthe rayangleiszero.

    ureofthepath ofOm.SeeSec.3-13.)

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    FTHEPLANEMOTION

    (10-1),....

    > Om= /5m,thisrelationbecomes

    hetwopolodesareconvex,andtheminusif one

    therconcave.Theresultis thusidenticalwith

    aphicalsolution,showninFig.10-6,

    constructionofFig.10-5in reverseorder.

    airsof conjugatepoints,QandOQonrayq

    givenincludedray angle6q,=0, 08

    (10-1),

    edfor0,, andd,-isthenfoundby Eq.(10-1),

    oblemmaybesolvedgraphicallyby

    einflectionpoints/,andI,,usingthe con-

    erseorder, andthenerectingnormalsthrough

    verays.Thetwo normalsintersectat/,the

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    AMICSOFPLANEMECHANISMS

    atively,theproblemmaybesolved by

    escribednext.

    ion;CollineationAxis

    fersfromthereverseconstructionofFig.10-5

    neandpointZare nolongerarbitrary.Here

    swiththeline throughthemovingpointsQand

    ttheintersectionofQSwithOQ()S.Becauseof

    noflineandpoint,the twoinflectionpointsIq

    neously.

    icationofBobillier'smethodtothe con-

    ircleforthecoupler3 ofafour-barmechanism

    struction.(QBoA)-Z-P18-Y-(/t,

    atZcoincideswiththe instantaneous

    ofthedrivinganddrivenlinks.

    PZinBobillier'sconstructionisknownas

    raysq ands.Thus,ina four-barmechanism,

    ativeinstantcentersPisand P24ofthephysi-

    ollineationaxisof drivinganddrivenlinks;it is

    ineationaxisofthemechanism.

    heoremstatesthattheanglebetweenthe

    equaltotheanglebetweentheother rayand

    tworays, bothanglesbeingmeasuredinthe

    ssofthetheoremin analysisandsynthesiswill

    ischapter.

    oremmaybeverifiedwiththe aidofFig.10-7.

    cle

    sP:*

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    OFTHEPLANEMOTION225

    uareparallel.Similarly,

    ction

    erminingtheinflectioncircleis somewhat

    onthe displacementvelocityoftheinstant

    outdifficulty inthemostcomplexsituations.

    gularspeedofthe planem,andvpthespeed

    erof rotationchangesitspositionalongthe

    stantaneouspoletangent.Vp istherefore

    locityoftheinstant center.Asshownpre-

    the positivepolenormal.Consequently,the

    poletangentisobtainedbyturningdi aboutP

    ofcom.Conversely,withVPknown,thedirection

    ormal,isobtainedby rotatingVPthrough90

    ethod,anarbitrarilyassumedvalueis

    ocitywm,andthe correspondingdisplace-

    tcenter isdeterminedgraphically,withthe

    n general,theabsoluteinstantcenterP

    oncircle istobe determinedisdefinedbythe

    rays.Theauxiliarylinkageconsists,there-

    tedto theframeatappropriatepoints,and

    blockswhicharefreeto slidealongtheselinks,

    butarepin-connectedtogetheratP. Thus

    nectionP,intheauxiliarylinkage,is identical

    placementvelocity.

    theauxiliarylinkageshavebeendrawn

    eexplanations.Inpractice,however,the

    uton theoriginalplan,aprocedurewhich

    ccuracy.

    nstructtheinflectioncirclefor amoving

    ne pairofconjugatepoints(S and0s),and

    ormalarespecified.

    emisshownin Fig.10-8o,andtheauxiliary

    tterconsists ofthebars, pivotedtothe

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    ICSOFPLANEMECHANISMS

    sq andr,pin-connectedtogetheratP,with

    ngentptandr freetoslidealongs. Thepoint

    denotedbyX,.

    correspondingtothe arbitrarilyassumed

    sec,ccw,isthe requiredpole-displacement

    yofthelinkageisvs =umX(P> S).

    y proportion,andthevelocityofPfollows

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    FTHEPLANEMOTION

    nstructionfortheparticularcaseofspecified

    hpolodes.

    nstructtheinflectioncircleforthecoupler3

    mofFig.10-9a.(Twosetsof conjugatepoints

    and 04.)

    ed)

    wstheauxiliarylinkage.Itconsistsof the

    tedtotheframeatOzand04,respectively,and

    nnectedtogetheratP, withblock5freetoslide

    oslide onbar4.Thepoints onbars2and 4,

    oted,respectively,byX2andXt.

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    ICSOFPLANEMECHANISMS

    =w3 X(Pis>A)and VB=waX(Pis> 5);

    ally,byproportion,andVP followsfrom

    nstructtheinflectioncircleforlink3 ofthe

    10a).(Thenameofthemechanismderives

    t onlink3describesa conchoidalpath.)

    ageconsistsoftheextendedslider2, the

    e frameat04,andthetwo blocks5and6,

    tP,ofwhichblock5isfree toslidealonglink 4,

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    FTHEPLANEMOTION229

    Thecoincidentpointsareagaindenotedby

    celinks3 and4forma slidingpair,t>4=u3.

    04>Xi).Sincelink2 isinrectilinear

    (P13-* 4).vpfollowsfrom

    nstructtheinflectioncircleforthebar3 of

    ig.10-1la.The mechanismconsistsofthe

    othecrankat A,andthestationarysurface1

    bar3.

    ageisshowninFig. 10-116.Itselements

    eframeat02, thebar4,pivotedto theframe

    cideswiththecenterofcurvatureMofthe

    blocks5 and6,pin-connectedtogetheratP,of

    dealongbar2,and block6alongbar4. The

    eX2(on 2)andX4(on 4).Sincetheaux-

    diculartothe link3duringan elemental

    dconsequently,vx,=u3X(04* Xi).Also,

    followsfrom

    nstructtheinflectioncirclefortheternary

    howninFig.10-12a.

    mplexproblem,andcanonlybesolvedin

    shownin Fig.10-126,involvesthedetermina-

    ementvelocityofthecenterP2t,which,to

    notedbyR.Theauxiliarylinkagefor this

    ntricallypivotedbars3and4 andtheblocks7

    heframeat 03=P13,andbar 4atOi= P14.

    tedtogetheratR,withblock7free toslideon

    .The pointsonbars3and 4,coincidentwith

    ely,byX3andXi.Theinput velocitiesare

    d= ujX(P1t>D). vRfollowsfrom

    nstruction,showninFig.10-12c,is con-

    tionofthedisplacementvelocityofP1t.The

    ageconsistsof thebar10,pivotedtothe

    ssingthroughR,thebar6, pivotedtotheframe

    nd12,pin-connectedtogetheratP=P15,

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    AMICSOFPLANEMECHANISMS

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    FTHEPLANEMOTION

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    ICSOFPLANEMECHANISMS

    onbar10and block12onbar6. Thepoint

    R,is denotedbyXi0>andthepointson

    withP,areshownasYIOandy6, respectively.

    = w5X(Pi6>E)andvXl,=componentof^v

    sfrom

    fortheRelativeMotionofTwo MovingPlanes

    teredaroundtheconstructionofthe inflec-

    theabsolutemotionofa plane.Occasionally

    ethecurvaturesofpathstracedby thepoints

    otherplane,also inmotion.Theinflection

    elativemotionoftwoplanesis constructed

    kinematicinversioninwhichtheparticular

    herespectivepolenormal

    tionary,andotherwisefollowingtheprocedure

    section.Itshouldbe notedthat,asshownin

    oncirclesinvolved(motionofmrelativeto /,

    m)arepolarimagesofeachother, afactwhich

    structtheinflectioncircleassociatedwith

    3 relativetothecam2 inFig.10-14.

    owstheauxiliarylinkagefortheinversionin

    onary.Thelinkageis basicallythesameasthe

    eExample4of theprevioussectionandshown

    ocitiesfor theinversionare

    Xt).VPfollowsfrom

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    FTHEPLANEMOTION

    ectionCircletoKinematicAnalysis

    providesthemeansfora purelygeometrical

    vatures,itbecomespossibletoanalyzecomplex

    oursetotheindirectanalyticalandgraphical

    re10-15ashowstheskeletonofacertain

    echanismwhoseinputcrank2revolvesatcon-

    theangularaccelerationoflink4 andthe

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    ICSOFPLANEMECHANISMS

    t,as shown,thesolutionbymeansof

    atherdifficult,andtheproblemisbest solved

    oncircle.AfterthepathcurvatureofBhas

    raphicallyorbycomputation

    mentary.

    nin Fig.10-16a,theproblemmaybesolved

    nflectioncircleorbythesubstitutionof the

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    FTHEPLANEMOTION

    entmechanism

    ntlow-complexitymechanismofFig.10-166.

    chlesscumbersome.

    eneralCase)

    which,byrolling ononeanother,reproduce

    thecharacteristicsoftheconstraints.The

    s investigatedinthefollowingsections.

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    ICSOFPLANEMECHANISMS

    definedbyQS,isconstrainedtomovein a

    fthefact thatthecentersofcurvatureOQ

    diS, respectively,aremadetotraversethe

    The locusofthecenterofcurvatureofa given

    ute.)

    thefixedpolodeis ageometricalproperty

    terminedhereindirectly,i.e.,byconsidering

    eristicsofthevelocitypole:

    speedofvelocitypole

    tofitsdisplacementacceleration(nottobe

    onofpointPm,aPm=wm2d,-)

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    OFTHEPLANEMOTION237

    ),a.pwillbecomputedwiththe aidofthe

    twasusedin determiningVpbyHartmann's

    uations

    dwm,which,tosimplifythe calculations,will

    ce,inthefollowing,du/dr= 0.

    othepositiveand negativesensealonga

    glestoit,werelaid downinSec.10-1.Since,

    he basisofthesubsequentderivations,all

    positive,thediacritical overbarwillbeomitted

    ereintroducedinthe finalexpressions.

    pendicularto0s >S=ps,consists oftwo

    omponentof&x,andthe Corioliscomponent

    x.)c0r(b)

    das follows:

    Oa->X.)-(c)

    =vg;and

    x.

    >X,)rsdps+ Os>X,dri]

    .(d) maybeexpressedintermsof thegiven

    manner:

    ointsontherays,

    s ->-S')>(Os-* S).]FromFig.10-16,

    6, {&)

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    AMICSOFPLANEMECHANISMS

    -> S') S).]With

    rs

    = P-> S= rs

    (/) into(d)yields

    sin0,

    px.)cariscalculatedasfollows:

    ^mvpsinS,=Wm2d,- -sin68(h)

    nowbe substitutedinto(6),giving

    0.(i)

    =UmWiKo(j)

    6q.7.

    . (Z)

    to

    h(m)yieldsthe finalresult

    ndX's aredefinedbyEqs.(i) and(j).

    f thefixedpolode,asdeterminedby

    ornegative.A positiveresultshowsthat

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    OFTHEPLANEMOTION239

    irectionofthepositivepole normal,which

    ectioncircleareonoppositesides ofthepole

    pecialCase);Hall'sEquation

    ssionforthe polodecurvatureinthemost

    wthespecialcasewherethe pathcurvaturesof

    edinthefollowingbyY andZ,haveinstan-

    es;thatis,dpy/dl dpz/dl=0.It isobvious

    ythiscondition,theevoluteserand ezmust

    ndinginstant;that is,pfr=pfl =0.

    herefore,to

    f r" ~PYcos0, sin6y

    thersimplified,and

    asfirstreportedin theliteraturebyA.S. Hall.1

    ationarypathcurvatures,thepolodecurva-

    din termsofaratio (R(whosephysicalsignifi-

    nSec.10-10)andits derivatives,inthefollowing

    > Y)

    Ydt,

    , tan6a

    P)dr, tan^

    cle andPolodeCurvature,Trans.FifthCon/,on

    58,pp.207-231,PurdueUniversity,Lafayette,Ind.

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    AMICSOFPLANEMECHANISMS

    rItan6y=((R - (R2)taney

    an0,

    + (P ->F)=(0r->P)

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    OFTHEPLANEMOTION

    ssedin termsoftan6y,andthe latterin

    Eq.(q),thenthefollowingexpressionresults:

    beobtainedby substituting

    essestheradius ofcurvatureinpolar

    heFour-barMechanism;CouplerMotion

    ththemotionofthe coupler3relativetothe

    m =7r3.Itis obviousfromFig.10-19athat

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    ICSOFPLANEMECHANISMS

    ddirectlyfor thecomputationofthecurvature

    rminethepolodecurvaturesforthecoupler

    mofFig.10-20.

    3in.,04-> B=-2.3in.,P ->A=1.7in.,

    oncircleyieldsthefollowingparticulars:

    =346 =-14.Hence,byEq.(10-11),

    n iscalculatedbyEq.(10-5),withm =3

    of P13,withthecentersofcurvaturedenoted

    y,areshowninFig. 10-20.

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    FTHEPLANEMOTION243

    ntheFour-barMechanism;RelativeMotionof

    DeterminationoftheOutputAngular

    f Change

    6revealsthat Hall'sequation,withappro-

    ,maybeusedtodeterminethecurvatureof the

    ththemotionofthe outputlink4relativeto the

    13)

    ncethediscussionis concernedwiththemotion

    hepositivesensealong bars1and3 isthe

    orrespondingpointsonlink 4,i.e.,fromPto

    tively.

    ablyalterednotation,isalso applicablein

    gs.10-18and10-19&showsthat dtp2=dy

    0randOtto Y.Hence

    W2

    erelativemotionof theoutputandinput

    ocityratioof themechanism.((Rmaybe

    ((R')2+(R(R'

    =

    fiednotation,yields

    0i

    rvelocityo>2,from Eq.(10-14)

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    AMICSOFPLANEMECHANISMS

    &i=2(10-17)

    )

    epositionofthe relativeinstantcenterP-u

    ityratio(Rofthe mechanism.

    at,inamechanismwitha uniformlyrotating

    e angle61betweenthepolenormalandthe

    heoutputangularacceleration.

    qs.(10-15)and(10-18)yieldsan expres-

    etodeterminethe timerateofchangeofthe

    on.

    maybeusedinthe analysisofagivenmecha-

    onisinthe fieldofsynthesis,particularlyin

    rivingcrank2ofthe four-barmechanism

    constantspeedofu2=2 rad/sec,ccw.Deter-

    ,and4.

    hepoletangent(and consequentlyofthe

    dbyBobillier'stheorem,i.e.,bymakingthe

    dthepoletangentequalthe angleformedbythe

    Bymeasurement,

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    OFTHEPLANEMOTION245

    oncircle maybedeterminedgraphicallyor

    ler-Savaryequationintheform

    S)- (Os-> 5)[(P -> 5)-d, cos0. ]

    ->04)[(P24->04)- d.cosO1]

    n.

    9 in.

    nd w4=0.78rad/sec

    rad/sec2

    ),p2= 10.12in.

    enterofcurvature0r2of t2liesonthe sideof

    othe inflectioncircle.)ByEq.(10-5),with

    0.39and(R'=0.92,

    ineation-axisTheorem;1Carter-HallCircle2

    ropertyonwhich Bobillier'stheoremis

    spossessesanumberofother characteristics

    ismdesign.

    Inafour-barmechanism,inthephasescor-

    valuesofthevelocity ratio,thecollineation

    coupler.(Inthesephases,ifw2 =const,

    atesthat(R'=((R2 (R)tan0i.Hence,

    ,andconsequently(R'=0, 0i=0also. Thus,

    d,thepolenormalcoincides withthefixed

    aximumandMinimumVelocitiesand theAccelerations

    Trans.ASME,vol.78,no.4,pp.779-787,1956.

    alysisandSynthesisUsingCollineation-axisEqua-

    ,no.6,pp. 1305-1312,1957,withdiscussionbyA.S.

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    ICSOFPLANEMECHANISMS

    erpendiculartothefixedlink,andbyBobillier's

    axisisperpendiculartothecoupler.

    rkinematicpropertywhichmaybe

    naxisisthe following.Ifafamilyoffour-bar

    edonthesamefixedbaseline02 >04,whose

    nstantaneousvelocityratio(R,thesamefirst

    ,andthesamesecondderivative(R"=d2&./d

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    FTHEPLANEMOTION247

    n,appliedtolink1,yields

    24-> 00-tU cos0,]

    * sint?J

    >04)+disint?i, .

    (c)

    forlink3,

    n

    (d) into(6)andrearrangementoftermsyields

    ?icos#3sin i?3sin(?3 t?i)

    ------------------

    -

    (2- - -1+3d, -si

    f Eq.(e)issubstitutedfor P24 >BinEq. (a),

    dto

    -cos#3(J)

    r--- -

    d,

    24)+(P24 ->04)

    00

    mbinedyield

    nd(A),Eq.(/) istransformedto

    C

    R

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    AMICSOFPLANEMECHANISMS

    6)showthatmechanismswhichhavethesame

    ,Si',and(R"have,ipso facto,thesameinflection

    ecurvature.Hence,forsuchafamilyof

    0-20)

    lar coordinates,ofacirclehavingthechar-

    enEqs.(10-15)and(10-19),then,aftersome

    raicoperations,thefollowingexpressionis

    toquantitiesdirectlydeterminableby

    hemechanismofFigs.10-21and10-22,

    9,0i=104.5,anddc= 5.6in.

    21)yields(R"= 0.72,whichagreeswiththe

    ativeexampleof Sec.10-10.

    Curve(GeneralCase)

    sedinthischapteris thecircling-pointcurve,

    ature,thelocusofall thosepointsonamoving

    stantconsidered,havestationarycurvature.

    ancein synthesis,andparticularlyinthe

    nismswithprolongeddwellrequirementsfor

    ecircling-pointcurve,andapplytheEuler-

    os0, ]=(P->F )2

    nsOY >Y=pyandP >Y=fy,becomes

    )

    arindicatingdirectedline elementswillbe

    s,butreintroducedinthefinal expression.)

    stobe instantaneouslystationary,then

    cementofthepoleP.

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    FTHEPLANEMOTION249

    elds,therefore,

    w \ = 2ry it(6)

    pm=vP/um,wasderivedinSec.10-1.)

    sions(c)and (g)into(b)leadsto

    d, - sin0f - r) = 2rysin0(A)

    etweenEqs.(h)and(a) yieldstheequationof

    olar coordinates,withthevariablesfyand0:

    ntsinthephaseconsidered.

    eevaluationofEq.(10-22),itis necessary

    eousrateofgrowthof thediameterofthe

    ase ofthemovingbody;thatis,d(d,)/dl.The

    sibleif,asshowninFig.10-17,the pathcurva-

    are given.

    ,relevanttothepresentinvestigation,were

    he assumptionum=const:

    ponentofthepole-displacementacceleration:

    , . .

    W

    npole-displacementaccelerationandpole-

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    ICSOFPLANEMECHANISMS

    Eqs.(t)and (j)ofSec.10-7.

    sconstant,

    fthelastthreeequationsyields

    10-23,thecircling-pointcurveisa looped

    ranchescrossatrightanglesat theinstant

    oinfinityin anasymptoticalapproachtoaline

    iththe polenormal.0Misobtainedby

    minatorinEq. (10-22):

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    FTHEPLANEMOTION251

    notpassthroughthe instantcenter.Itsoffset

    6g=6m. However,ifthenumeratorand

    iatedseparatelywithrespectto#v,thelimiting

    0-25)

    egeneratesintoacircleandastraightl ine

    mevalue.ByEq.(10-22),if d(di)/dl=0,

    )reducesto

    0 =equationofacircleof diameter2/M,

    ndpassingthrough

    straightli necoincident

    CurvefortheCouplerofa Four-barMechanism

    hetwocouplerhingesare obviouslypoints

    .Hence,iftheirpolarcoordinatesaresub-

    woindependentequationsareobtained,from

    TVcanbe calculated.WithMandTVknown,

    easilyconstructed.

    wthecircling-pointcurveforthecouplerof

    fFig.10-24.

    hepoletangentand polenormalarefound

    dthepolarcoordinatesofA andBaredeter-

    substitutedintoEq. (10-22),yield

    60

    tsonthecurveare locatedasshownindetail

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    AMICSOFPLANEMECHANISMS

    gle6C =125.ByEq.(10-22),

    0cos125'

    ythedegreetowhichthe actualpathofa

    curvemaybeapproximated,inthevicinityof

    heosculationcircle.ForthepointC, thetwo

    nguishablefromoneanotherforabout70 of

    ce,iftwolinks5and6 wereaddedtothe

    outputlink6wouldremainsensiblyat restdur-

    etweenlinks5 and6whichcoincideswith,

    hepath ofCmaybefoundeither graphically,

    ectioncircle,orbycalculation,asfollows:

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    FTHEPLANEMOTION253

    n,appliedtoA,yieldsthediameterofthe

    A)=(0, ->A)[(PU->A)-di cos.]

    n,appliednexttopointC,yieldsthe required

    >O -dicostfj

    .

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    ESIS;

    thedesigner'sworkis thedevelopment,or

    sfortheperformanceofspecifiedoperations.

    ntivenessandintuitionplayamajorpart in

    arecertainfundamentalproblemsofsynthesis

    ationalway.Suchproblemsinclude:

    numberofprescribedpositions

    tionsofthe outputandinputlinks,i.e.,

    prescribedpath,i.e.,pathgeneration

    nstantaneousmotioncharacteristics

    numberofmethods,bothgraphicaland

    oftheseproblems.Theaccentwillbe onthe

    useitisthemoredirectof thetwoandyields

    uracy,withmuchlesseffort.

    utionwill bebasedonthefour-barmecha-

    gationofthecharacteristicpropertiesofthis

    prisinglyversatile,linkageiscalledfor.

    e

    nthe followingdiscussionarelistedbelow

    therotocenters,aredefinedbyFig. 11-1.

    r

    ardisplacementofqbetweenphasesmandn

    isplacementofsbetweenphasemandn

    splacementofrbetweenphasesmand n

    ebetweenrands

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    ESIS;GRAPHICALMETHODS

    withrespectto theframe,definingthe

    mtophasen

    ningtherelativedisplacementoflinksq

    nd n

    ducedanddefinedasrequired.

    ism.Figure11-2showsthethreetypesof

    rank-rockermechanism.Therotationofq

    ,whilescanonlyoscillatethroughalimited

    thattheforwardandreturnstrokesof sdonot

    onsofq.

    uble-crank,ordrag-link,mechanism.The

    reunrestricted.Auniformrotationofq

    tationofs.

    ble-rockermechanism,qandscanonly

    nedas inversionsofthesamelinkage,pro-

    thsoftheshortestandlongest linksislessthan

    shof'srule):

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    ICSOFPLANEMECHANISMS

    rankcrank-rockermechanism

    amedrag-linkmechanism

    ouplerdouble-rockermechanism

    anism,derivedfromGrashof'slinkage,the

    eterevolutionwhiletherockersmovethrough

    arlinkagedoesnotsatisfyGrashof'scriterion,

    gementoflinksis used,onlydouble-rocker

    ngcouplersresult.

    riencehasshownthatmechanismswith

    helimitsofGrashof'srulearenot satisfactory

    ioncycle,linksassumerelativepositions

    centerpositions),withconsequentchatterand

    es.Moreover,sincesuchlinkagesrequirethe

    emachiningtolerances,ifundesirableeffectson

    cteristicsaretobeavoided,theyaremore

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    ESIS;GRAPHICALMETHODS

    nlinkageswithamoresubstantialinequality

    he designstage,totheeventualperformance

    smissionanglen oritssupplementn'.Alt,1

    eof thisparameterasaqualityindex forthe

    commendedaminimumvalueof40 forlow-

    eedapplications.Otherkinematicianshave

    owever,itisextremelydoubtfulwhethersuch

    accepteduncritically.Clearly,inlow-speed

    ansferwillbe"best"if n=90 andimpossible

    gswinkelundseineBedeutungfuerdasKonstruieren

    erkslattstechnik,vol.26,no.4,p. 61,1932.

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    ICSOFPLANEMECHANISMS

    bviousthatthe effectofinertiaforcesin

    annotbeaccountedforbyasimplegeometrical

    ggestedbyAlt maybeusedsafelyasa

    theinitialdesignina givensituation.A

    sclosethesuitabilityorsatisfactorinessofthe

    tline)

    nd,forinstance,thatthe inertiaeffects

    reductionofn,whichmaybe quitedesirable

    achesits extremevaluesinamotioncycle

    ollinearwiththefixedlink p.Thecorre-

    tedby1and 3.Akinematicallyoptimum

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    ESIS;GRAPHICALMETHODS

    issionangles,isonein which^min=^Vn.The

    for prescribedvaluesofMminand^13isshowni n

    ,thedrivenlink,ofarbitraryl ength

    sesSiand s3,andthelinesTI andr3aredrawn

    ns,determinedbythespecifiedtransmission

    gthsrx=BiAix=B$A3Xarethen trieduntil

    tainedwhichpassesthroughO,.Therequired

    themidpointofA3Ai.Inthe alternative

    -46,abundleofrays isdrawnthroughO,,

    A* andliner3in pointsA*.Thesolution

    ointsA* =AiandA$= A3,forwhich

    mplishedbyplottingthelengthsBiAfversus

    sBtA*.Theintersectionofthelocusobtained

    nedrawnthroughB3at45 totherayr3, clearly

    nismasQuick-returnMotion.1Figure11-5

    chanisminthetwoextremepositionsofthe

    rvedthatthecrankangle

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    ICSOFPLANEMECHANISMS

    hesisofa crank-rockermechanismfora

    rnaction,i.e.,forprescribedvaluesof

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    ESIS)GRAPHICALMETHODS261

    s. Since,byEq.(6),OqB2 OqBt=2q,

    ectionofthepivotcirclewithahyperbolaof

    2andBi(Fig.11-66).

    . Since,byEq.(a),OqB2+OqBt=2r,

    ectionofthepivotcirclewithanellipse ofmajor

    BA(Fig.11-6c).

    positionfa.Oq islocatedattheintersection

    hercircle,of radiusMOwhosecenterMis

    ctorofO,B2sothat thecentralangle

    snotcompletelyfree;an inspectionof

    g.1l-6arevealsimmediatelythat:

    nsidepivotcircleandfa< (90 -^J

    outsidepivot circleandfa>(90 -^J

    #24 180 canberealizedbymeansofa

    ftheinitialcrankpositionfa =90 ^24/2.

    pivotcirclepassesthroughOandanyother

    ationforthepivot Oq.Since,inthiscase,the

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    ICSOFPLANEMECHANISMS

    nsisinfinite,additionaldesignrequirements

    sconditions1to 4above.

    180 and

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    ESIS;GRAPHICALMETHODS

    edinmanyways,e.g.,byattachingratAand

    xedpivotsOqandO, maybelocatedany-

    tors[n^]i2and[na]u ofAiAzandBiB2,respec-

    four-barlinkagesisevidentlyinfinite.

    alsobe broughtaboutbyasimplerotation

    oint ofintersectionof[nA]uand[ns]i2.This

    he rotocenterofthebody,orplane,r forthe

    -r2.Inthefollowing,sincethereisno possi-

    xrwill bedropped,andtherotocenterwill

    AninspectionofFig. 11-9revealsthat,as

    2R^B2arecongruent,theamountofrotation

    tualangulardisplacement[tpr]uofthebody.

    propertiescanalsobededucedbyinspection:

    theguidinglinks (cranksorrockers)qands

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    AMICSOFPLANEMECHANISMS

    s,capableofguidingtheircouplerr through

    ndequalanglesatthe rotocenter[Rr]u=R^;

    sareequaltohalfthe angulardisplacementofr:

    ,andeffectivelengths(betweenhinges)of

    mechanismsalsosubtendequalanglesatRi2:

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    ESIS;GRAPHICALMETHODS

    cablemechanismsisinfinite,itis possible

    mutuallycompatible,requirementstobesatis-

    n.Examplesofsuchadditionalcriteria,the

    hisfour,arethefollowing:

    hefixedpivotsOq andO,androtationsof

    s, [

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    ICSOFPLANEMECHANISMS

    underconsideration,pointsOqand D

    ivotsof afour-barmechanismwhosecoupler

    therequiredpointC,respectively.The

    plerislocatedat theintersectionofthenormal

    12.Thepositionof Ciisobtainedbymaking

    uidinglinkssubtendequalangles atthe

    dm,wereattachedtotheslider-crank

    shedlines,adwellmechanismwouldresult,

    hitlinkm,wouldremainvirtually atrest

    dfromAIthroughA2 andA3toAt.

    ghThreeDistinctPositions

    uidingabodyr, definedbythelinesegment

    dpositionswouldbebymeansof twolinks,

    to theframeatthecentersof circlesdrawn,

    A2,A3andBi,B2,B3.

    erthanAandB maybeusedequallywell

    beroffour-barmechanismscapableofguiding

    ribeddistinctphasesbecomesinfinite.This

    nofadditionalrestrictionsonthe design.

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    ESIS;GRAPHICALMETHODS267

    ationsofOq andO,arespecifiedinadditionto

    ecorrespondingmovinghingesCandD is

    kinematicinversioninwhichthebodyitselfis

    e threephases,forinstance,AiBi,andthe

    erelativepositionsofO,andO3are determined

    2B2Og,A2B2O,andA3B3Oq,A3B3O,tothe

    =A42B20,,etc.)

    hemovinghingesin phase1arethen

    e circlesdrawn,respectively,throughOq,011,

    ngle

    m =ABinthreedistinctphasesand the

    RU,RM,andRu.

    therotocentertriangleyieldsanumberof

    orems.

    terTriangle.InFig.11-136,the bodyhas

    ethepointsCand D,judiciouslyplacedsothat,

    cideswithR^and,inpositions 1and2,D

    eextendedlineRuRi3coincideswith[nc]i2

    edlineRuR^coincideswith[nc]isand [rio^s,

    attheanglesof therotocentertriangleare

    dingbodyrotations.

    eterminationoftherotationalsense,the

    mmended:

    montobothrotocenters

    mmontobothrotocenters

    montobothrotocenters

    maybetransferredfromposition1to posi-

    rclockwiserotation

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    ICSOFPLANEMECHANISMS

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    HESIS;GRAPHICALMETHODS

    gle,for example,AIaboutside1,yieldingthe

    ctionsof Acabouttheother twosidesof

    d correlatedpositions.Thecorrectnessof

    elf-evident:

    sefulinitself,

    mportanttheorem.

    the Heights.Thecorrelatedpositionsof

    alpointHccoincideswith theorthocenter(the

    ofthe rotocentertriangle,arelocatedonthe

    edasfollows.

    R^XR^,inFig.11-15,

    ngleH2R^

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    AMICSOFPLANEMECHANISMS

    rtoR^R^andRitRnis perpendiculartoXR23,

    rtoRuR andR^Ruisperpendiculartofli2Z,

    ngle

    ngleRuZH3,

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    ESIS;GRAPHICALMETHODS

    ntRuH^subtendsequalanglesp, atH2,

    hat allsixpointslie ononeandthesamecircle.

    nthis respectmaybeseenfromFig.11-156.

    nts PcwhosecorrelatedpositionPIison

    theimagecircle1,i.e.,the reflectionofthe

    tside1.Similarly,imagecircle2isthe locus

    latedphasePz liesonthecircumscribedcircle,

    ocusofallcardinalpoints Pcwhosecorrelated

    e circumscribedcircle.However,thethree

    epointin common,viz.,theorthocenterHc.

    sofaPointin aStraightLine.Ifthree

    ointarecollinear,theyare alsolocatedonthe

    es,andthelinecontainingthempassesthrough

    ollinearcorrelatedpositionsofthepoint A

    ocentertriangle.Hcislocatedatthe inter-

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    AMICSOFPLANEMECHANISMS

    siderationoftheanglesaroundthe vertexAi

    ndiculartoR^RnandRiJIeis perpendicular

    sequalanglesatAiand Hc,itfollowsthat

    sRi2,Ru,andHc,that is,imagecircle1.

    armannerthatA2 liesonimagecircle2,and

    at,asindicatedbytheconstruction,Hc

    .

    >u+o-=360

    ^23

    7=180

    onthesamecircle,R^Aisubtendsequal

    equently,

    ,andA3 lieononecircle,

    sofaLinethrougha Point.Ifthethree

    ectatagivenstationarypointS, thenli,l2,

    ,throughHI,H2,andH3,and Sislocatedonthe

    ntertriangle.

    tions ofZ,dennedbythecorrelatedposi-

    niquelydeterminetherotocentertriangle.

    sectionofthenormalbisectors[n^]i2and

    eenomittedsoasnotto clutterupthedrawing

    onlines.)

    sect,respectively,theangleliSls=

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    HESIS;GRAPHICALMETHODS273

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    AMICSOFPLANEMECHANISMS

    nsequently,

    rto6i sandR^Sis perpendicularto623,

    thesamecircleasRu,Ru,and#23.

    slythatHI, H2,andH3arecorrelatedposi-

    hereforethe directionsHiS,HzS,andH3S

    nsofaline. Thatthesedirectionsareidentical

    tively,followsfromthefactthat,asshownin

    rtriangleandagivenpoint Sonthecircum-

    thecorrelatedlinepositions.[Theconstruc-

    dproceedasfollows.Therotocentertriangle

    enseofthe rotation^13.SincetherayRi3S

    ions1and3,lines Ziandl3are inclinedtoitat

    dN3 arecorrelatedpositionsofthepointN.

    ngthe angleZi

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    le

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    ESIS;GRAPHICALMETHODS277

    ditscircumcircleareconstructedinthe

    of thecorrelatedpositionsofAandof asuit-

    coupler.TheorthocenterHcislocatedatthe

    s,anditsposition checkedbymeansofthe

    2,andH3are located,respectively,atthe

    mcirclewiththeextendedaltitudesHM^,HcRu,

    din aconvenientpositiononthecircum-

    einphase1 ismadeparalleltoHiM. (An

    curacyoftheworkingistheconditionthatO,,

    ionof thethreecorrelatedpositionsofthe

    cumcircleandthattheextendedlinesAiBi,

    passthroughHi, HI,andH3,respectively.)

    ghFourDistinctPositions;Burmester'sCurve

    ody,or plane,throughfourdistinctposi-

    agesisrathercomplex.Itssolutionentailsthe

    ne,ofpointswhosefour correlatedpositions

    oints(of whichthereisaninfinitenumber)

    inghinges,andthecentersofthecorresponding

    ocusofthe fixedcentersisknownasBur-

    ter-pointcurve.

    r'sCurve.1Figure11-20showsabodyr,

    ctpositions,togetherwith thesixassociated

    RM,Rzt,andRat,whicharelocatedatthe

    entifiednormalbisectors[HA]and[UB\.(The

    andR-uhavenot beenshownbecausethey

    bsequentdiscussion.)

    cognitionofthegeometricalrelations,point

    vein acircularpath.Thusallnormal

    hthepointOA.Theradius 0^Amovesfrom

    oughanangle5i2;fromposition2 toposition3

    tion3 toposition4through534.Hence,

    eangleincludedby thebisectors[n^]i4and

    gasami,GraphicalLinkageAnalysis,MachineDesign,

    1953.

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    ICSOFPLANEMECHANISMS

    bythebisectors[uaJuand[nA]23,

    ces#14^34andR12Rnsubtendequalangles

    hown,ina similarmanner,thatotherpairs

    osubtendequal(or supplementary)anglesat

    le11-1.

    eanalysisis that,ifapoint Omistoserve

    ntainingfourcorrelatedpositionsof some

    thecommonvertexoftwotriangleswhich

    ndhavecorrespondingrotocenterdistances

    ructionshownin Fig.11-21yieldstwopoints

    eseconditions.Theradiiofthe twocircles

    maybe determinedeithergraphicallyor,alter-

    lideruleto theratioofthe basedistances

    dingvalues.Arepetitionof theconstruction

    s (andconsequentlydifferentapexanglese)

    Thecurvepassesthroughthesix rotocenters

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    ESIS;GRAPHICALMETHODS

    BMESTER'SCURVE

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    ICSOFPLANKMECHANISMS

    becomeclearlater,andthroughthesixpoints

    ondingrotocenterlines,asheree =0.Thus

    urveareknownimmediately.

    urmester'scurvehasbeenselectedasaloca-

    ecorrespondingmovingpointislocatedby

    version,asshowninFig.11-22.(Figure

    uationasFig.11-20. O,hasbeenplacedarbi-

    t.)Thebody risassumedtobe stationary,

    fO,are determinedbyreferringthetriangles

    O,tothebaseline AiBi.Thecouplerhinge

    tedatthecenterof thecirclethroughO,,

    epresentexample,becauseO.hasbeenselected

    tocenter,twoofitsrelativepositionscoincide.

    sible todrawacirclethroughthreepoints,it

    ocentersmustbepointsofBurmester'scurve.)

    emofhavingto designalinkageforthe

    body,thedesignershouldcheckfirst whether

    ofthe availablerotocentersorpointsofinter-

    ticablemechanisms.If,forsomereason,no

    eobtainedinthismanner(e.g.,the mecha-

    tetransmissionanglesormayhavetopass,

    anin-linepositionofall links,whichnormally

    ion),thenBurmester'scurvemustbedevel-

    her locationsofthefixedpivotsinvestigated.

    bodyr(Fig.11-23)is hingedatAto the

    totheframeat Oq.ThepointBis tomove

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    ESIS;GRAPHICALMETHODS

    onsBi,B2,B3,andB^A secondguiding

    ablefour-barlinkage.

    Bknown,thecorrelatedpositionsAi,

    ocatedandthefourrotocentersRu,Ru,RM,

    thesecenters,partofBurmester'scurveis

    ectedarbitrarilyaslocationforthe fixedpivot

    tionsofO,aredeterminedbykinematic

    iBi0J1,etc.SinceO,isentirelyarbitrary,

    vepositions,O}= O,,O]1,O}11,andO}v.

    e,inwhosecenterCiislocated.

    n;GeneralDiscussion

    ntfacetofkinematicsynthesisisthe devel-

    ators,devicesusedinmechanicalcontrolsystems

    inwhichthedisplacementoftheoutputlink

    e input.

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    AMICSOFPLANEMECHANISMS

    edmechanisms,adefiniterelationshipexists

    tsofthedrivinganddrivenlinkswhichis gov-

    rtionssuggeststhepossibilityof usingbar

    orfunctiongeneration.Theideaisattractive

    msofferanumberofconstructionalandopera-

    aseofmanufacturewithinclosetolerances,excel-

    otsandsliders,and absenceofabruptchanges

    nsmoothandquietoperation.However,two

    sttheir useasfunctiongenerators,viz.,their

    efinite numberoflinks,toreproduceagiven

    alexactitudeoverafinite rangeandtheextreme

    mechanismswithmorethanfourmembers.

    ringproblemsrequirerigorouslyexactanswers.

    barlinkageandits sliderderivativespossess

    oallow,ingeneral,the findingofasolutionin

    ructural"erroriskeptwithinaprescribed

    nctiongenerationbymeansofbarandslider

    pproximate.Moreover,becauseofthephys-

    outputdisplacementranges,onlyalimited

    anbe mechanized.

    tofunctiongenerationarepossible.

    tion.Thegeneratedandspecifiedfunctions

    nctpoints.Betweenthese"precision"points,

    buttheerror iskeptwithinpermissiblelimits.

    alprocedures.)

    neration.Thespecifiedandgeneratedfunc-

    erivativesatonepoint.The approximation

    npoints,but withinamuchshorterrange.

    alyticalprocedures.)

    saandb.

    therprecisionpointsnor precisionderiva-

    eerror isconfinedtoanacceptabletolerance

    erange.Nomographicprocedures(notdealt

    "methods,andexperimentalmethodsfall

    on.Thefirststepinthesynthesisof afunc-

    rsionofthe givenfunction

    gtheoutputand inputdisplacements,e.g.,

    s,

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    HESIS;GRAPHICALMETHODS

    nsformationequations

    ors,indegrees perunitofcorrespondingvariable

    utlink positionscorresponding,respec-

    andy

    aybeofthe openorthecrossedtype.The

    sgenerallyyieldsthemorecompactmechanism.

    the factthattheinputand outputdisplace-

    e.Consequently,ifacrossedlinkageis desired,

    chosenasfollows:

    ction (ydecreasingwithincreasingx)and

    n

    aFour-barMechanism.Thecharacteristic

    inkingthepositionsof theoutputandinput

    tions(11-1)and(11-2)showthatthe

    signparametersinvolvedinthemechanization

    specifiedrangeisseven:

    ple,q/p,r/p,s/p

    andk$(or rangesA

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    AMICSOFPLANEMECHANISMS

    erivativetothree,etc.)However,sincethe

    osynthesizeamechanismfora seven-point

    ve,twoparameters,atleast,areassumedin

    ndinglyfewerpointsofagreement.(Ina

    thefollowingparametercombinationscould

    ctors,onescalefactorandoneinitial position,

    deratio.) Shouldtheresultantmechanism

    ,byexceedingthepermissibleerrormargin,

    tbemade,basedondifferentassumptions.

    orationalmethodsforchoosingtheparameters,

    erbe guidedbypastexperienceorsimplyrely

    bmayserveas aroughguideforthe start:

    ^/A

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    ESIS;GRAPHICALMETHODS

    mainstationaryinits phaseSi=O.B1,and

    2is referredtoitby meansoftherotation

    edin Fig.11-25c.BecauseofthisrotationB2

    dAitoAu.TherotocenterRuis thenlocated

    ormalbisectorsof 0,OJ1andA1Au,anditwill

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    ICSOFPLANEMECHANISMS

    torofOqOl* passesthroughO,andmakesan

    of centersOqO,.

    256andc revealsthatRumaybelocated

    raysdrawn,respectively,throughOqand

    i2/2totheline ofcentersOqOasshown

    -26showsafour-barmechanisminthree

    ethereforethreerotocentersassociated

    vetoq,namely,R12,Ru)andRu-

    3 aredeterminedasinthe two-position

    terminationofthelocationofR23relative

    uiresfurther discussion.Theintersectionof

    ely,at 023/2and ^23/2tothelineof

    appropriatepivotpointsdefinestherelative

    2-3in phase2oithemechanism.Conse-

    edby Rnm.Itspositionreferredtoqh

    nedby rotatingtherayOqR23(2)through 4>u-

    iwouldbe obtainedbyrotatingtheray

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    ESIS;GRAPHICALMETHODS

    beextendedtotheconstructionofrelative

    threepositions.

    der-crankMechanisms.Figure11-27

    therelativerotocentersinmechanismswhich

    tructionisself-explanatory.InFig.11-276,

    nreferredto q%.Inordertorefer ittoSi,

    oveda distance lu.

    gnaslider-crankmechanismforthegenera-

    x,withprecisionpointsatx =1,2,3, and

    0.47712,and0.60206.Theindependent

    ntedbythehorizontaldisplacementofthe

    dthedependentvariableybya counterclock-

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    ICSOFPLANEMECHANISMS

    equirementofafour-pointapproximation,

    maybechosenarbitrarily.Themostcon-

    ethetwo scalefactorsandtheinitialposition

    v ingA l=k1A x=A x

    y,givingA0=fc* Ay=100Ay

    in., lu=3in.

    u=6012'

    itionmechanisminvolvestheconstruction

    chrequiresthedeterminationoftworelated

    ccordancewithTable11-1forexample,R^Ru

    ,thesecentershavebeenreferredto qt.

    ter'scurveisa theoreticallypossiblelocation

    eAi, thechoiceoftheinitialposition isarbi-

    Ai locatedonthecrankcircle,theconstruc-

    ofthesecondcouplerhingeBproceedsas

    edtobe stationaryinitsphases1,and the

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    ESIS;GRAPHICALMETHODS

    oundby makingA2>A11= lu,

    t>AIV=ln; Biisthecenterof the

    11,andAIV.

    sibleto synthesize,bythismethod,a

    tapproximation.Thechoiceoftheinitial

    uldnolongerbearbitrary.Thepoint would

    onoftwo Burmester'scurves,developed,

    ntsetsoffourpositions.Ofcourse,thesolution

    n;ReductionofPointPositions1

    Thethree-positionproblemistrivial,and

    meansforexplainingtheprincipleofthe

    s.

    nthespecifiedandgeneratedfunctionsis

    s,four designparametersarearbitrary.

    ceisthatofthe twoscalefactorsk^,andk+,of

    ofthelinkratiop/q. (Theactualdimensions

    hesolution,exceptfortheover-allsize ofthe

    ptionsleadtothevaluesoffa2,fa3,^12,and

    edbythe design.

    etriebelehre,"pp.326-341,HermannSchroedelVerlag,

    en,Point-positionReduction,Trans.FifthCon/,on

    1-193,PurdueUniversity,Lafayette,Ind.

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    ICSOFPLANEMECHANISMS

    the positionofthecouplerhingeB,the

    and3are referredtotheoutputlinks inits

    ofthecirclethroughthethree relativeposi-

    edas follows:

    edthrough 0i2.

    edthrough 0i3.

    reductionofpointpositionsisthefact that

    wacirclethroughthreepoints.In thefour-

    tions,thedesignparametersaresochosenthat

    hepoint

    mberof

    ducedto

    this

    parameters

    d fc^(or

    erto

    elative

    derto

    relative

    einitial

    kmust

    le0,+i

    djusted

    entersOqOs

    +i,asshownin Fig.11-30

    ativesignof 0,n+iisdisregarded.)

    chanizethefunctiony=log xinthe

    cisionpointsat x1 1,y1=0; X2=4,

    =0.8451;andx4= 10,2/4=1.0000.

    yassumptions,k$=10 perunitofx

    y, thelinkdisplacementsarecalculatedas

    30 i3=60 0i4=90

    =-368'0= -5042'0=-60

    hosenthatoneoftheinput angles,here0i2,

    Oandthecorrespondinglinkratiop/qis

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    HESIS;GRAPHICALMETHODS

    ermined,theremainderofthesolution

    eresultantmechanismisshowninFig.11-31.

    precisionpointsexceedthe permissible

    ativesolutions,obtainedbybisectingeither

    veto beinvestigated.Otherchangeswhich

    redistributionof precisionpointswithinthe

    fthe assumedscalefactors.

    onlythreedistinct relativepositionsofA

    >i andthedistributionoftheprecision points

    oinputdisplacementsm,narebisectedbythe

    oftheprecisionpositionsis nolongercom-

    n,onlyonedesign parameter,viz.,fc$may

    ngementinwhichthe crankpositions1,4

    ydisposedwithrespecttoOqO,.Theproblem

    nofalinkratio p/qsuchthattheoutput-

    enbythelinkage,is equaltothatobtainedby

    onvaluesofthe specifiedfunction,where

    nt_ A^j_ Ay.-

    entA^0Ay0

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    AMICSOFPLANEMECHANISMS

    e input-displacementratioR^,,similarly

    ent_ A,_ Az,-,...^

    entA

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    HESIS;GRAPHICALMETHODS293

    a trial-and-errorprocedure.Asmall

    tween1 and3istried graphically,andthe

    andA^0aremeasured.Thusthe approxi-

    nestablished.Itsexactpositionis foundby

    cal(R* versusp/qcurve.Ithas thefol-

    ueof1.

    p/q= 1.

    Gfyisslightlysmallerthan (R^;outsidethis

    osesaserious restrictiononthetypeof

    mechanizedtoa five-pointapproximationby

    point positions:

    -r-1andconsequently-~> -r2-

    besuchthatthe slopeofthe"innerchord"is

    terchord,"asshowninFig.11-32c.

    hodofreductionofpoint positionshasthe

    er,therestrictionsplacedonthe designby

    blecrankarrangementsoftenprecludethe

    tion.In general,therelative-rotocenter

    pectsforthesuccessfuldevelopmentofa useful

    chanizethefunctiony= sin* xwithinthe

    ecisionpointsat xx0,y10; x* =2230',

    3=0.5000;x4=6730', yi=0.8535;and

    entralsymmetry"ofthegivenfunction,

    gementmaybeexpectedtoresultin agood

    designis choseninwhichtheangles 4>nand

    eofpivotsOqOs,as showninFig.11-33.The

    dat1 perdegreeofx.Therequired ratioffl*

    eeventuallyyieldsp/q=1.85,giving

    ment.

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    ICSOFPLANEMECHANISMS

    ofy

    put rotationsknown,therelativepositions

    usualmanner.A1andAvcoincidewithA1,

    dcoincidentpair,andA1u occupiesthe

    ethethreepoint positionshappentobe

    smresults.(B1,thesecondcouplerhingein

    rightanglesto thelineA1AuAUI.)

    eneratedFunctiony=sin's

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    HESIS;GRAPHICALMETHODS

    unctionsarecomparedin Fig.11-34,and

    ownin Table11-2.

    dnegativeerrorsmaybeequalizedbya

    r"range.Should theresultantmaximum

    entofthe outputrange)beconsideredexces-

    gns,basedondifferentvaluesofthe scale

    ei nvestigated.

    ;OverlayMethod1

    aphicaltrial-and-errorprocedurewhich

    egeneratedoutputhasneitherprecisionpoints

    commonwiththespecified function,but

    gMechanismsandLinkages,"pp.147-154,McGraw-

    ewYork,1948.

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    ICSOFPLANEMECHANISMS

    thinanarrowtolerancebandthroughoutthe

    ortwodesign parametersarechosenarbi-

    onesarevaried inasystematicmanneruntila

    uracyisobtained.

    pton.Thechosenparametersarek$,k*,and

    .Thedesignprocedureisasfollows:

    ontobemechanizedissuitablysubdivided,

    gularincrementsm,nand\f/m,narecomputed.

    ufficientlylargescale,ofthesuccessive

    k,andwith theassumedlengthofthecoupler

    plercirclesisdrawn,centeredinthesuccessive

    (Fig.ll-35a).

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    ESIS;GRAPHICALMETHODS

    e,on transparentpaper,ofthesuccessive

    In addition,markedonthisoverlay,

    circles,centeredinO,,whoseradiirepresent

    putlink (Fig.11-356).

    thefirstlayoutandmovedacrossit until

    hthecouplercircles1,2,3,etc.,pass through

    onecircleofthe overlay.(Intryingto

    toverlaycircleswill bescannedinturn.It

    polate.)

    und,asshownin Fig.11-36,thelengthsof

    utlinkandtheinitial positionoftheinput

    ereadoff thedrawing.

    ng,noacceptablesolutioncanbefound,

    allyassumedparametersmustbechanged,

    ed.

    einthesign ofk+willhavethe effectof

    overlay.It shouldbenotedthatthesame

    urningtheoverlayfacedown.

    n.Thetwochosenparametersarefc^,and

    wn,itis notpossibletoconstructaspecific

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    ICSOFPLANEMECHANISMS

    unction.However,iftherangeAj/ ofthe

    dividedintonintervalswhichincreasein a

    ndanoverlayisconstructedofzangularspaces

    hesameratioas thefunctionintervals,then

    pacesmaybeusedtorepresentthe ncorre-

    eoutputrangeA^.Thusthis typeofoverlay

    aybeused inthesolutionof anyproblem.

    t,differentsectorsofthe overlaywillbe

    ay,IntervalRatiofffc=y/2

    edfromthereferenceline)

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    ESIS;GRAPHICALMETHODS

    taforthe constructionofageneraloverlay,

    ectedintervalratio(R,- =-\/2,whichdoubles

    e11-37showsaportionof thisoverlay.

    ewi tisadvantageoustohavetheinput

    yaspossible.Forthis reason,inthecaseof

    slope,asshownin Fig.11-38a,Ayisdivided

    lis atthelowerendof therange,andthe

    hosenforafunctionwithdecreasingslope,as

    softhe outputintervalsasfractionsofthe

    sinto4,6, and8spaces.Thevaluesare

    R, -=-\/2.

    hanizethefunctiony=logiox,between

    therangedividedintosixintervals.

    ndthecoupler-crankratioareassumed.

    =60, givingk$=A0/Ax=^-= 6f per

    wingvaluesforthe outputintervals(Ay=1,

    698,yu= 0.4262

    95,yn =1.0000

    ,andm,n=k^cm,n,

    0xn=9.000

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    AMICSOFPLANEMECHANISMS

    tudesBasedon(Ri=y/2

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    ESIS;GRAPHICALMETHODS

    ationincrossedandopen mechanisms,makesit

    moresuited totheformerarrangement.

    dontwoprecisionpointscumderivatives,

    rily,correspondingtotheextremesofthe

    ativesatanumberofselectedvaluesof the

    esolutionproceedsasfollows:

    dfc^andthe linkratioq/pareassumed.

    respondingtothe prescribedorselectedn

    culatedandmarkedoffonp[Eq.(10-14)]:

    Og>O,

    chosenarbitrarilyonthecrankcircle.

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    CSOFPLANEMECHANISMS

    nsAfPi andA+Pnaredrawnin,and the

    usteduntil BfandB+lie onthesamecircular

    le\f/^nis comparedwiththerequired

    caseatthe firstattempt,thetwoangles

    iterated

    untilthe

    ained.

    nreached,

    ositions

    ponding

    esame

    wnin

    edureis

    ratiosq/p

    olutionis

    reached

    torsare

    yof scan-

    atio,which,

    only10to 15min,thisapproachleadsto there-

    verlaymethodwith a"free"outputscale.

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    ESIS;GRAPHICALMETHODS

    hanizethefunctiony=log x,between

    precisionpointsatx=1 and10andprecision

    7,and10.

    1.Assume

    ^=^ perunitofx

    =-90 perunitofy

    culatedbyEqs.(11-6)and (11-7),where

    746p,h=0.594p

    butnot averysatisfactoryone)obtainable

    orsisshownin Fig.11-42.Theparticulars

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    ICSOFPLANEMECHANISMS

    rones'sandNelson'sMotionAtlas1

    hesisofmechanismsforthe productionof

    ossessingcertaindesirablecharacteristics,or

    gha numberofprescribedpositions.

    urvesinthe designofsingle-dwellmechanisms

    ouslyinFigs.11-11and 11-18.Otheruses

    onsofengineindicators,specialindexingdevices,

    dapplicationsassociatedwithagricultural,

    ngmachinery.

    diusDC

    ratD1i radiusDC

    onAtlascontainssome7,000couplercurves,

    callyoperatedfour-barmechanismwhoselink

    tematicmanner.Ineachsetting,thecoupler

    mberoftracingpoints,arrangedina grid

    oducedbymechanicalmeans,thepagesof

    a familyofcouplercurvesisfoundwhose

    hedesiredgeneralshape.Correspondingto

    arateoverlayofthegivencurveis thencon-

    son,"AnalysisoftheFour-barLinkage,"JohnWiley

    1.

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    ESIS;GRAPHICALMETHODS30")

    axesof bothareequal,andtheir shapesare

    ocedureislaborious,butoftenyields a

    eratethespecifiedcurvewithinanacceptable

    anaidin thedesignofdwelllinkages.For

    ofFig.11-43,witharise-dwell-fall-dwell

    eru,wasdevelopedin thismanner.Itsbasic

    obtainedasa resultofamethodicalsearchof

    a couplercurvewhichhadtwoappropriately

    engthwiththesamecurvature.Thelinkage

    andr/p=s/p= %,andasfaras canbe

    drawinginstruments,thepathofthecoupler

    = 90 andBC/p=1.6/3,satisfiesthe

    eductionofPointPositions1(FixedPivot

    er)

    generation,themethodofreductionofpoint

    eapproach,ofsomewhatlimitedscope,to

    on.Thebasisofthe methodwillagainbe

    trivialthree-pointconstruction,andthe

    endedtothe morecomplexproblemsinvolving

    positionsofa point.

    ig.11-44,thecouplerpointCis required

    prescribedpositionsCi,C2,and3.Ifno

    bemet,the problemadmitsasixfoldinfinity

    ofthefree choiceofthefollowingdesign

    (2d.o.f.),directionofthebaseline and

    gthOqAofthe crank(1d.o.f.),andthe

    (1d.o.f.).

    foundbymeansofkinematicinversion,i.e.,

    tionaryinits phaseTIandmovingtheframe.

    arefound,therefore,bymaking

    d0J"=A^3C30.

    ofthecircumcircleofthetriangleO,O}1O}11.

    ismsformorethan threeprescribedpoint

    signparametersaresochosenthatsome rela-

    e,leavingthreedistinctpositionsthroughwhich

    etriebelehre,"pp.326-341,HermannSohroederVerlag,

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    ICSOFPLANEMECHANISMS

    dertoachievetherequiredreductionof

    votO,of thedrivenlinkismadeto coincide

    softhe coupler,forexample,[Rr]u,asshown

    ositionof thesepointsonthenormal

    elyarbitrary.)Asa consequenceofthis

    metricallydisposedwithrespecttothe

    e

    ,A

    O,Oy=

    ;because

    and

    ry,butonceassumed,determinesthe

    Oqon thebaselineis alsoarbitrary,but

    ranklengthOqA.Theintermediatepositions

    don thecrankcircle[(C2A2=CiAi),etc.],

    fO,constructedinthe usualmanner.Because

    th[Rr]u,0,IVcoincideswithO}= O,,andthe

    sitionsis reducedtothree.

    infinityof solutions(4),asfollows:

    o.f.),directionofbaselineandpositionof

    ebetweenCandA(1d.o.f.).

    scaseO,ismadeto coincidewithtwo

    sly.Itisthereforelocatedattheintersection

    oneof thefollowingcombinations(onepoint

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    ESIS;GRAPHICALMETHODS

    r):

    e O,Oqisarbitrary.

    madetocoincidewith[Rr]nand[Rr]3t-

    =^16/2and$.A3O,Oq=^34/2.PointsA\

    respectiverayswithanarbitrarilyassumed

    attheintersectionofthebase linewiththe

    smarkedonthe crankcircle,andtherelative

    cted.Asaconsequenceoftheparticular

    swithO]=O,,O}vcoincideswith0J11,and

    inctposition.

    utionshasbeen reducedtoatwofoldinfinity

    fthebaseline(1 d.o.f.)anddistancebetween

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    ICSOFPLANEMECHANISMS

    ally,thecouplerpointisnotmerely

    numberofdiscretepositions,buttotracea

    taindesignpositionsarechosen.It ispossible

    nstructiontosixpoints,providedthe sixth

    nthe samecircle,centeredat0asthe

    n.Thusthethreerotocenters[Rr]u,[Rrhs,

    oincidewithOasshownin Fig.11-47.

    sthatof thedirectionofthebaseline.

    a3havebeendrawn,asuitablelengthCA+is

    thepointsAf,A$,and A^arelocatedon

    ndthecenter0+oftheir circumcirclecon-

    he casewiththefirstrandomattempt,0+

    nbaseline,theconstructionisreiteratedwith

    dthelocusofO+developed.Theintersection

    lineyieldsthetrue positionofOq.Next,the

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    ESIS;GRAPHICALMETHODS

    erminedbyinterpolation,theactualpositions

    ys,andtherelativepositionsofO,constructed.

    ,,0,vwith0.11,0JV with0.m,andBiislocated

    mcircle.

    lutionshasbeenreducedto asingleinfinity,

    oiceofthebase-linedirection.Thusit would

    rtherandspecifyaseventhdesignposition.

    ina systematicsearchforaparticularbase

    awingacirclethroughfour distinctrelative

    eductionofPointPositions(MovingHinge

    er)

    tions,accomplishedbyplacingthefixed

    centersofthecoupler,hascertainlimitations.

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    ICSOFPLANEMECHANISMS

    d itselftothesynthesisof couplercurves

    ofdouble-dwelllinkageswithextendeddwell

    sareovercometoalargeextentbythe

    ichthe movinghingeB,ratherthanthe

    esamepositionas thecouplerrotocenter.

    oachesareavailabletothedesigner;should

    red result,theothercouldbesuccessful.

    re11-48showsfourpositions,Ci,C2,C3,

    raversedbythecouplerpointC.Asshownin

    problemhasafourfoldinfinityof solutions.

    equiredreductionof pointpositions,the

    coincideintwopositionsofthecouplerwith

    nter,forexample,[Rr}u,whosepositiononthe

    tirelyarbitrary.Alsoarbitraryis theposition

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    HESIS;GRAPHICALMETHODS311

    auseofthecoincidenceoffi1|4with [Rr]u

    nd BzAzaresymmetricalwithrespectto

    inedtoit atanangleXu/2,whereXH isthe

    ecouplerbetweenpositions1and 4;thatis,

    tobe choseniseitherthelength CAorthe

    rmediatepositionsofA andBcannow be

    z CiAi,whichdeterminesthepositionof

    the positionofB2is foundwithA2B2=AiBi,t

    edpivotO,islocated atthecenterofthe

    B3.

    olutionoftheproblem,thefollowingkine-

    noted(Fig.11-48).In theinversion,in

    stationaryinthephaseri,the fourrelative

    ecenteredat AI;furthermore,therays

    aresymmetricalinrelationtothe lineBi,tAi

    /2.

    movinghingeBismadeto occupytwo

    ntwiththerespectiverotocenters.InFig.

    .RJis,andBs,4 with[/2r]s4.Thepointpairs

    thesequenceinwhich thepointpositionsare

    closesthe other.Consequently,thefollowing

    rsarepossible:

    Rr]^;[Rr]16 [Rr]!H;

    [Rr]34

    irectionofthelineBi,6Oq arearbitrary,but

    neisno longerso,aswillbe seenfromthe

    locatedinanarbitrary positionontheray

    , andOvqarethepositions occupiedbyOqin

    coupleriskeptstationaryinits phaserI.

    atrandom,thesepointswill notsatisfythe

    ttheylieonone andthesamecircle.To

    aysSi,60J andBi,sO mustbemirrorimages,

    iAi,oftheraysBi,6O\ andBi,6O\11;thatis,

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    AMICSOFPLANEMECHANISMS

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    ESIS;GRAPHICALMETHODS313

    thisdiagram,therayB3,tOqisinclinedto

    tanangle

    edto thenormalbisector[ncjisat

    gandB3itOqmakeequalangleswith thecorre-

    gleincludedbythem(vertexOq)is equalto

    sectors(vertex^15.34); i.e.,

    ^15-34.83,4

    tsOq,B1i6B3,4,and#15.34(the pointof

    bisectors[nc]isand[nc]n)lie ontheperiphery

    enotedbyk ]5.34,isthe locusofallpossible

    catedatthe intersectionofthechosen

    16.3t,thepositionsofOqrelative toriare

    edat thecenterofthecirclethrough

    distanceACarethusdetermined.Next,

    arefound,andthemechanismiscompleted

    rof thecirclethroughJ5i,6B2,and#3,4.

    itionof AIonthecrankcircle;A2,82 =AiBi

    ethepositionof B2.)

    boveconstructionmaybeextendedtosix

    mhasasingle infinityofsolutions,dueto

    engthCB.The couplerhingeBismadeto

    ositionsBi,e=[Rr]u,#2,5= [Rrlu,and

    catedatthecenterofthecorrespondingcircum-

    ytheconditionthatit mustliesimultaneously

    ci6-34.

    explanatory,showstheapplicationofthe

    ofadouble-dwellmechanism.Inpractice,the

    kerarmmay havetocorrespondtodefinite

    le.Therequiredcorrelationmaybeobtained

    , orfollower,ofadrag-linkmechanism,

    ouble-dwelllinkage.Thecoordinationofthe

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    ICSOFPLANEMECHANISMS

    otatingprimarydriver(determinedbythe

    epositionsqiq3andqtq^ (whichdefinethe

    hedbymeansofBurmester'scurve.

    oberts'sTheorem1

    ecurvegeneratedby agivencouplerpoint

    anbe reproducedbytwootherfour-bar

    ththefirst.Itis ofpracticalimportance

    nerconcernedwith thesynthesisofamechanism

    rticularcurvetwoadditionalalternatives,

    o bemorefavorablethantheoriginaldesign

    glesorspacerequirements.

    Motionin PlaneSpace,Proc.LondonMath.Soc.,no.7,

    enbergandJ. Denavit,TheFecundFour-bar,Trans.

    s,pp.194-206,1958,PurdueUniversity,Lafayette,Ind.

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    ESIS;GRAPHICALMETHODS

    maryfour-barmechanism,p=OgO,,

    ,towhichadditionallinksareattached,

    DCE,suchthatOqDandDCforma parallelo-

    dADCEis similartoAABC.

    CFG,such thatO,FandFCformaparallelo-

    ACFGissimilar toAABC.

    areadded,whichformaparallelogram

    hanismhas13lowerpairs(two eachatOq,O,,

    B,D,E,F,G, andH)andis thereforeconstrained:

    2l=3(9)-2(13)=1

    hroughoutthemotionofthis compound

    nsstationary,sothatthelinkagecouldbe

    eframewithoutaffectingitsmobility.If

    mechanismmaybesplitupinto threeseparate

    showninFig.11-52,eachofwhichwillgivethe

    C.

    thepoint0

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    ICSOFPLANEMECHANISMS

    os(+a)+-sc os(^+a-180)

    (+a)sc os(^+a)

    sc os^)c osa

    sin^)sina]

    sc os^)sina

    n*)c osa]

    ateralOqABO,,

    os^=p

    n^=0

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    ESIS;GRAPHICALMETHODS

    ly provethat0

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    AMICSOFPLANEMECHANISMS

    otheconclusionthatthefollowingcombi-

    nismsarepossible:

    hanismsandonedouble-rockermechanism

    isms

    echanisms

    aybeappliedalsotoslider-crankmechanisms.

    s,whilenotingthatO,is atinfinity,itwill be

    natemechanismsvanishes.Thusthereexist

    hanismswhichwillproducethesamecoupler

    nsionofthetheoremisoflittle practical

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    ESIS;

    eanalyticalapproachtosynthesisisits

    tunately,thissuperiorityovergraphical

    etbya numberofadversefeatures.For

    rogressivephysicalimagesofthemechanism

    nofdesirablemodificationsduringthedevelop-

    lt,obtainedafterlengthyand laborious

    etobecompletelyimpracticable.Moreover,

    impossible,toassessintelligentlytheeffects

    thedesign,themethodoftendegeneratesinto

    ocedure.Itsfullpotentialitiescanbe

    ofahigh-speeddigitalcomputer.

    n;Freudenstein'sEquation1

    echanismareregardedasdirectedlineele-

    1,then

    c os4>(a)

    in(b)

    qs.(a) and(b)yieldstherelation

    os^ 2pqcos 2qscos(0 \p)(c)

    onofthesideratios

    +61,cos\p=cos ( 4d(12-2)

    edbyFreudenstein,formsthebasisof a

    mateSynthesisofFour-barLinkages,Trans.ASME,

    1955.

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    ICSOFPLANEMECHANISMS

    achtosynthesis.Itisadaptabletoboththe

    ion-derivativemethodsoffunctiongeneration.

    edfromthediscussionof Chap.11.In

    atedandspecifiedfunctionsagreein anumber

    s,andeverywhereelseanunavoidablestructural

    osemagnitudedependsonthespacingofthe

    tureofthe function.(Thelowestmaximum

    acinginwhichereachesthesamevalue between

    tsandbetweenthe limitsoftherangeand the

    )Inthesecondmethod,thegeneratedandideal

    tandhave anumberofderivativesincommon.

    edesignofafunctiongenerator,thegiven

    rtedintothefunction^=/(

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    hods321

    n;Precision-pointApproximation

    r,precisionpointswillbe designatedby

    gewillbedenotedbythe newsymbols

    y,butneednot,coincidewiththefirst precision

    echosenparametersareft*,ft*,fa,and

    ecomputedbymeansofEq. (12-3),as

    i,7i,etc.

    esintoEq.(12-2) yieldsthreeequationsfrom

    maybe calculated:

    fa.=cos(fa \p1)

    a>=cos(fa fa)

    a,=cos (fa fa,)

    parametersassumedareft*,ft*,andfa,

    requations:

    (fa+fa,1)=cos[(fa fa,1)-fa]

    (fa+fa,2)=cos[(fa fa.i)-fa]

    (&+ fa,3)=cos[(fa fa,3) fa]

    +faA) =cos[(fa-fa,i) -fa]

    sideratios yieldsacubicequationintanfa,

    +m3tanfa+ml=0

    ntsm,thereaderis referredtoFreudenstein's

    fa known,thesideratiosarefoundas inthe

    n.

    Thearbitrarychoiceofft* and ft* leadsto

    ,cos(fa +faA)=cos[(fa,1- faA)+fa-fa]

    ,cos(fa +fa,i)=cos[(fa,i- fa,i)+fa-fa]

    R,cos(fa +fa,3)=cos[(fa,3- fa,3)+fa-fa]

    (R,cos(fa+ ^,-,4)=cos[(faA-faA)+ fa-fa]

    ,cos(fa +fa,s)=cos[(fa,s- fa.t)+fa-fa]

    sideratios yields,afterextremelytediousand

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    AMICSOFPLANEMECHANISMS

    ns,thefollowingexpressions,whichmustbe

    WJ)

    tf-4F[F'3]

    bic expressionsintan^t-,andF[,F2, andF'3

    an#,-.(For detailsoftheseexpressions,the

    enstein'soriginalpaper.)After 0,-and\pfhave

    atiosaredeterminedas inthethree-point

    onofaparticularproblem,basedonthe use

    ke10 to12weeks.

    ;Precision-derivativeApproximation

    iminarystepin themechanizationofa

    ethodofprecisionderivatives,itis necessary

    tocorrespondingderivativesofthe function

    ^dx

    bedvaluesofthese derivativesintothebasic

    tionswhichdeterminetheparticularlinkage.

    equationsareobtainedbysuccessive

    2).

    os\p=cos ( iA)(12-2)

    (1-

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    METHODS323

    +Vsin}}

    )2c oa(0-tf )(12-9)

    +W''"-(^')31sin ^}

    (1 -^)3]sin(pand thesideratiosaredeterminedfromthe

    btainedduringthereductionprocess.

    errepresentationofvectors(Fig.12-2),

    havedevelopedaveryelegantapproachtothe

    Sandor,Synthesisof Path-generatingMechanismsby

    gitalComputer,Trans.ASME,vol.81B,no.2,pp.

    orandF.Freudenstein,KinematicSynthesisofPath-

    yMeansoftheIBM650Computer,IBM650Program

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    AMICSOFPLANEMECHANISMS

    hanismsforthepurposeofgeneratingapath

    rypoints,with prescribedcrankrotations.

    stillmanageablewiththe aidofadesk

    ntsynthesisdemandstheuseofa high-speed

    procedurehasbeenprogrammedtosuitthe

    whichautomaticallydeterminesallexisting

    2linkages),selectsoneonthe basisofa

    omputesthecoordinatesofthetracingpoint

    rotation.

    definedas

    mumandmaximumskeletaldimensionsoflinkage

    eencouplerhingesand

    drivinglink

    yofanunrestrictedcrankrotation,thequality

    favorof linkagespossessingthischaracter-

    ratherthan2w.

    rMechanismsforSpecifiedInstantaneous

    mponents1

    y,andaccelerationdiagramsofthefour-bar

    12-3aredefinedbythe vectorequations:

    +s=q +r

    A+VBA

    &A+&BA

    ntocomponentsinthedirectionofthe xand

    ionscanbereplacedbysix algebraicequations:

    esisofFour-barMechanismsbytheMethodof Com-

    chanics,vol.24,no.4,pp.22-24,1957.

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    METHODS

    3variables,viz.:

    of thedrivinglink,itsangularvelocityW3,

    a,

    thecoupler,itsangularvelocity,,and

    p

    tions,problemsofsynthesisinwhichseven

    cribedmaybesolvedeither directlyorbythe

    ch.

    efollowingdesignparametersarespecified:

    onwanda.

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    AMICSOFPLANEMECHANISMS

    t outlinedbelowwouldbeadoptedifthe data

    inkswereinterchanged.)

    biningEq.(12-12)withEq.(12-15),and

    ),thefollowingequationsareobtainedin

    eexpressedintermsofthe unknownangular

    bedquantities:

    17)arecombinedto eliminatear,giving

    qxry)+ur2(rx2+rv2)

    y rysx)(e)

    (d)intoEq.(e)yields aquadraticequation

    sequaltouq,giving infinitelylonglinksq

    ,whichrepresentstheactualangularvelocity

    theexpression

    mechanismshallsatisfythefollowing

    secaq=0

    4.625in.w,=5 rad/sec

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    ods327

    66,090=0

    sec

    1.77in.q =1.92in.

    r= 7. 22in.

    followingparametersarespecified:

    ,andaq

    arctan >uanda,

    outlinedinthefollowingwouldbeused if

    ddrivenlinkswereinterchanged.)

    sethe gradualeliminationoftheunknown

    ldanequationofthe fourthdegreeinqx,thus

    ofthegradual-approachmethodofsolution.

    andthecorrespondingvaluesofwr andtan

    ,usingthegeneralprocedureoutlinedin Illus-

    pis reiteratedanumberoftimes,andthe

    gainstqx ortabulated.Thefinalresultis

    edure.

    mechanismshallsatisfythefollowing

    = 10rad/ secaq= 0

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    esultsforNumericalExample2

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    METHODS329

    ecaq 0

    secar=15rad/sec2

    a, =10rad/sec2

    =sx+p (a)

    =sy(b)

    y= 5sy(c)

    rx= 5sz(d)

    4rx+15ry =25sz+10sv (e)

    4ry- 15rx=25sv-10sz (/)

    mbining(b) with(c),and(6)with(/):

    lOs^(A)

    cedtofiveequations,Eqs.(a), (d),(e),(g),

    eunknownquantitiesqx,rx,ry,sx, andsy.

    ombining(g)with (e),and(g)with(h):

    t)

    to fourequations,Eqs.(a),(d),(i),and(j),

    uantitiesqx,rx,ry,andsy.

    minatedis ry.Equation(i)combinedwith

    nextbycombining(k)with(a),and(k) with(d):

    m)

    nd(m)resultsin

    hanismare:

    .240

    5

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    AMICSOFPLANEMECHANISMS

    rMechanismsforPrescribedExtremeValues

    theDrivenLink; MethodofComponents1

    (Fig.12-3)the drivingcrankqisassumedto

    ularvelocityw,.Since thedrivenlinks

    tion,co,isvariableboth inmagnitudeandin

    linkagewhichwouldgiveprescribedvalues

    umw,withaspecified constantwg.

    >g =const,Eqs.(12-16)and(12-17)reduce

    w,2+sya,(12-16a)

    xar=s^Wj2 sxa,(12-17o)

    seof therequirementthatw.=maxor min,

    equationsarefurtherreducedto

    12-166)

    =svw,2(12-176)

    ration,velocity,andreducedacceleration

    ectionsof thelinksmaybeexpressedin terms

    follows:

    wgo>, o>.[(o>3 wr)2(w, Wr)2+ay*],.-.

    '^\2I21(b)

    !-o>r)2 +ar2]

    ,r)2+af2](d)

    +ar-'

    +

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    ods

    +(w, wr)2w,2wr2

    (w,-wr)2+ar2]

    )2+ar2

    scorrespondingto maximumw,are

    1,andthose referringtominimumw,bythe

    emofthreeequationsis obtained:

    l2Wrl2

    wrl)2+ari2]

    2w,22Wr22

    (w,2 Wr2)2+ar22]

    wrl)2+ari2]

    )2(w,2 0)r2)2+ar22]

    enEqs.(g)and(i) yields

    ,2 wr2)2

    O,22_ (Wg W.2)2(w,l Wrl)2Wrl2,..

    accomplishedbyeliminatingar22between

    ningtheresultantequationwithEq.(J)] gives

    , W,2)2[(w,l Wrl)2 (w9 Wrl)2]wrl2

    rl)2[wri2 (w, wrl)2]

    Wrl)2[wrl2 (w,l Wrl)2]}= T(Jk)

    ndsideofEq.(k) issimilartothe left-hand

    es1 and2areinterchanged.Equation(k)

    andwr2.Since itcontainstwounknownquanti-

    atthe problemhasaninfinitenumberof

    nga definiteresultistoassumea valuefor

    elimitssetbythe followingcriteria:

    3Wrl w,l)]0

    s,derivedintheAppendixatthe endofthis

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    AMICSOFPLANEMECHANISMS

    ondtimederivative

    edriven linkattheinstantwhen thelatter

    es.

    tedinto Eq.(A;),thecubicequationis

    eroots, theonewhichsatisfiescondition

    valuesforari2 andari2hasphysicalmeaning.

    if eitheruT1orwr2is takenaszero,the

    toaquadratic,andthe calculationsaresimpli-

    ebornein mind.Inthecaseofa crank-

    dw,2haveoppositesense:

    -linkmechanism,wiandw,2havethesame

    signacrank-rockermechanismtothe

    d/sec,w,2=8rad/sec,p= 10in.

    ay betakenaszerosincethis value

    .

    4.11rad/sec

    sfycondition(12-21)andisdiscarded.The

    sconditionandyields positivevaluesfor

    = 197andar22=3,740.

    edintoEqs.(a) to(/),yielding:

    towi:

    q =3.41in.

    .s =5.69in.

    r=9.74in.

    tow,2:

    .

    .

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    hods

    nFig.12-5.The correctnessoftheresult

    ofFreudenstein'stheorem,accordingtowhich,

    e,thecollineationaxisisperpendiculartothe

    signadrag-linkmechanismforthefollow-

    rad/sec,u>,2=5rad/sec,p=10 in.

    er tosatisfycondition(12-21),wri>

    rthercalculationsrevealthat,ifonlyinteger

    hechoiceofsuitablevaluesofur1 islimitedto

    c,sincevaluesoutsidethisrangegivenegative

    ctedvalueofwri=15 rad/sec,Eq.(k)reduces

    o!r2- 3,125=0

    real root,wr2=12.5rad/sec,whichsatisfies

    dsan2=9,490and ar22=703.

    smare:

    tow,i:

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    AMICSOFPLANEMECHANISMS

    owl2:

    nFig.12-6.

    quationa,=w,[w,(3wr uq) &j,(3wr w,)]

    ombiningEqs.(12-16a)and(12-17a):

    x2+r2) =w,2^* +rysy)+a,(rxsy r^)(l)

    ryandrxsx+rysyare recognized,respectively,

    and r-s, andtheterm(r^ r^x)asthe

    maybe writteninthefollowingform:

    wr2r2=w,2rscos (

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    METHODS

    hevelocitiesVAandVBin thedirectionAB

    n Fig.12-7,