5_Threaded Fasteners.pdf

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    Screw fasteners and non

    permanent joints, Power

    ScrewNut, Bolt, Stud, Screw

    M. S. Dasgupta, BITS Pilani

    http://www.google.co.in/url?sa=i&rct=j&q=bolted+joint+under+shear&source=images&cd=&cad=rja&docid=GmV04eBQNC27-M&tbnid=Bcafv1d39qI6rM:&ved=0CAUQjRw&url=http%3A%2F%2Fen.wikipedia.org%2Fwiki%2FBolted_joint&ei=DZsfUfwTsPCYBYLvgZgG&bvm=bv.42553238,d.bmk&psig=AFQjCNGtH1uwQFbZ0bk6duH39-vbky1CLg&ust=1361111899979833
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    Threaded Fastners

    Design of machine elements needs complex geometryand joints; single integral parts not possible

    Parts are joined by fasteners and they are convenientlyclassified as permanent, semi-permanent and non-

    permanent joints Permanent :Welded joints, adhesive bonding

    Semi-permanent : Riveted joints

    Non-permanent fasteners: Threaded / non threadedjoints

    Non threaded joints- keys, pins, snap-fit etc.

    Threaded joints- screws, bolts and nuts, studs etc.

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    Thread Standards and Definitions

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    Lead and multi-threaded screws

    Lead is the distance moved by nut parallel to thescrew axis when the nut is given one turn.

    l=p* multiplicity of threading

    Single threaded, l=p

    Double threaded, l=2p

    Triple-threaded, l=3p

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    The Metric Thread

    M121.75 mmNominal / major diameter of 12 mm

    pitch of 1.75 mmmetric designation

    d = major diameter

    dr=minor diameter

    = d - 1.226 869p

    dp=pitch diameter= d - 0.649 519p

    p = pitch

    pH2

    3

    basic ISO 68 profile with 60symmetric threads

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    Square & Acme threads

    Square thread Acme thread

    Knuckle thread ?

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    Power screw or Screw jack mechanism

    A device used in machinery to change angular motion intolinear motion, and, usually, to transmit power

    Used in machines such as universal tensile testing

    machines, lead screws of lathes and other machine tools,

    automotive jacks, vises, linear actuators, adjustable floor

    posts and micrometers etc

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    Bolts/Screw

    The ideal bolt length is one in which only one or two

    threads project from the nut after it is tightened

    Locations of stress concentrationin a bolt

    At the fillet

    At the run-out

    At the thread-root fillet in the plane of the nut

    The washer face and washersare used to distribute theload under the bolt head and nut face. It also prevent

    fatigue failure of bolt that may result when the burs on

    the imperfectly drilled bolt holescut into the bolt head

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    Understanding Shear and Crushing failure in bolt

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    Understanding failure in plate (joint)

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    Nomenclature of bolt

    or 0.4 mm

    (See Table A-29; page-1053)

    d, Nominal dia or

    major dia

    48

    200

    200125

    125

    252

    122

    62

    ,

    d

    L

    L

    L

    d

    d

    d

    LlengthThreaded T

    45o

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    Table A-29; page-1053

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    CAP screws

    Fillister

    Flat Socket; may be hexagonal or square

    See Table A-30, page-1054 for dimensions.

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    Machine screws

    notice that there is no shank

    driven all the way up to the head

    into the part

    sometimes having a hole for

    screw head to seat in the part

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    Hexagonal nut

    Jam nuts: they are thinner

    (a) end view, general; (b) washer-faced regular nut; (c) regular nut chamfered on both

    sides; (d) jam nut with washer face; (e) jam nut chamfered on both sides.

    See Table A-31, page-1055 for dimensions.

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    Nut Varieties

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    Locking Mechanisms

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    Special purpose bolts & markings on bolt head

    Bol ts with no markings are low strength

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    Note: the dimension H includesthe washer face thickness which is

    normally 0.4 mm.

    Table A31; Dimensions of Hexagonal Nuts

    T i l i

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    -Roundup Table A-17

    td lll ,lengthGrip

    HlL Length,Fastener

    Td LLl grip,inportionunthreadedofLength

    dt lll grip,inportionthreadedofLength

    2,

    2min'length,Grip 2 d

    thl

    dhL 5.1Length,Fastener

    Td LLl

    portion,unthreadedusefulofLength

    dt lll '

    portion,threadedusefultheofLength48

    200

    200125

    125

    ____

    252

    122

    62

    ,

    d

    L

    L

    L

    d

    d

    d

    LlengthThreaded T

    Terminologies

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    Bolt Stiffness

    21

    111

    kkk

    21

    21

    kk

    kkk

    t

    tT

    lEAk

    d

    ddl

    EAk

    td

    tdb

    kk

    kkk

    dttd

    tdblAlA

    EAAk

    Scenario of

    springs in

    series

    At

    = Thread tensile stress area from Table 8-1

    portiond)(unthreadeshanktheofarea;4

    2dAd

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    Table 81 (p:412) Diameters and Areas of Metric Threads.

    dr=minor diameter

    = d - 1.226 869p

    dp=pitch diameter

    = d - 0.649 519p

    The mean of drand dpwas

    used to compute the

    tensile-stress area.

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    Joints- Member Stiffness

    im kkkkkk

    1....

    11111

    4321

    Scenario of

    springs in

    series

    When one of the membersis a soft gasket, km is

    simply the gasket stiffness.

    If there is no gasket, the stiffness of the members is rather

    difficult to obtain, except by experimentation, because thecompression spreads out between the bolt head and the nut

    and hence the area is not uniform.

    Itosultrasonic technique method shows that the pressure

    stays high out to about 1.5 bolt radii and falls off farther

    away from the bolt and suggested to use pressure cone

    method for stiffness calculation.

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    Joints- Member Stiffness

    Figure 815

    Compression of a member with the equivalent elastic

    properties represented by a frustum of a hollow cone.

    Here, l represents the grip length.

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    EA

    dxPd

    .

    2tan

    2tan

    22tan)(

    2222

    dDx

    dDx

    dDxrrA io

    dDdDtdDdDt

    Ed

    P

    tan2

    tan2

    lntan.

    dDdDt

    dDdDt

    EdPk

    tan2

    tan2ln

    tan.

    t

    dDxdDx

    dx

    E

    P

    02tan2tan.

    The Theory of the Frustum of a Hollow Cone

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    Resultant member stiffness:

    dDdDt

    dDdDt

    dEk

    iii

    iii

    ii

    tan2

    tan2ln

    tan.

    If for ithmember,

    i=1, 2, n

    nm kkkkkk

    1....

    11111

    4321

    When all members are made of same material then we will use only two

    identical frusta arranged back to back, and hence

    2

    211111

    21

    kk

    kkkkkk

    m

    m

    dDdDt

    dDdDtEd

    km

    tan2

    tan2ln2

    tan.

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    Resultant member stiffness

    dDdDt

    dDdDtEdkm

    tan2

    tan2ln2

    tan.

    Ito suggested an angle

    = 45 to use, but Little reports that this overestimates theclamping stiffness. When loading is restricted to a washer-face annulus (hardened steel,

    cast iron, or aluminum), the proper apex angle is smaller. Osgood reports a range of 25

    33for most combinations.

    If is 30o

    dDdDt

    dDdDt

    Edkm

    155.1

    155.1ln

    .5774.0

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    Resultant member stiffness

    dl

    dl

    Edkm

    5.25774.0

    5.05774.05ln2

    5774.0

    If is 30o and D is taken as the waster face diameter dw.

    The washer face diameter is roughly 1.5 the major diameter of the bolt.

    ddddl

    ddddlEdk

    ww

    wwm

    tan

    tanln2

    tan.

    If the members of the joint have the same Youngs modulusE withsymmetrical frusta back to back, then they act as two identical springs

    in series (i.e. km= k/2). Using the grip as l = 2t and dwas the diameter

    of the washer face, the spring rate of the members to be

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    Use table 8-7 to read A and B

    or use graph.

    Wileman et al. FEM results for the same situation: when all members weremade of same material and hence having same Youngsmodulus.

    )/exp( lBdA

    Ed

    km A, Bare constants; l is the grip length;

    dis the major diameter of bolt.

    Resultant member stiffness

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    According to SAE or ASTM, the bolt strength is specifiedby its minimum tensile strength and its minimum proof

    strength

    Theproof load is the maximum load (force) that a bolt can

    withstand without acquiring a permanent set (i.e. first

    measurable deviation from elastic behavior, which is

    approximately equal to 0.0001 in )

    Theproof strength is the quotient of the proof load and thetensile-stress area

    Use Table 811 (page:435) for proof strength of steel

    For other materials, take Sp= 0.85 Sy

    Bolt Strength

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    Estimation of Preload, Fi

    For both static and fatigue loading

    sconnectionpermanentF0.90

    fastenersreuseds,connectionntnonpermaneforF0.75

    p

    p

    forFi

    whereFpis the proof load, obtained from the equation,

    Fp= At Sp

    HereAtis the tensile stress area obtained from Table 8-1

    Spis the proof strength obtained from Table 811

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    Load Shared by Bolt and Member

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    Tension joints- The External load

    where

    is stiffness constant of the joint

    ii

    mb

    bibb FCPF

    kk

    PkFPF

    0m

    F

    ii

    mb

    mimm FPCFkk

    PkFPF )1( 0

    mF

    mb

    m

    bmb

    b

    mbm

    PPP

    and

    kkPPor

    kkPP

    m

    m

    b

    b

    kP

    kP

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    Relating Bolt Torque to Bolt Tension

    The torque required to produce a given preload

    The dia of the washer face of a hexagonal nut is the same as the width acrossflats and equal to 1.5 times the nominal size. Therefore the mean collar dia is

    2sectan

    sectan

    22sec

    sec

    2

    ccimicci

    m

    mmi dfF

    fl

    fdFdfF

    fld

    fdldFT

    dKFdFffl

    f

    d

    dT

    ddd

    iicm

    625.0sectan

    sectan

    2

    25.12

    )5.1(dc

    Where K is called torque coefficient

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    The coefficient of friction depends upon the surface smoothness,accuracy, and degree of lubrication. On the average, bothf and fcare

    about 0.15.

    The interesting fact is thatK = 0.20 forf = fc= 0.15 no matter what

    size bolts are employed and no matter whether the threads are coarseor fine.

    Relating Bolt Torque to Bolt Tension

    Table 815 :Torque Factors K

    L d f f i ll l d d

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    Load factor for statically loaded

    tension joint with preload

    CP

    F-ASfactorloadn

    )/AF(CnPstrengthproofS

    SstrengthprooftheisofvaluelimitingThe)/AF(CP/AFboltinstresstensile

    FCPFP

    loadboltresultantF

    itp

    tip

    pb

    titbb

    iib

    b

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    Fig illustrates the connection of a cylinder head to a pressure vesselusing 10 bolts and a confined gasket seal. The effective sealing

    diameter is 150 mm. A=100, B=200, C=300, D=20, E=20 (all in

    mm). The cylinder is used to store gas at a static pressure of 6

    MPa. ISO class 8.8 bolts with a diameter of 12 mm have been

    selected. Find load factor n?

    Cylinder head is steel (E = 207 GPa )

    Cylinder is grade 30 cast iron (E = 100 GPa)

    Problem:

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    For a general case with constant preload and an externalload on per bolt is fluctuating between Pminto Pmax.

    loading.fatigueforsolveto

    equationsfailureellipticASMEandGerberGoodman,

    instressesamplitudeandmidrangeabovetheSubstitute22

    22

    minmaxminmax

    minmaxminmax

    maxmax

    minmin

    t

    i

    t

    m

    t

    bbm

    t

    a

    t

    bba

    ib

    ib

    A

    F

    A

    PPC

    A

    FF

    A

    PPC

    A

    FF

    FCPF

    FCPF

    Fatigue Loading of Tension Joints

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    Fatigue Loading of Tension JointsThe statistics indicate that the bolts under dynamic loading failed 65% in the

    thread at the nut face, 20% at the end of the thread (at the runout point) and 15%

    under the head.

    Table 817

    Fully Corrected Endurance Strengths for Bolts and Screws with Rolled Thread

    Table 817

    Fatigue Stress- Concentration Factors Kf for Threaded Elements

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    Fatigue Loading of Tension Joints

    tt

    i

    t

    i

    t

    aA

    CP

    A

    F

    A

    F

    A

    CP

    22

    1

    2

    1minmax

    t

    i

    tt

    i

    t

    i

    t

    mA

    F

    A

    CP

    A

    F

    A

    F

    A

    CP

    22

    1

    2

    1minmax

    In the common bolted joints of pressure cylinders, the

    external load varies from a lower extreme of P=0 to the

    upper extreme of P itself.

    ima The equation of the load hence is,

    In this case

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    1ut

    m

    e

    a

    S

    S

    S

    SGoodman

    1

    2

    ut

    m

    e

    a

    S

    S

    S

    S

    Gerber

    1

    22

    p

    m

    e

    a

    S

    S

    S

    S

    ellipticASME

    Fatigue Loading of Tension Joints