threaded fasteners ch 10

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Threaded Fasteners andPower Screws

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.1 (p. 386)Helical threads of pitch p, lead L and lead angle .

    Some worm and power screws

    have multiple threads

    Lead L = pitch p for single thread

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.2 (p. 386)Unified and ISO thread geometry. The basic profile of the external thread isshown.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Table 10.1b (cont.)

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Table 10.2 (p. 388)Basic Dimensions of ISO Metric Screw Threads

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    3 Classes of Fit for Screw Threads

    Class 1

    Loosest fit and largest tolerances

    Class 3

    Tightest fit and smallest tolerances

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.4 (p. 389)Power screw thread forms. [Note: All threads shown are external (i.e., on thescrew, not on the nut); dm is the mean diameter of the thread contact and is

    approximately equal to (d+ dr)/2.]

    Difficult tomanufacture

    High axial loadcarrying capacity

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.5 (p. 391)Weight supported by three screw jacks. In each screw jack, only the shaded

    member rotates.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.6 (p. 391)Screw thread forces.

    Kinematics:: tanm

    L

    d

    =

    Infinitesimal portion of nut

    q = tangential force, w = portion of total axial force

    W, n = normal force, f = friction coefficient,fn = friction force, q dm/2 = torque applied to nutsegment

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Equilibrium Yields Torque Eq. In tangential direction

    In axial direction

    Combine and solve for q

    Torque

    cos cos sin 0nq fn n =

    sin cos cos 0nw fn n + =

    cos cos sin

    cos cos sin

    n

    n

    fq w

    f

    +=

    cos cos sin

    2 2 cos cos sin

    m m n

    n

    d Wd f T Q

    f

    += =

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Torque (cont.) Using kinematic relationship

    If application has bearing surface or thrust collar

    For square thread or ACME thread cosn is nearly 1:

    For lower load, reverse signs on q and friction force fn

    cos

    2 cos 2m m n c c

    m n

    Wd f d L Wf d T

    d fL

    += +

    2 2m m c c

    m

    Wd f d L Wf d Td fL

    += +

    cos2 cos

    m m n

    m n

    Wd f d LTd fL

    +=

    cos

    2 cos 2 2 2

    m m n c c m m c c

    m n m

    Wd f d L Wf d Wd f d L Wf d T

    d fL d fL

    = + = +

    + + S uare

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.7 (p. 394)Comparison of thread angles measured in axial and normal planes ( and n).

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Overhauling and Self-Locking Self-locking screw: sufficient friction so that

    positive torque required to lower the load Overhauling screw: low enough friction so that

    axial load will cause screw to turn

    Neglecting collar friction

    Beware of vibration that can reduce f, and selflocking screw no longer locks!

    cos= tan (square thread)n

    m m

    L Lf

    d d

    =

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Efficiency of Power Screws

    Output work by power screw for one turn =

    WL

    Input work = T = 2

    Efficiency = output work/input work

    cos cos tan

    cos cos cot

    m n n

    m m n n

    d fL f Le

    d fd L f

    = =

    + +

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.8 (p. 396)

    Efficiency of Acme screwthreads when collar friction isnegligible. (Note: Values for

    square threads are higher by

    less than 1 percent.)

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.9 (p. 397)Ball bearing screw assembly with a portion of the nut cut away to show

    construction. (Courtesy Saginaw Steering Gear Division, General Motors

    Corporation.)

    Very low coefficient of friction due to mostly rolling contact-

    usually overhauling screw

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.11 (p. 400)Force flow for a bolt in tension.

    Bearing stress on thread = P/A where

    ( )2 2 / 4iA d d=

    t/p = no. of threads in contact

    ( )2 24

    i

    P p

    td d

    =

    This is average value of

    Bearing stress for the threads

    Thread 1 carries more load. Why?

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    To distribute load more evenly overthreads

    Make the nut out of softer material than

    the thread Manufacture threads of nut with slightly

    greater pitch than bolts

    Modify nut design

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.12 (p. 402)A special nut provides more nearly equal distribution of load amount threads incontact.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Thread stripping stress

    Stripping due to shear failure. Shear area for ISOthread:

    where t = nut height, d = diameter of shear fracturesurface

    For balance between bolt tensile failure and nut

    thread shear failure

    If made of same material Ssy = 0.58 Sy, so

    Nut is usually softer, so t = (7/8) d is standard

    ( )0.75A d t=

    ( ) ( )2

    0.9 S = d 0.75 S4

    t y y syF A S d d

    = =

    0.47t d=

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.15 (p. 404)Basic threaded fastener types.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.16 (p. 405)Some common screw (and bolt) head types.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.17 (p. 405)"Tamper-resistant" screw heads.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Table 10.4 (p. 407)Specifications for Steel Used in Inch Series Screws and Bolts

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Table 10.5 (p. 408)Specifications for Steel Used in Millimeter Series Screws and Bolts

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.18 (p. 409)Bolt loads and stresses that are due to initial tightening of a nut. M= 0 for the

    bolt and nut assembly shown, that is, T1 = T2 + T3 + T4 (where T1 = nut wrench

    torque). T2 = nut face friction torque = fFira(where ra is the effective radius of nutface friction forces). T3 = bolt head friction torque fFirh(where rh is the effectiveradius of bolt head friction forces). T4 = wrench torque required to keep bolt headfrom turning. Note that T4 = 0 if fFirh> T1T2.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.19 (p. 409)Bolt tension versus elongation, resulting from tightening by torquing versus directtensioning, and for black oxide versus galvanized surfaces [5]. Note: Directtension is produced by hydraulic loading; hence, no torsional stresses are

    produced.)

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.20 (p. 412)Common types of lock washers.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.21 (p. 412)(a) Slotted and (b) castle nuts. Each is also shown with a drilled bolt and cotter pin.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.22 (p. 412)Examples of free-spinning locknuts.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.23 (p. 413)Examples of prevailing-torquelocknuts. ( Courtesy SPSTechnologies, Inc.)

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.24 (p. 414)Free-body study of bolt tensile loading.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.25 (p. 414)Fband Fcversus Fe per bolt for soft clamped membersrigid bolt.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.26 (p. 415)Fband Fcversus Feper bolt for

    rigid clamped memberssoft bolt.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.27 (p. 416)Force relationships for bolted connections.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.28 (p. 417)One method for estimating the effective area of clamped members (forcalculating kc). Effective area Ac is approximately equal to the average area of

    the dark grey section.

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    Fundamentals of Machine Component Design, 4/Eby Robert C. Juvinall and Kurt M. MarshekCopyright 2006 by John Wiley & Sons, Inc. All rights reserved.

    Figure 10.29 (p. 418)Examples of nonintended bolt bending.