Ch3 Torsion Lecture

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    Topic 3: TORSION1. Introduction

    2. Stresses in Elastic range3. Angle of twist

    4. Design transmission shafts

    5. Thin-wall hollow shafts

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    1. Introduction

    - Members subjected to loads along the longitudinal axes

    (Axial deformation)

    - Members subjected to torsional loads twisting the

    members about their longitudinal centroid axesare

    considered in this topic.

    - Examples: a lug-wrench, power transmission shaft

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    - A lug-wrench:

    + A lug-wrench shaft AB, arm CD

    + Apply equal and opposite forces (P) to ends of CD

    AB is a torsion member

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    Sign convention:

    + Torque T(x): right-hand-rule sense

    + Angle of rotation, (x)

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    - Power transmission shaft:

    + Turbine exerts torque T on the shaft

    + The shaft transmits T to the generator+ Generator creates an equal & opposite torque T

    Generator

    Rotation

    Turbine

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    2. Stresses in Elastic range

    Shear stress in shaft:

    How is torque transferred through shaft?An element dA distance from the center of the shaft has

    shear force dF.

    For equilibrium: = 0 =

    Since dF = dA = ()= T

    Shear stress distribution?

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    Shaft deformations:

    Square shaft: wrapped under tension, cross section do not

    remain plane.

    Circular shaft: Every cross section remains plane and

    undistorted.

    - Circumferential lines remain in a plane after deformation- Longitudinal lines: Parallel to the axis become helical

    - Right angleABC : Shear deformation

    - : Torsional deformation

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    Consider a circular shaft attached to a fixed support.

    - Apply torque T: + Shaft will twist

    + Free end will rotate through angle

    - By observation: + T

    + L

    Relationship of , T, L?

    Shear stress distribution?

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    Shearing strain in circular shaft:

    Consider a shaft of length L, radius c,

    angle of twist .

    AA = L= =

    , [rad]

    is proportional to and

    varies linearly with the distance

    from the axis of the shaft.

    max

    =

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    Stresses in the elastic range:

    We have: =

    and max=

    =

    From Topic 2: = G

    G= G

    =

    As long as the yield strength is not exceeded, varies

    linearly to the distance from the axis of the shaft.

    min

    =

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    Recall that ()= T

    T =

    T =

    .

    J = : the polar moment of inertia of the crosssection with respect to its center O.

    max=

    and =

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    + A solid cross section of radius r:

    dJ = dA = 2udu

    J =

    2

    = 2

    3

    J =

    4 =

    3

    + A tubular shaft of outer radius r0and inner radius ri:

    =

    4

    4

    Example 1:

    a/ Tmax=? If max= 120 Mpa

    b/ min= ?

    Solution: T =

    min=

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    Example 2:

    Determine maxin shaft AB, BC.

    Solution:

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    Axial shear components:

    A torque applied to a shaft shearing stresses on the face

    perpendicular to the axis.

    Equilibrium equal stresses on planes containing the axis.

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    Normal stresses due to Torsion:

    - Element a: pure shear

    - Element b:

    Normal stress, shear stress or

    combination of both.

    - Consider an element at 45to the

    shaft axis:

    F = 2(maxA0) cos45= maxA0 2

    45 =

    =

    = max

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    Torsion failure modes:

    When subjected to torsion:

    + Ductile specimen breaks along a

    plane of maximum shear.

    + Brittle specimen breaks along planes perpendicular to the

    direction in which tension is a maximum.

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    - Shaft deformation: + Shear deformation

    + Torsional deformation

    - Strain: Shearing strain max=cL

    - Stress: max=Tc

    J and =

    TJ

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    3. Angle of twist

    max=

    max=

    In the elastic range: = G

    = G

    =

    - For shaft with cross-section changes:=

    Each segment has constant cross section an torque.

    - If cross section changes continuously:

    d=

    =

    ()

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    Gear assembly:

    E/B= E- B=

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    Example 3:

    rA= 2rB Apply T at E

    Determine E?

    TAD= 2T

    A=

    =

    CC = CC rAA= rBB

    B= (rA/rB) A= 2A =4

    E= B + E/B=4

    +

    = 5

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    Example 4:

    Shaft ABC with d = 60 mm

    is supported by 2 journal

    bearings.

    Shaft EH with d = 80 mm,

    is fixed at E and supported

    by a bearing at H.

    If A/C= 0.04 rad, determine T1and T2?

    Solution:

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    Example 4:

    d = 40 mm.

    Determine B/A(rad) =?

    Solution:

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    Comparison of axial and torsion:

    4 D i f T i i h ft

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    4. Design of Transmission shaft:

    - Select the shaft material (G) and cross section (J) to meet

    performance specifications (power - P and speed - ) without

    exceeding the allowable and allowable .Step 1: Determine T? From dynamics: P = T= T(2f) T =

    SI units: T: torque [N.m]

    P: power [N.m/s] [W]: angular velocity (rad/s)

    f: frequency of rotation in Hz

    US units: f [rpm], 1 rpm =

    1

    6HzP [hphorsepower]

    1 hp = 550 ft.lb/s (6600 in.lb/s) = 746 W

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    Step 2: Select a material (set all)

    Design requirement: max=

    all

    Step 3: Find shaft cross section?

    If considering the allowable angle of twist: all

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    Example 5:

    P = 16 hp from motor A machine tool D

    Motor A: f = 1260 rpm

    all= 8 ksi

    Determine dABand dCD?

    Solution:

    all= 8 ksi = 8 x 103

    (lb/in2

    )P = 16 hp = 105600 in.lb/s

    f = 1260 rpm =16

    6= 21 Hz

    T = = 156..1 = 800.72 (lb.in)

    max=.

    alldAB0.798 [in.]

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    3

    =

    5TCD= 1334.53 (lb.in)

    max=

    .

    alldCD0.947 [in.]

    Example 6:

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    Example 6:

    dAB= dCD;

    max80 Mpa,

    D1.5; G = 70 Gpa

    Determine d AB= dCD= ?

    Solution:

    Design based on allowable stress:

    =.

    =

    max =.

    =

    max

    TAB = rB.F

    TCD= rC.F TAB=.

    = 2500 (N.m)

    dAB= 59.6 mm

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    Design based on allowable angle of twist:

    D= D/C+ C =.

    + C1.5

    C rC= B rBC

    dAB= 62.9 mm

    Design must use the lager value for d: d = 62.9 mm

    St ti ll d t i t h ft

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    Statically determinate shaft:

    Example 7:

    a/ Determine T1, T2: = 0

    TCT2= 0 TC+ TBT1= 0

    b/ Determine C, B

    - Torque-twist behavior: 1= 11 =

    1=

    1 =

    - Geometry of deformation: = + ;

    = 1+ =1

    St ti ll i d t i t h ft

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    Statically indeterminate shaft:

    The unknown torques exceeds the number of applicable

    equilibrium equations.

    - Step 1: Write equil. eqs.

    - Step 2: Formulate compatibility eqs.

    - Step 3: Use torque-displacement

    eqs. to relate and T.

    Example 8:

    E ilib i

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    - Equilibrium eqs:

    TA= -T1

    T1T2= TB

    TC= T2

    - Element torque-twist behavior:

    1

    = 1

    1

    =

    1

    =

    =

    T

    2

    - Geometry of deformation:

    =1+ = 0

    Results: T1,

    T2are determined

    1=

    3 =

    3

    - Determine rotation angle B

    =1 =

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    1/

    a/ Determine expressions of

    max1

    , max2,

    max3

    b/ B= ?

    2/

    Problem 3.53 in Mechanics of Materials, 6thedition, Beer

    and Johnston.

    5 Thi ll d h ll h ft

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    5. Thin-walled hollow shafts

    Consider a thin-walled circular hollow shaft with inner

    radius r1, outer radius r2, thickness t = r2r1, and median

    radius rm= 1(r1+ r2)

    The stress distribution for a circular shaft increases linearly

    as we move from the center axis to the surface of the

    member.

    =

    =

    where J =

    (

    4 1

    4)

    Write r1and r2in terms of rm:

    r2= rm+ t/2

    r1= r

    mt/2

    4 4

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    J =

    +

    4

    4

    t2

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    The average force per unit length on the member cross-

    section is: q = mt

    where q is the shear flow

    The total torque can be estimate as:

    T = shear flow x total length x moment arm

    T = (mt)(2rm)(rm)

    Therefore: m=