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    8. SENSORS

    8.2. POSITION AND SPEED MEASUREMENT

    (1) Proximity Sensors and Switches

    Magnetic, electrical capacitance, inductance, and eddy current methods are used.

    Photoemitter-detector pair: interruption or reflection of a light beam is used to detect an

    object in a noncontact manner as illustrated in Fig. 8.1.

    Applications of proximity sensors and limit switches: counting moving objects (e.g., cans

    on a convey belt), and limiting the traverse of a mechanism.

    Switches are characterized by the number of poles (P) and throws (T) and whether

    connections are normally open (NO) or normally closed (NC).

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    (2) Potentiometer

    Variable resistance device (a wiper makes contact with a resistive element, and as the

    contact point moves, the resistance between the wiper and end leads of the device changes).

    Through voltage division, the change in resistance can be used to create an output voltage

    that is proportional to the input displacement.

    (3) Linear Variable Differential Transformer (LVDT)

    Operation Thoery

    Transducer for measuring linear displacements.

    It consists of primary and secondary windings and a movable iron core.

    As with any transformer, the voltage of the induced signal in the secondary coil is linearly

    related to the number of coils, i.e.,in

    out

    in

    out

    N

    N

    V

    V= .

    As the core is displaced, the number of coils in the secondary coil changes linearly.

    Therefore the amplitude of the induced signal varies linearly with displacement.

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    With two secondary coils connected in series-opposing configurations, the output signal

    includes both the magnitude and direction of the core motion.

    At the null position (midpoint in the cores position), the voltage induced in each coil will

    be of the same amplitude and 180o

    out of phase, producing a null output.

    As the core moves from the null position, the output amplitude will increase a proportional

    amount over a linear range around null.

    Demodulation and Low-pass filter

    The diode bridges in this circuit produce a positive or negative rectified sine wave

    depending on what side of the null position the core is on.

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    A low-pass filter is used to convert the rectified output into a smoothed signal. The cutoff

    frequency of the low-pass filter should be higher than that of the core motion (at least 10

    times the maximum expected frequency of the core motion).

    Characteristics

    Advantages: accuracy over the linear range, an analog output that may not require

    amplification, and insensitivity to wide ranges in temperature.

    Disadvantages: limited range of motion and limited frequency response.

    (4) Digital Optical Encoder

    Encoders have both linear and rotary configurations.

    The absolute encoder where a unique digital word corresponds to each rotational position

    of the shaft, and the incremental encoder, which produces digital pulses as the shaft rotates,

    allowing measurement of relative position of shaft.

    Rotary encoders are composed of a glass or plastic code disk and photoemitter-detector

    pairs. As redial lines in each track interrupt the beam between a photoemitter-detector pair,

    digital pulses are produced.

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    Absolute Encoder

    Producing a digital word that distinguishes Ndistrict positions of the shaft. For example, if

    there are 8 tracks, the encoder is capable of producing 28=256 district positions or angular

    resolution of 1.406o

    (360o/256).

    Gray and binary codes for numerical encoding of the absolute encoder.

    [4-bit Gray code] [4-bit Binary code]

    For the gray code, the uncertainty during a transition is only one count, unlike with the

    binary code, where the uncertainty could be multiple counts.

    The gray code provides data with the least uncertainty, but the binary code is the preferred

    choice for direct interface to computers.

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    A simple circuit to convert from gray to binary code (binary bit (iB ), gray bit ( iG ), and

    is the exclusive OR gate):

    01012123233 ,,, GBBGBBGBBGB ====

    Incremental Encoder

    It consists of two tracks and two sensors whose outputs are called channels A and B.

    The A and B channels are used to determine the direction of rotation by assessing which

    channel leads the other. The signals from the two channels are a 1/4 out of phase with

    each other and are known as quadrature signals.

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    The third channel, called INDEX, yields one pulse per revolution, which is useful in

    counting full revolution. It also useful as a reference to define a home base or zero position.

    There are two separate tracks for the A and B channels, but a more common configuration

    uses a single track with the A and B sensors offset a 1/4 cycle on the track to yield the same

    signal pattern.

    Decoder circuits: A= with B=1 implies a CW pulse, and B= with A=1 implies a CCW

    pulse, in the 1X mode. The D flip-flops decode whether the shaft is rotating CW or CCW,

    and this information is used to drive an up-down counter to keep the current pulse count.

    An incremental encoder can be used in conjunction with a limit switch to define absolute

    position relative to some home position defined by the switch.

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    8.3. STRESS AND STRAIN MEASUREMENT

    - Stress, force, pressure and temperature can be determined from strain measurements, i.e.,

    the electrical resistance strain gage.

    (1) Electrical Resistance Strain Gage

    The metal foil strain gage illustrated in Fig. 8.17 consists of a thin foil of metal (usually

    constantan) and etched in a grid pattern onto a thin plastic backing material (usually

    polyimide). The foil pattern is terminated at both ends with large metallic pads for allowing

    leadwires to be attached with solder. The size of gage is typically 5mm to 15 mm long.

    The gage is adhesively bonded directly to the surface of a mechanical component, usually

    with epoxy.

    Fig. 8.17 Metal foil gage.

    When the component is loaded, the resistance of the metal foil changes, and if this

    resistance change is measured accurately, the strain on the surface of the component can be

    determined in the following ways:

    The metal foil grid lines in the active portion of the gage can be approximated by a single

    rectangular conductor. The total resistance is given by

    A

    LR

    =

    where is the foil metal resistivity, L is the total length of the grid lines, and A is the

    cross-sectional area.

    To see how the resistance changes under deformation, we need to take the differential of

    the above equation.

    ALR lnlnlnln += AdALdLdRdR //// += (Eq. 8.4)

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    The resistance increase ( 0>dR ) with increased resistivity and increased length, and

    decreases with increased cross-sectional area.

    The cross-sectional area and the area differential are

    whA = w

    dw

    h

    dh

    hw

    dwhdhw

    A

    dA+=

    +=

    From the Poissons Ratio (see Appendix 2),

    L

    dL

    h

    dh= and

    L

    dL

    w

    dw= axial

    L

    dL

    A

    dA 22 ==

    where axial is the axial strain. When the conductor is elongated ( 0>axial ), the cross-

    sectional area decreases ( 0/

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    (2) Measuring Resistance Changes with a Wheatstone Bridge

    - It consists of a four-resistor network excited by a dc voltage, in order to measure small

    changes in resistance.

    Static Balanced Mode

    2R and 3R are precision resistors, 4R is a precision potentiometer with an accuratescale for displaying the resistance value, and

    1R is the strain gage resistance.

    To balance the bridge, the variable resistor is adjusted until the voltage between nodes A

    and B is zero.

    In the balanced state, the voltages at A and B must be equal so

    2211 RiRi = (Eq. 8.14)

    With the high-input impedance voltmeter,

    41

    41RR

    Vii ex

    +== , and

    32

    32RR

    Vii ex

    +== .

    Substituting these expressions into Eq. 8.14 gives

    3

    2

    4

    1

    R

    R

    R

    R= .

    So, we can calculate the unknown resistance 1R as (the result is independent of exV )

    3

    241

    R

    RRR =

    Dynamic Deflection Mode

    The changes in the strain gage resistance 1R that occur when the mechanical component

    is loaded can be determined from changes in the output voltage.

    The output voltage is expressed in terms of the resistor currents as

    324122110RiRiRiRiV +==

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    The excitation voltage can be related to the same current as

    )()(322411

    RRiRRiVex

    +=+=

    Eliminating the currents from these equations results in

    ++= 322

    41

    10RR

    R

    RR

    RVV ex

    When the bridge is balanced,0V is zero and 1R has a known value. When 1R changes

    value, the voltage change0

    V can be related to the change in resistance1

    R . To find

    this relation, we can replace 1R by 11 RR + and 0V by 0V .

    +

    ++

    +=

    32

    2

    411

    110

    RR

    R

    RRR

    RR

    V

    V

    ex

    1

    132

    20

    32

    20

    1

    4

    1

    1

    +

    ++

    =

    RR

    R

    V

    V

    RR

    R

    V

    V

    R

    R

    R

    R

    ex

    ex

    By measuring the change in the output voltage 0V , we can determine the gage resistance

    change 1R .

    Leadwire Effects

    When using a strain gage located far from the bridge circuit, each of the leadwire

    resistances R add to the resistance of the strain gage. The problem is that if the leadwire

    temperature changes, it will cause changes in the resistance of the bridge.

    As shown in Fig. 8.22b, a 3-wire connection can solve this problem. Equal resistances are

    added to adjacent branches in the bridge so the effects of changes in the leadwire

    resistances offset each other.

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    Fig. 8.22 Leadwire effects in 1/4 bridge circuit.

    Temperature Compensation

    In addition to temperature effects in leadwires, temperature changes in the actual strain

    gage can cause significant changes in resistance.

    A method for eliminating this effect is to use a 1/2 bridge circuit where two of the four

    bridge legs contain strain gages.

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    (3) Measuring Different States of Stress with Strain Gages

    Uniaxial Stress (1 strain gage)

    When a component is loaded only in one direction in tension and compression.

    By measuring the strain x , the stress is known from Hooks Law to be

    xx E = . The axial stress in the bar

    x is given by

    A

    Px=

    where A is the bars cross-sectional area.

    The force P can be determined from the strain gage measurement:

    xAEP =

    Biaxial Stress (2 strain gages)

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    When a component is loaded in two orthogonal direction in tension or compression.

    By measuring the strainsx and y , the stresses in the tank shell can be determined by

    EE

    yx

    x

    = and

    EE

    xy

    y

    =

    Solving for the stress components gives

    )(1 2

    yxx

    E

    +

    = and )(

    1 2xyy

    E

    +

    = .

    For a thin-walled pressure vessel (i.e., t/r < 1/10), the stresses are given by

    t

    prx= and

    t

    pry

    2= .

    The pressure of vessel can be calculated by

    )()1(2 yx

    x

    r

    tE

    r

    tp

    +== or )()1(

    222 xy

    y

    r

    tE

    r

    t

    p

    +== .

    General Planar Stress (3 strain gages)

    For uniaxial and biaxial loading, we already know the directions of principal stresses.

    However, when the loading is more complex or when the geometry is more complex, we

    have to use three gages in three different directions.

    An assembly of strain gages is referred to as astrain gage rosette.

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    (4) Force Measurement with Load Cells

    A load cell is a sensor used to measure a force. It contains an internal flexural element,

    usually with several gages mounted to its surface. The flexural elements shape is designed

    so that the strain gage outputs can be related to the applied force.

    A typical connection is that

    Strain gage (or load cell) Amplifier Low-pass filter A/D Converter.

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    8.4. TEMPERATURE MEASUREMENT

    (1) Liquid-in-Glass Thermometer

    (2) Bimetallic Strip

    It is composed of two or more metal layers having different coefficients of thermal

    expansion. So, the deflection is related to the temperature of the strip.

    It is used in household thermostats where the mechanical motion of the strip makes or

    breaks an electrical contact to turn a heating or cooling system on or off.

    (3) Electrical resistance Thermometer

    Resistance Temperature Device (RTD)

    It is constructed of metallic wire wound around a ceramic or glass core and hermetically

    sealed.

    The resistance-temperature relationship is approximated by

    )](1[ 00 TTRR += .

    The most common metal used in RTDs is platinum, and the operating range for a typical

    platinum RTD is 220oC to 750

    oC.

    Thermistor

    It is a semiconductor device whose resistance changes exponentially with temperature

    given by

    =)

    11(

    00TTeRR

    The accuracy of thermistors is better than that of RTDs, but thermistors have much

    narrower operating ranges than RTDs.

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    (4) Thermocouple

    Two dissimilar metals in contact form a thermoelectric junction that produces a voltage

    proportional to the temperature of the junction known as the Seebeck effect.

    The wires of metals A and B form junctions at different temperatures1

    T and2

    T , resulting

    in a potential V that can be measured. The thermocouple voltage V depends on the

    metal properties of A and B and the difference between the junction temperatures1T and

    2T given by

    )(21 TTV = where is called the Seebeck coefficient.

    A standard configuration is shown in Fig. 8.40. The reference junction is used to establish a

    temperature reference.

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    8.5. VIBRATION AND ACCELERATION MEASUREMENT

    Accelerometer

    It detects acceleration along one axis and is insensitive in orthogonal directions.

    As a position transducer, strain gages or piezoelectric elements converting vibration into a

    voltage signal are used.

    Through the frequency response analysis, we can relate the displacement transducer output

    to acceleration of the object.

    The relative displacementrx between the seismic mass ( 0x ) and the object ( ix ) is

    defined asirxxx = 0 .

    The equation of the motion for the seismic mass is

    0xmFF bk &&= 0xmxbkx rr &&& = )( irrr xxmxbkx &&&&& +=

    irrrxmkxxbxm &&&&& =++

    whererik

    kxxxkF == )(0

    ,ribxbxxbF &&& == )(

    0and

    irxxx &&&&&& +=

    0.

    Referring to the analysis of a second order system in Chapter 4, the amplitude ratio and

    phase angle can be obtained as

    2/12

    2

    22

    2

    41

    )/(

    +

    =

    nn

    n

    i

    r

    X

    X

    and

    =

    2

    1

    1

    2

    tan

    n

    n

    where the input and output displacements are )sin()( tXtxii

    = and

    )sin()( += tXtx rr .

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    To relate the output displacement signal rx to the input acceleration ix&& , differentiate the

    displacements:

    )sin()( 2 tXtx ii =&& and )sin()(2 += tXtx rr&&

    Rearranging the amplitude ratio with the amplitudes of the input and output acceleration

    gives

    2/12

    2

    22

    2

    2

    41

    1)(

    +

    ==

    nn

    i

    nra

    X

    XH

    .

    If we design the accelerometer so that )(aH is nearly 1 over a large frequency range,

    then the input acceleration amplitude is given directly in terms of the relative displacement

    amplitude scaled by a constant factor 2n :

    rni XX )(amplitude,onAccelerati22 =

    The largest frequency range resulting in a unity amplitude ratio occurs when the damping

    ratio is 0.707 and when the natural frequency n is as small as possible. We can

    make the natural frequency, mkn /= , large by choosing a small seismic mass and a

    large spring constant.

    Vibrometer

    Instead of measuring acceleration, this device measures displacement.

    The displacement ratio can be defined asi

    rd

    X

    XH =)( . The input displacement amplitude

    iX is related to the measured relative displacement amplitude rX as

    r

    d

    ri X

    H

    XX =

    )(

    where )(dH is nearly 1 over a large frequency range.

    As seen in Fig. 8.47, the largest frequency range resulting in a unity amplitude ratio occurs

    when the damping ratio is 0.707 and when the natural frequency n is as small as

    possible.

    We can make the natural frequency small by choosing a large seismic mass and a small

    spring constant. This explains the large size of seismographs used to measure the earths

    displacement during an earthquake.

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    Piezoelectric Accelerometers

    As a displacement sensor, high quality accelerometers use a piezoelectric crystal, a

    material whose deformation results in charge polarization across the crystal. In a reciprocal

    manner, application of an electric filed to a piezoelectric material results in deformation.

    An equivalent circuit for a piezoelectric crystal is shown in the following figure. The

    crystal is effectively a capacitor and a charge source Q generating charge across the

    capacitor plates proportional to the deformation of the crystal. By a Thevinin equivalent

    circuit, the open circuit voltage V is equal to the charge (typically in pico-coulomb)

    divided by the capacitance (typically in the pico-farad range):

    pC

    QV =

    The sensitivity of the accelerometer is the ratio of the charge output to the acceleration of

    the housing expressed in pC/g, (rms pC)/(rms g), or (peak pC)/(peak g), where g is the

    gravity acceleration.

    (read Ch 8.6 and 8.7)