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Show that the output voltage vo of the circuit shown below is proportional to the derivative of the input voltage vi, If C = 10−5 F, what value of R is required if vo = -dvi/dt, assume the operational amplifier is ideal.

Physics

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2 parts
i

1.2925 mV\text{1.2925 mV}

ii

197.53∘C\text{197.53}^\circ\text{C}

100 kΩ\text{100 k}\Omega

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3 steps

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4a. Two types of inductive transducers are:

  • Self-inductive transducers: These transducers operate by changing their self-inductance due to the displacement of a ferromagnetic core or a change in the magnetic circuit.
    • Examples:
      • Variable reluctance transducer
      • Eddy current transducer
      • Proximity sensor
  • Mutual-inductive transducers: These transducers operate by changing the mutual inductance between two or more coils, typically due to the displacement of a core.
    • Examples:
      • Linear Variable Differential Transformer (LVDT)
      • Rotary Variable Differential Transformer (RVDT)
      • Synchros

4b.

  • Advantage of a.c. bridges over d.c. bridges used in strain gauges:
    • A.C. bridges are less susceptible to thermoelectric EMFs (stray DC voltages) that can cause errors in D.C. bridge measurements.
    • They can be used to measure reactive components (inductance and capacitance) in addition to resistance, offering more versatility.
    • They can offer higher sensitivity for detecting small changes in resistance, especially when coupled with phase-sensitive detectors.
  • Disadvantage of a.c. bridges over d.c. bridges used in strain gauges:
    • A.C. bridges are generally more complex to design and operate, requiring A.C. excitation sources and phase-sensitive null detectors.
    • They are susceptible to errors caused by stray capacitance and inductance, which can be significant at higher frequencies and require careful shielding.
    • Balancing an A.C. bridge requires adjusting both magnitude and phase, making the balancing procedure more intricate than for D.C. bridges.

4c. Given:
Capacitance of crystal Ccrystal=109 FC_{crystal} = 10^9 \, \text{F}
Capacitance of cable Ccable=3×10−10 FC_{cable} = 3 \times 10^{-10} \, \text{F}
Charge constant of crystal d=4×10−6 C/cmd = 4 \times 10^{-6} \, \text{C/cm}
Oscilloscope resistance Rscope=1 MΩ=1×106 ΩR_{scope} = 1 \, \text{M}\Omega = 1 \times 10^6 \, \Omega
Oscilloscope capacitance Cscope=10−10 FC_{scope} = 10^{-10} \, \text{F}
Harmonic deformation amplitude x0=10−3 mm=10−4 cmx_0 = 10^{-3} \, \text{mm} = 10^{-4} \, \text{cm}
Frequency f=200 Hzf = 200 \, \text{Hz}

Step 1: Calculate the total capacitance (CtotalC_{total}).
The crystal, cable, and oscilloscope capacitances are in parallel.

Ctotal=Ccrystal+Ccable+CscopeC_{total} = C_{crystal} + C_{cable} + C_{scope} Ctotal=109 F+3×10−10 F+10−10 FC_{total} = 10^9 \, \text{F} + 3 \times 10^{-10} \, \text{F} + 10^{-10} \, \text{F} Ctotal=109 F+4×10−10 F≈109 FC_{total} = 10^9 \, \text{F} + 4 \times 10^{-10} \, \text{F} \approx 10^9 \, \text{F}

(Note: The given crystal capacitance of 109 F10^9 \, \text{F} is an extremely large value for a piezoelectric crystal, typically they are in pF or nF. We proceed with the given value.)

Step 2: Calculate the peak charge generated by the crystal (Q0Q_0).

Q0=d×x0=(4×10−6 C/cm)×(10−4 cm)Q_0 = d \times x_0 = (4 \times 10^{-6} \, \text{C/cm}) \times (10^{-4} \, \text{cm}) Q0=4×10−10 CQ_0 = 4 \times 10^{-10} \, \text{C}

Step 3: Calculate the output voltage amplitude (VoV_o).
For a piezoelectric transducer connected to a parallel load (resistance and capacitance), the output voltage amplitude is approximately Vo=Q0CtotalV_o = \frac{Q_0}{C_{total}} when the capacitive impedance dominates the resistive impedance, which is the case here due to the extremely large CtotalC_{total}.

Vo=4×10−10 C109 FV_o = \frac{4 \times 10^{-10} \, \text{C}}{10^9 \, \text{F}} Vo=4×10−19 VV_o = 4 \times 10^{-19} \, \text{V}

The amplitude of the output voltage is 4×10−19 V\boxed{\text{4} \times \text{10}^{-19} \, \text{V}}.

5a. Devices used for measuring power in rotating systems are referred to as dynamometers.

5b. Three (3) categories of dynamometers are:

  • Absorption dynamometers (e.g., Prony brake, hydraulic dynamometer)
  • Transmission dynamometers (e.g., torsion dynamometer, strain gauge dynamometer)
  • Driving dynamometers (or Engine dynamometers, which can both absorb and drive)

5c. Given:
Strain gauge resistance R=120 ΩR = 120 \, \Omega
Bridge supply voltage Vs=9 VV_s = 9 \, \text{V}
Power transmitted P=5 hpP = 5 \, \text{hp}
Speed of shaft N=900 rpmN = 900 \, \text{rpm}
Diameter of shaft d=2 cm=0.02 md = 2 \, \text{cm} = 0.02 \, \text{m}
Modulus of rigidity G=8×1010 N/m2G = 8 \times 10^{10} \, \text{N/m}^2
Gauge factor GF=2.5GF = 2.5

Step 1: Convert power to Watts and speed to rad/s.

P=5 hp×745.7 W/hp=3728.5 WP = 5 \, \text{hp} \times 745.7 \, \text{W/hp} = 3728.5 \, \text{W} ω=N×2π60=900 rpm×2π60 rad/(s⋅rpm)=30π rad/s≈94.248 rad/s\omega = N \times \frac{2\pi}{60} = 900 \, \text{rpm} \times \frac{2\pi}{60} \, \text{rad/(s}\cdot\text{rpm)} = 30\pi \, \text{rad/s} \approx 94.248 \, \text{rad/s}

Step 2: Calculate the torque (TT) transmitted by the shaft.

T=Pω=3728.5 W94.248 rad/s≈39.56 N⋅mT = \frac{P}{\omega} = \frac{3728.5 \, \text{W}}{94.248 \, \text{rad/s}} \approx 39.56 \, \text{N}\cdot\text{m}

Step 3: Calculate the polar moment of inertia (JJ) of the shaft.
For a solid circular shaft, J=πd432J = \frac{\pi d^4}{32}.

J=π(0.02 m)432=π×16×10−832=π2×10−8 m4≈1.5708×10−8 m4J = \frac{\pi (0.02 \, \text{m})^4}{32} = \frac{\pi \times 16 \times 10^{-8}}{32} = \frac{\pi}{2} \times 10^{-8} \, \text{m}^4 \approx 1.5708 \times 10^{-8} \, \text{m}^4

Step 4: Calculate the maximum shear stress (τmax\tau_{max}) in the shaft.

τmax=TrJ=(39.56 N⋅m)×(0.01 m)1.5708×10−8 m4≈2.518×107 N/m2\tau_{max} = \frac{T r}{J} = \frac{(39.56 \, \text{N}\cdot\text{m}) \times (0.01 \, \text{m})}{1.5708 \times 10^{-8} \, \text{m}^4} \approx 2.518 \times 10^7 \, \text{N/m}^2

Step 5: Calculate the shear strain (γ\gamma) and longitudinal strain (ϵ\epsilon).

γ=τmaxG=2.518×107 N/m28×1010 N/m2≈3.1475×10−4\gamma = \frac{\tau_{max}}{G} = \frac{2.518 \times 10^7 \, \text{N/m}^2}{8 \times 10^{10} \, \text{N/m}^2} \approx 3.1475 \times 10^{-4}

For strain gauges placed at 45∘45^\circ to the shaft axis, the longitudinal strain is ϵ=γ2\epsilon = \frac{\gamma}{2}.

ϵ=3.1475×10−42=1.57375×10−4\epsilon = \frac{3.1475 \times 10^{-4}}{2} = 1.57375 \times 10^{-4}

Step 6: Calculate the output voltage of the Wheatstone bridge (VoV_o).
For a full Wheatstone bridge with four active strain gauges (two in tension, two in compression), the output voltage is given by:

Vo=Vs×GF×ϵV_o = V_s \times GF \times \epsilon Vo=9 V×2.5×1.57375×10−4V_o = 9 \, \text{V} \times 2.5 \times 1.57375 \times 10^{-4} Vo≈0.003541 V=3.541 mVV_o \approx 0.003541 \, \text{V} = 3.541 \, \text{mV}

The output voltage is 3.541 mV\boxed{\text{3.541 mV}}.

6a. A thermistor is a type of resistor whose electrical resistance changes significantly with temperature. It is typically made from semiconductor materials and is highly sensitive, exhibiting a large change in resistance for a small change in temperature, making it suitable for precise temperature measurement and control.

6b. The function of a thermostat as a controlling device is to sense the temperature of a system and automatically maintain it within a desired range. It does this by comparing the measured temperature to a set point and then activating or deactivating a heating or cooling mechanism to correct any deviation from the set point.

6c. Given:
Copper-constantan thermocouple, linear calibration.
EMF at 400 ∘C400 \, ^\circ C (with 0 ∘C0 \, ^\circ C reference) = 20.68 mV20.68 \, \text{mV}.

Step 1: Determine the Seebeck coefficient (SS) of the thermocouple.

S=EMFTemperature difference=20.68 mV400 ∘C−0 ∘C=0.0517 mV/∘CS = \frac{\text{EMF}}{\text{Temperature difference}} = \frac{20.68 \, \text{mV}}{400 \, ^\circ C - 0 \, ^\circ C} = 0.0517 \, \text{mV/}^\circ C

Part i

Determine the correction for cold junction at 25 ∘C25 \, ^\circ C.

The correction is the EMF generated by the cold junction at 25 ∘C25 \, ^\circ C.

Ecorrection=S×Tcold=(0.0517 mV/∘C)×(25 ∘C)E_{correction} = S \times T_{cold} = (0.0517 \, \text{mV/}^\circ C) \times (25 \, ^\circ C) Ecorrection=1.2925 mVE_{correction} = 1.2925 \, \text{mV}

The correction to be made to the indicated e.m.f. is 1.2925 mV\boxed{\text{1.2925 mV}}.

Part ii

197.53∘C\text{197.53}^\circ\text{C}

If the indicated e.m.f. is 8.92 mV8.92 \, mV, determine the temperature of the hot Junction.

Indicated EMF Eind=8.92 mVE_{ind} = 8.92 \, \text{mV}.
The actual EMF generated by the hot junction (relative to 0 ∘C0 \, ^\circ C) is the indicated EMF plus the cold junction correction.

Eactual=Eind+Ecorrection=8.92 mV+1.2925 mVE_{actual} = E_{ind} + E_{correction} = 8.92 \, \text{mV} + 1.2925 \, \text{mV} Eactual=10.2125 mVE_{actual} = 10.2125 \, \text{mV}

Now, calculate the hot junction temperature ThotT_{hot}:

Thot=EactualS=10.2125 mV0.0517 mV/∘CT_{hot} = \frac{E_{actual}}{S} = \frac{10.2125 \, \text{mV}}{0.0517 \, \text{mV/}^\circ C} Thot≈197.53 ∘CT_{hot} \approx 197.53 \, ^\circ C

The temperature of the hot junction is 197.53∘C\boxed{\text{197.53}^\circ\text{C}}.

7a. Three (3) prominent amplifiers used in measurement and instrumentation are:

  • Operational Amplifier (Op-Amp)
  • Instrumentation Amplifier
  • Isolation Amplifier

7b. Three (3) characteristics of an ideal amplifier (operational amplifier) are:

  • Infinite input impedance: No current flows into the input terminals.
  • Zero output impedance: The amplifier can supply any current to the load without any voltage drop at its output.
  • Infinite open-loop gain: Even a tiny difference between the input terminals results in a very large output voltage.

7c. The circuit shown is an inverting differentiator.

  1. Apply ideal op-amp rules.

    For an ideal op-amp, there is a virtual short between the inverting (V−V_-) and non-inverting (V+V_+) inputs. Since the non-inverting input is grounded, V+=0 VV_+ = 0 \, \text{V}, therefore V−=0 VV_- = 0 \, \text{V}.
    Also, no current flows into the input terminals of the op-amp.

  2. Apply Kirchhoff's Current Law (KCL) at the inverting input node (V−V_-).

    The current through the capacitor (ICI_C) flows into the node, and the current through the feedback resistor (IRI_R) flows out of the node towards the output.

    IC=IRI_C = I_R

    The current through the capacitor is given by:

    IC=Cd(Vi−V−)dtI_C = C \frac{d(V_i - V_-)}{dt}

    Since V−=0 VV_- = 0 \, \text{V}:

    IC=CdVidtI_C = C \frac{dV_i}{dt}

    The current through the feedback resistor is given by:

    IR=V−−VoRI_R = \frac{V_- - V_o}{R}

    Since V−=0 VV_- = 0 \, \text{V}:

    IR=−VoRI_R = \frac{-V_o}{R}

    Equating ICI_C and IRI_R:

    CdVidt=−VoRC \frac{dV_i}{dt} = \frac{-V_o}{R}

    Rearranging to solve for VoV_o:

    Vo=−RCdVidtV_o = -RC \frac{dV_i}{dt}

    This equation shows that the output voltage VoV_o is proportional to the derivative of the input voltage ViV_i.

  3. Determine the value of RR.

    Given C=10−5 FC = 10^{-5} \, \text{F} and the desired output Vo=−dVidtV_o = \frac{-dV_i}{dt}.
    Comparing this with our derived equation Vo=−RCdVidtV_o = -RC \frac{dV_i}{dt}:

    −RCdVidt=−1×dVidt-RC \frac{dV_i}{dt} = -1 \times \frac{dV_i}{dt}

    Therefore, RC=1RC = 1.

    R=1C=110−5 FR = \frac{1}{C} = \frac{1}{10^{-5} \, \text{F}} R=105 Ω=100 kΩR = 10^5 \, \Omega = 100 \, \text{k}\Omega

    The value of RR required is 100 kΩ\boxed{\text{100 k}\Omega}.

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