CONTENTS
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MEASURING INSTRUMENTS
2.1 PERMANENT MAGNET MOVING COIL (PMMC) TYPE
2.1.1 Operating Principle
2.1.2 Constructional Features
2.1.3 Torque Equation
2.1.4 Shape of the Scale
2.1.5 Use as D.C. Ammeter or as D.C. Voltmeter (Extension of Range):
2.2 ELECTRODYNAMIC (ELCTRODYNAMOMETER) TYPE
2.2.1 Construction (more to follow)
3. MOVING IRON INSTRUMENT (IRON-VANE INSTRUMENT)
3.1 CLASSIFICATION OF MOVING IRON (M.I.) INSTRUMENTS
3.2 ATTRACTION TYPE (OR SINGLE IRON TYPE)
3.3 REPULSION TYPE (DOUBLE IRON TYPE)
3.4 COMBINED ATTRACTION-REPULSION TYPE
3.4.1 Basic Principle and Construction
3.5 GENERAL TORQUE EQUATION
3.6 SHAPE OF SCALE
3.7 ADVANTAGES OF M.I. INSTRUMENTS
3.8 DISADVANTAGES OF M.I. INSTRUMENTS
Prepared by – M. R. Mohanta
MSE, BARIPADA
MEASURING INSTRUMENTS
1. MOTIVATION
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
2. MOVING COIL INSTRUMENT
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
Fig. 1(a) Suspension Type (Laboratory Type) PMMC (D’Arsonval) Movement;
(b) Light-beam and mirror arrangement
Fig. 2 Pivot & Bearing Type (Portable Type) PMMC (D’Arsonval) Movement.
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2.1.2 Constructional Features:
Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
Fig. 3 Coil and Former / Bobbin Shapes
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
2.1.3. Torque Equation:
Dimensions of a PMMC instrument are as in Fig. 4:
Fig. 4 Dimensions of a PMMC instrument.
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α = angle between the direction of magnetic field and the active coil side. This angle is 90° since the field is radial and active coil side is vertical and it moves within the radial field region (i.e., it moves within the pole-arcs).
Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
= NiAB Newton metre (1)
Since N, A, B are constants for a given instrument,
where G = NBA is ‘instrument constant’.
If spring control (usually used in PMMCs) is used, then controlling torque is:
where Ki = K/G = a constant
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2.1.4 Shape of the Scale:
Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
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2.1.5 Use as D.C. Ammeter or as D.C. Voltmeter (Extension of Range):
Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
Fig. 5 Basic PMMC meter in conjunction with a shunt to form an ammeter.
Fig. 6 Basic PMMC meter in conjunction with a multiplier to form a voltmeter.
Similarly, basic PMMC meter can read micro or milli volts by calibrating its scale in micro or millivolts. But, to convert it into a volt-meter (capable of reading >100 mV, say), suitable high resistance (called multiplier) to be connected in series with meter (Fig. 6).
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2.2 ELECTRODYNAMOMETER (OR DYNAMOMETER OR ELECTRODYNAMIC) MOVING COIL TYPE:
Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
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2.2.1 Construction:
Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech., Ph.: 9416351300, Email: jssain@rediffmail.com
Fig. 7 Electrodynamic Instrument
Fig. 8 Schematic diagram of electrodynamic movement.
… More to follow
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3. MOVING IRON INSTRUMENT (IRON-VANE INSTRUMENT)
3.1 CLASSIFICATION OF MOVING IRON (M.I.) INSTRUMENTS
3.2 ATTRACTION TYPE (OR SINGLE IRON TYPE) :
Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
Fig. 9 Basic set-up to demonstrate principle of operation of Attraction Type Moving Iron Instrument.
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
Fig.10 Construction of Attraction Type Moving Iron Instrument.
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3.3 REPULSION TYPE (DOUBLE IRON TYPE):
Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
Fig. 11 Basic set-up to demonstrate the principle of operation of Repulsion Type Instruments
S
N
+ –
A C
B D
Soft iron rods
Coil
S
N
S
N
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
Two sub-types (designs) of repulsion type instruments are now discussed.
Fig. 12 Radial Vane Type (a) Front Section View Fig.13 Co-axial Vane Type (a) Front Section View
(b) Plan View (b) Plan View
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
Fig.14 Developed view of Fixed & Movable Co-axial vanes.
3.4 Combined Attraction-Repulsion Type:
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
3.5 GENERAL TORQUE EQUATION
Fig.16 Developed view of one movable and three fixed vanes.
Fig.15 Combined attraction-repulsion type (front section view).
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Now, electrical energy supplied = (voltage)x(current)x(time increment)
…
Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
So, Incremental energy supplied = (incremental voltage)x(current)x(time increment)
= eidt which, by using =n 5, becomes:
= i2dL + iLdi (6)
Now, assuming: stray capacitance neglected (this assumption not justified at high frequencies), ⟹ energy stored in electric field neglected, so energy stored only in magnetic field as (½)Li2. For the case at hand, the energy stored changes from (½)Li2 to (½)(L + dL)(i + di)2.
So, Change in stored energy = (½)(L + dL)(i2 + 2idi + di2) – (½)Li2 (neglect di2)
= (½)Li2 + Li di + (½)(dL)i2 + I di dL – (½)Li2 (neglect I di dL )
= Li di + (½)i2dL (7)
For circular motion, mechanical work done = Torque x angular displacement
(just as for linear motion, Work done = Force x covered distance)
So, Mechanical work done = (τd)idθ (8)
Where (τd)i = instantaneous deflecting torque in N-m.
From the principle of conservation of energy,
Incremental energy supplied = Increase in stored energy + Mechanical work done
So, using Eqns. 6 to 8, we have:
i2dL + iLdi = Li di + (½)i2dL + (τd)idθ
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
So, (τd)idθ = (½)i2dL
Or, (τd)i = (½)i2(dL/dθ) (9)
Instantaneous torque is a function of square of instantaneous current & will, therefore, have a non-zero +ve average value. It is a mathematical proof that M.I. instruments can be used on D.C. as well as on A.C.
In this case, i = Idc = steady D.C. current = I (say)
So, Average torque = (τd)av = (½)I2(dL/dθ) (10)
The Average torque = (τd)av = (1/T) dt
where T = Time period of one cycle.
So, (τd)av = (1/2)(dL/dθ)
As term in square bracket ⟹, by defn., the square of RMS value of A.C. current,
So, (τd)av = (½)I2(dL/dθ) (11)
Where I = RMS value of A.C. current.
As pointed earlier, spring control is normally used, we have controlling torque,
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
τc = Kθ
where K = spring constant; N-m/rad & θ = deflection in rad.
At equilibrium (final steady) position, τc = τd
So, Kθ = (½)I2(dL/dθ)
Or, Deflection, θ = (½)(I2/K)(dL/dθ) (12)
So, steady deflection is a fn. of sq. of rms value (D.C. value in case D.C.) of current.
3.6 SHAPE OF SCALE
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
3.7 ADVANTAGES OF M.I. INSTRUMENTS
a) Robust due to their simple construction & no current-carrying moving parts.
b) Can be used both for A.C. & D.C., although not with the same accuracy.
c) Less prone to frictional errors due to their high torque to wt. ratio & as their moving system can be made light (because not to carry any current).
d) No current-carrying moving parts, so identical moving sys’s may be used for an entire range of instruments, thus M.I. instruments can be produced at less cost. Possible because for a given displacement of moving sys. (i.e., to produce a given m.m.f.), either a coil of a few turns of thick cross section, or a coil with large number of turns of thin cross section may be used.
e) Attraction type M.I. instruments usually have lower L & hence more accurate over a wider range of frequency, as compared to repulsion type M.I. instruments.
f) For repulsion type M.I. instruments, a comparatively (compared to attraction type) wider & nearly uniform scale is more easily obtainable.
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Dr. J.S. Saini, Prof., EED; Dean, Faculty of Engg. & Tech.,
Ph.: 9416351300, Email: jssain@rediffmail.com
3.8 DISADVANTAGES OF M.I. INSTRUMENTS
a) Serious errors due to hysteresis, eddy currents, freq. changes & waveform changes, thus can’t be calibrated with D.C. & used on A.C. and vice-versa. They need to be calibrated separately for D.C. & separately for each frequency of A.C. at which they are used.
b) Their scale is cramped at the lower end, giving less accurate readings at this range.
THANKS. ANY QUESTIONS PLEASE?
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