pre measuring instruments 2013
TRANSCRIPT
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Pressure above
atmospheric pressure
Ordinary pressure gage
reads difference between
absolute pressure andatmospheric pressure,
Pg
Pressure less than
atmospheric pressure
Atmospheric pressure
Ordinary vacuum gage
reads difference between
atmospheric pressure
and absolute pressure,
Pvac
Absolute pressure that is
less than atmospheric
pressure, Pabs
Absolute pressure
that is greater than
atmospheric
pressure, Pabs
Barometer reads
atmospheric pressure,
Patm
Zero pressure
Figure 1. Illustration of terms used in pressure measurements.
dead-weight pressure gages;
electrical-type pressure gages: piezoelectric pressure gages, capacitance pressure gages, strain-type pressure gages.
Here is the classification of instrumentation for pressure measurements with respect to the typeof the measured pressure:
pressure gages, for measurements of pressures above atmospheric pressure;
vacuum pressure gages, for measurements of pressures below atmospheric pressure;
vacuum manometers, for measurements of both pressures above and below atmosphericpressure;
barometers, for measurement of atmospheric pressure;
differential pressure and vacuum gages, for measurements of difference of pressures.
2. U-tube liquid filled manometers
These manometers are used for measurement of gauge pressures (up to 0.1 MPa), vacuumetricpressures (down to 0.1 MPa below atmospheric pressure) and for differential pressures of liquids
and gases. The principle is based on the static balance between the measured pressure and the
head of the liquid column. Fig. 2 shows the schematic of this manometer. A glass tube1, bended
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to the U-shape, is filled by one half of its volume with liquid 2 (water, mercury). This tube is
placed vertically, and a scale 3 (usually in mm) is attached along its height. Pressures 1P and
2P are supplied to legs of the tube, and levels of liquid in the legs change their position.
When static balance between a measuring pressure and the head of the liquid column is reached,this pressure can be evaluated according to the equation:
)( 2121 hhgHgPPP locloc +=== , (3)
where,
1P and 2P - pressures supplied to the legs of the manometer, Pa ;
1h and 2h - deviations of liquid levels from the zero point of the scale in two legs of the
manometer, m ;21 hhH += - total length of the liquid column corresponded to the measuring differential
pressure, m ;
- density of liquid filled the U-tube,3
m
kg;
locg - local gravitational acceleration, 2s
m.
We need always make two readings of the liquid level, namely, in each leg of the tube, because
in reality due to non-uniformity of the tube diameter along its length, values of 1h and 2h are
not equal. As the result of such reading the error introduced during pressure measurement will be
reduced. When this type of manometer is used for pressure measurements three cases may take
place:
1). 1P is above atmospheric pressure, atmPP =2 . In this case the manometer measures the
difference between absolute and atmospheric pressures: )( 211 hhgPP locg +== .
2). 2P is below atmospheric pressure, atmPP =1 . In this case manometer measures the
difference between atmospheric and absolute pressures: )( 212 hhgPP locvac +== .3). In this case the equation (4.3) refers to measurements of differential pressures.
Since the gravitational acceleration is used for the evaluation of pressure, then, when using U-
tube manometers, it is necessary to introduce correction which takes into account the difference
between gravitational acceleration in the place where this manometer was calibrated from thatwhere it is used.
Another source of the error is the deviation of liquid temperature in the tube from that
temperature when this manometer was calibrated. Due to thermal expansion of the liquid in thetube the volume of liquid will change and this inevitably introduces an error.
But the most common mistake is made by not correct reading the scale in respect to the meniscusof liquid in legs of the tube. Fig. 3 gives examples how operator should make readings when
using U-tube manometer with various liquids. We should always read a surface of the
meniscus in its centre. In the case with water - in the bottom, and in the case with mercury - inthe top of the meniscus. But in everyday industrial measurements the first two corrections
(gravitational and thermal) are not always used, whereas the last one (the meniscus correction)
must always be taken into account.
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0
P1P2
h2
h1
H
1
2
3
Figure 2. Liquid filled U-tube manometer.
When one measures low pressures several modifications of U-tube manometer are used,
namely, well or reservoir manometer, inclined manometer, absolute pressure gauge.
Water wets glass Mercury does not
wet glass
Figure 3. Correct reading of the U-tube manometer.
3. Bourdon and diaphragm gages3.1. Bourdon gauge
The most widely used in industry for pressure and vacuum measurements (from 20 kPa to 1000
MPa) is a pressure gauge with sensitive element made of a metallic (various stainless-steel
alloys, phosphor bronze, brass, beryllium copper, Monel, etc.) Bourdon tube 1 (see Figure 4).The tube was named after its inventor, E. Bourdon, who patented his invention in 1852. This
tube has an elliptical or oval cross-section AA and has the shape of a bended tube. When the
pressure inside the tube 1 increases, its cross-section dimension 1b also increases by the value of
1b , whereas the cross-section dimension a1 reduces its length by the value of 1a . Therefore,the tube tends to straighten (if pressure has increased) or twist (if pressure has decreased, forexample, during vacuum measurements), and the tip 2 of the tube moves linearly with applied
pressure. The movement of the tip is transmitted to the pointer3
through a mechanism4
. The
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tube tends to return to its original shape (the pointer returns to the starting position) after pressure
is removed. A relationship between the value of the tip movement x and the measuredpressure is linear, so the scale of this pressure gauge is uniform.
P
2
1
3
4
a1
a1- a1
b1
A - A
A
A
b1+ b1
Figure 4. Bourdon tube pressure gauge.
Some degree of hysteresis still exists during operation of these pressure gages, because metals
cannot fully restore their initial elastic properties. If we have two Bourdon tubes made of the
same metal, the tube with a bigger radius and a smaller thickness of the wall will have higher
sensitivity. An accuracy of a typical Bourdon-tube pressure gauge is equal to 1%, whereas a
specially designed gauge may have better accuracy which varies from 0.25 to 0.5%.
3.2. Diaphragm gauge
Another type of pressure gauge, which utilises elastic-element properties, is a diaphragmpressure gauge. These gages are used when very small pressures (from 125 Pa to 25 kPa) are to
be sensed. Fig. 5 shows a sensitive element for this type of pressure gauge.
A flexible disc 1 made of trumpet brass, or phosphor bronze, or beryllium copper, or titanium, or
tantalum, etc., is used to convert the measuring pressure to the deflection of the diaphragm.
Deflection vs pressurecharacteristic should be close to linear as much as possible. In reality for
a flat diaphragm this characteristic is non-linear. So, flat membranes are not used as sensitiveelements. To linearise this relationship special diaphragms with concentric corrugations 6 are
designed. Linearisation of a static characteristic of the membrane can be achieved by using a flat
spring 2, which is connected, to the diaphragm through the mechanism 3. The movement of themechanism 3 is transmitted by the link4 to a pointer of the gauge. The measuring pressure is
supplied to the pressure chamber5and causes the diaphragm to move upwards until the force
developed by this pressure on the diaphragm is balanced by the force acted from the spring. Toincrease the sensitivity of this type of pressure gauge, we may increase the diameter of the
diaphragm, to lengthen the spring, to change the material of the diaphragm and the spring to
more elastic, to increase the depth and the number of corrugations of the diaphragm.
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P
1
2
3
4
5
6
Figure 5. Sensitive element of a diaphragm pressure gauge.
When pressure is applied to both sides of the membrane, then the resultant reading isproportional to the differential pressure. The space above the diaphragm is connected to
atmosphere, so the diaphragm separates a measured media from the environment. In other words,
it serves as a fluid or gas barrier or as a seal assembly, thus preventing contact of corrosive andaggressive fluids with pressure elements.
Accuracy of diaphragm pressure gages varies from 1.0 to 1.5% of the span.
3.3. Bellows pressure gauge
These pressure sensitive elements are usually made of stainless steel; phosphor bronze, brass andare used for pressure measurements for pressures up to 6 MPa. Bellows sensors have large
displacement sensitivity. Figure 6 shows this type of sensor.
The effective area of a bellows can be calculated using the following formula:
4
)( 221 RRAef+
=
, (4)
When pressure is applied to the internal surface of a bellows the force is developed
according the formula: efef PAF = . (5)
4.4. Dead-weight pressure gagesThese are the most accurate pressure gages, so they are used mostly for calibration of other
pressure gages or for measurements, when high accuracy is required (for scientific purposes).The accuracy achieved may vary from 0.01 to 0.02% of the measuring pressure (these
instruments are used for calibration of dead-weight pressure gages), those with the accuracy of
0.05% are used for calibration of other types of pressure gages. The range of measured
pressures varies from 0.1 to 250 MPa. Figure 7 shows a schematic of a dead-weight pressuregauge.
A cylindrical piston 1 is placed inside a stainless-steel cylinder 2. The measuring pressure issupplied through the vent 8 to the fluid 4 of this gauge. To avoid contact of a measured media
with the fluid in the gauge, U-shape separating tubes (made of stainless steel with a thick wall)
are used. These tubes are filled by one half of their volume with mercury. The measuring
pressure spreads throughout the fluid in the dead-weight gauge system. Transformer mineral oil
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and castor oil are used for measurements of low (up to 6 MPa) and high (up to 250 MPa)
pressures, respectively. The measuring pressure by acting on the piston develops a force, whichtends to bring the piston upwards. The gravitational force developed by calibrated weights 3 can
balance this force and the piston itself. This force acts downwards. The balance should be
achieved for a certain position of the piston against a pointer 9 of the stainless-steel cylinder. A
manual piston pump 5is used to achieve approximate force balance (to increase pressure in the
system), whereas a wheel-type piston pump6
serves for accurate balancing. A Bourdon-typepressure gauge 7is used for visual reading of pressure, but not for pressure measurements in this
case.
2R2
2R1
P
a
r
Figure 6. Bellows pressure sensitive element.
1
2
3
4
5
6
7
8
2
9
Figure 7. Dead-weight pressure gauge.
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Thus measuring pressure can be evaluated using the formula:
locw
S
mmP
, (6)
where, P - measuring pressure, Pa ;
pm - mass of the piston, kg;
wm - mass of calibrated weights, kg;
locg - local gravitational acceleration, 2s
m;
pS - cross-section area of the piston, 2m .
In reality, this formula is more comprehensive in order to achieve high accuracy. Therefore,several corrections should be introduced, namely:
the correction for the variation of piston cross-section area with variation of its
temperature;
the correction which takes into account the difference between local
gravitational accelerations of the place where this dead-weight pressure gaugewas calibrated and where it is used for pressure measurements;
the buoyancy-type correction takes into account the weight of the air displaced
by the piston and calibrated weights;
we need to reduce friction of the piston inside the cylinder by spinning the
weight platform with the piston to keep the piston floating;
head of the oil should be constant in every measurement, this corresponds to a
certain position of the piston in the cylinder.
5. Piezoelectric pressure transducers
The principle of these pressure transducers is based on the well-known phenomenon, that whenan asymmetrical crystal is elastically deformed along its specific axes, an electrical charge isdeveloped on its sides. The value of this charge is proportional to the force applied to the crystal,
and, therefore, to the pressure under measurement.
Fig. 8 shows piezoelectric crystal circuit. An electrical charge developed on the sides of thecrystal is converted into a voltage-type signal using a capacitor. This voltage is proportional to
the electrical charge developed, and to the pressure to be measured. Piezoelectric sensors cannot
measure static pressures for more than a few seconds, but they have a very quick response whenmeasure dynamic pressures.
+
-
+
-
RC
P
U
Q
Figure 8. Piezoelectric pressure sensor with electrical circuit.
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Synthetically developed quartz crystals (barium titanate, lead zirconate) have similar propertiesas natural single crystal (quartz). But natural quartz still is the perfect material for manufacturing
piezoelectric sensitive elements, because it has perfect elasticity and stability, it is insensitive to
temperature variations and it has high insulation resistance.
These pressure transducers are used for measurements of hydraulic and pneumatic pulsations,flow instabilities, fuel injection, etc.
A variation of the electrical charge piezq , developed on the surfaces of a piezoelement for a
change in the input variable measured pressure, P. Now we should measure this electricalcharge. For this purpose two metal electrodes are attached to the opposite sides of a piezoelectric
crystal. Thus, a capacitor is formed. The value of capacitance of this capacitor can be evaluated
as follows:
d
AC xpiez
0= , (7)
where,
piezC - electrical capacitance of the piezoelement, F (Farad);
m
pF,85.80 = - the permittivity of vacuum, 1pF=10
-12 F;
- the relative permittivity of the material of the piezoelectric crystal,
this is the dimensionless parameter;
xA - cross-sectional area of the piezoelectric sensor in the direction,
perpendicular to the axis X, 2m ;
d - the thickness of the piezoelectric crystal in the direction,perpendicular to the axis X, m.
The relative permittivity, also called dielectric constant, for various piezoelectric materials isgiven below:
for quartz (natural piezoelectric material) 5.4= ; for tourmaline (natural piezoelectric material) 6.6= ; for lead-zirconate-titanate (man-made piezoelectric ceramic material) 1500= ; for lead metaniobate (man-made piezoelectric ceramic material) 250= .
It is also noted in the above mentioned reference, that natural piezoelectric materials have very
low charge to force sensitivity, and therefore man-made piezoelectric ceramic materials are usedas sensing elements:
charge sensitivity to force for quartzN
pC,3.2 ;
charge sensitivity to force for tourmalineN
pC,9.1 or
N
pC,4.2 ;
charge sensitivity to force for lead-zirconate-titanateN
pC,265 ;
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charge sensitivity to force for lead metaniobateN
pC,80 .
We need to develop an electrical circuit which will allow us to convert variations of the
capacitance of the piezoelectric sensor into the variation of an easy measurable electrical signal,voltage, for example. Such equivalent electrical circuit was developed, and is named after
Norton.
+
-
RloadCpiez
P
Ccable Vload
1 2 3
Ipiez
Figure 9. Norton equivalent electrical circuit for piezoelectric pressure/force measurements.
1- piezoelectric element, 2 connecting cable, 3 recorder.
The piezoelectric element can be represented as a current source (or a charge generator) which is
connected in parallel with a capacitance piezC . Then, this element is connected to a voltage
recorder via connecting cables, which have the capacitance cableC . A recorder has a resistive
load, loadR . The voltage measured across loadR is equal:
ZIV piezload *= , (8)
where,
loadCC RRRZ cablepiez
1111++= - the impedance of three resistances connected in
parallel, .Ohm
According to the definition, the capacitance is equal to the ratio of the charge to the voltageacross the capacitor plates, according to:
V
qC= , (9)
Lets consider capacitance
load
piez
piezV
qC = , (10)
After differentiating both sides of (10) we can get:
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load
piezpiez
Vdt
dq
dt
dC 1*= , (11) or
load
piez
piezV
I
dt
dC = , (12)
or, according to the Ohms Law,piez
piezRdt
dC
1= . (13)
Similar we can getcable
cableRdt
dC
1= . (14)
Substitution of (4-74) and (4-75) into (4-69) will give:
sCCR
RIV
cablepiezload
loadpiezload
)(*1*
++= , (15)
where,
dt
ds = - the Laplace operator.
Expressing variables loadV and piezI in deviation form and applying the Laplace transform to
(15) we can get:
sCCR
RsIsV
cablepiezload
loadpiezload
)(*1*)()( ''
++= , (16)
The transfer function for the Norton equivalent electrical circuit for piezoelectric pressure/force
measurement system (see Figure 9) is as follows:
sCCR
R
sI
sVsG
cablepiezload
load
piez
loadIV
)(*1)(
)()(
'
'
++==
, (17)
According to the definition:
dt
dqI
piez
piez =, (18). Expressing these variables in deviation form and applying the
Laplace transform to (18) we can get:
ssqsIpiezpiez
*)()( '' = . (19)
The transfer function relating current and charge of the piezoelectric sensor is as follows:
ssq
sIsG
piez
piez
qI ==)(
)()(
'
'
. (20)
The transfer function relating the voltage loadV and the measured pressure P can be determined
as follows:
)(*)(*)()()( sGsGsGsGsG IVqIPqPVoverall == . (21)
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After substitution of1
21)('
)()(
2
2
'
++
==
ss
K
sP
sqsG
nn
xpiez
Pq
, (17) and (19) into (21) we can
get an expression for an overall transfer function of the piezoelectric pressure/force measurement
system:
sCCR
Rs
ss
K
sI
sV
sq
sI
sP
sqsG
cablepiezload
load
nn
x
piez
load
piez
piezpiez
PV
*)(*1**
121
)(
)(*
)(
)(*
)('
)()(
2
2
''
''
++++
=
==
(22)
6. Capacitance pressure transducersFig. 10 presents a transducer for sensing and transmitting differential pressure. Pressures to be
measured act on isolating diaphragms 1 and 2 and are transmitted through a silicone oil 3, which
fills the system, to a sensing diaphragm 4. This sensing diaphragm is balanced by two forcesdeveloped by measured pressures and presents the sensitive element. Capacitor plates 5and 6detect the position of the sensing diaphragm, which moves to the left or to the right, and, thus,
the differential pressure applied to the sensitive element. The change in electric capacitance is
electronically amplified and converted to the standard electrical analog or digital output signal,which is directly proportional to the difference of pressures. In order the capacitance transducer
be able to measure comparatively low pressures, the device should produce about 25% change in
capacitance for a full-scale pressure change. These transducers have low mass and high
resolution. However, they are slightly dependent on temperature variation. Newly developed all-silicon capacitive pressure sensors have better thermal stability.
1 2
4
5
6
3
P2
P1
Figure 10. Variable capacitance differential pressure transducer.
Variable separation capacitance sensors have non-linear relationship between electrical
capacitance and the movement of the separating membrane according to the formula:
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ad
AC
+=
0 , (23)
where,
C - the electrical capacitance of the pressure sensor, F (Farad);
m
pF
,85.80=
- the permittivity of vacuum, 1pF=10
-12
F;
- the relative permittivity of the insulating material between plates of
the capacitor, this is the dimensionless parameter;
A - the cross-sectional area of the capacitor plate, 2m ;
d - the distance between the capacitor plates, m ;a - variation of the distance between the capacitor plates, m .
A three-plate differential version of the capacitive pressure sensor doesnt have such
disadvantage (see Figure 11).
Two fixed plates form two capacitances with the moving separating plate/membrane as follows:
ad
AC
+=
01 , (24) and
ad
AC
=
02 . (25)
2d
a
d-a
d
d+a
Figure 11. Three-plate differential pressure/displacement sensor(.
Figure 12 shows an a.c. deflection bridge for the detection of variations of capacitances.
Vcd
Z2
Z3
a b
d
c
Vab
Z4
Z1
I1I1
I2 I2
Figure 12. a.c. deflection bridge.
In this bridge:
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1
1
1
CjZ
= , (26)
2
2
1
CjZ
= , (27) RZZ == 43 ,(28)
where,
1Z and 2Z - reactive impedances, Ohm;
3Z and 4Z - resistive impedances, Ohm.
When 0=cdI , then cdV is called an open-circuit voltage of the bridge. According to the
Kirchoffs laws we have:
3141 ZIZIVab += , (29) 2212 ZIZIVab += . (30)
Let potential at 0=bV , then:
( ) ( )
d
Va
adad
adV
ad
A
ad
A
ad
A
V
CC
CV
RR
R
CjCj
CjV
ZZ
Z
ZZ
ZVZ
ZZ
VZ
ZZ
V
ZIZIZIVZIVVVV
ab
abab
abab
ababab
ababdccd
2*
2
1
11
1
*2
1*
2
1*
11
1
*
*
00
0
21
2
21
1
43
4
21
14
43
1
21
41121241
=
=
+
+
=
+
+
=
=
+=
+
+=
=
+
+=
+
+=
====
(31)
So, the relationship between cdV and a is linear.