For
the insulation of hot objects - especially large-dimensional ducts as found
in nuclear power plants, flue gas desulphurization, and denitronisation
systems -, it must be considered that reinforcing stiffeners on the duct wall
always constitute thermal bridges. Two problems result:
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The
increased thermal transmission through the thermal bridge leads to reduced
temperatures at the inner surface of the duct wall. This may lead to going below the dew point temperature of the flue gas on that inner surface. This problem is not considered in this paper.
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With
unacceptably high-temperature differences between the inner and the outer
edge of the stiffeners, thermal stress may result leading to distortion of
profiles resulting in cracking of welded seams. For this reason, it is common
to calculate maximum admissible temperature differences that are to be maintained
through an appropriate construction and dimensioning of the insulation.
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The
limitation to the temperature differences demanded does not constitute a problem in steady-state service, i. e. with flue-gas temperatures not
changing over time as long as the required insulation material coverage on
the outside of the stiffeners - 1/3 s for stiffeners up to 100 mm, 2/3 s for
stiffeners over 100 mm - is observed.
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Difficulties,
however, may occur in the non-steady-state service - where flue-gas temperatures
change over time as the installation is started up or shut down.
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On
starting up the installation, the temperature on the inner surface of the
wall and the inner edges of the reinforcing stiffeners follows the increasing
flue-gas temperature, whilst the outer edges of the stiffeners remain cold,
and the temperature there increases only after a considerable delay. This
may lead to temperature differences substantially above those in steady-state
service.
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The magnitude of these „non-steady-state temperature differences“ is dependent
upon a variety of factors:
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The
speed of temperature increase in the flue gas: the faster the installation the startup, the higher the temperature differences.
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Size
of the stiffeners: with big profiles and large masses, the temperature
differences are higher than with smaller profiles.
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Shape
of the reinforcing stiffeners.
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Thermal the conductivity of the materials used.
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Thermal
transmission conditions.
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To
lower the temperature differences, measures must be taken to allow for the
movement of as much heat as possible through radiation and convection from
the duct wall to the outer edge of the reinforcing stiffeners. This may be
achieved - if technically feasible - by leaving an ample portion of the duct
wall uninsulated.
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These
and other measures in the area of insulation are, however, of limited effect. With big reinforcing stiffeners, the steady-state temperature differences cannot be reduced to acceptable values even through „the best possible insulation“. Therefore, other measures - outside of the control of the insulation trade - are required. Such measures could be e. g. to use
several smaller stiffeners instead of one large one, or to reduce the rate of temperature increase when starting up the installation.
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2. Principal considerations concerning the
non-steady-state temperature distribution in reinforcing stiffeners
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Depending
upon the individual design, the temperatures in reinforcing stiffeners are
influenced by the shapes, and the appropriate insulation material design
values.
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Some
observations of principle can be made for the design examples
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The
simple reinforcing fin is shown in Figure 1 (steel sheet; generally smaller than
100 mm) would generally have roughly equal temperatures at the inner and outer edges, providing the insulation material coverage d was sufficiently extensive (see chapter 1). In this case, no elevated thermal stress occurs. The „dew point temperature problem“ on the inner surface of the duct wall, however, must also be considered in this case.
Contrary
to this example, the temperature on the outer flange of the normally bigger I-profile (double T-profile - generally with webs exceeding 100 mm)
definitely be lower than the inner flange, since bigger masses must be
heated on the outer edge and the heat transport requires more time due to the
length of the web.
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Frequently,
the insulation contractor is required to prove mathematically the temperature
differentials to be expected - normally calculated against known warming-up
conditions in the start phase of the installation. Such calculations can be
computed with numerical procedures such as the finite difference or the
finite element method. However, it must be remembered that with these methods the thermal transmission inside the stiffener can be calculated satisfactorily exactly, however, assumptions must be made regarding the movement of heat through radiation and convection, the precision of which is frequently very difficult to assess. This applies especially to radiation.
Here, the surface conditions of the duct wall and the reinforcing stiffener are of decisive importance. They are not known to the insulation contractor with the precision required. Therefore, the declaration of warranties on the basis of such calculations should be cautioned against.
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3. Examples
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For
insulation following the surface of a profile IPE 360 as in Figure 2a, some
results of finite element calculations are given below. Figure 3 shows the
temperature increase over time at an uninsulated duct wall, the inner and
outer edges of the reinforcing flange when the warming-up transients are 1,6
K/min and 0,4 K/min.
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The
maximum occurring temperature differences for a profile IPE 400 insulated
according to Figure 2a is given for different warming-up transients and for
the steady-state service in Table 1.
Instationär
Ausgangstemperatur
= +40 °C
non-steady-state
Initial temperature = +40 °C
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Profil
Profile
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Temperaturdifferenz
der
Flansche = DJ [K]
Temperature differ-
ence in stiffeners =
DJ [K]
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Anfahrgeschwindigkeit
K/min
Initial temperature
K/min
(temperature transient)
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IPE
400
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ca.
(about) 50-60
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1,6
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„ -
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ca.
(about) 40
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0,8
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„ -
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90
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2,0
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IPE
460
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75
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1,6
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„ -
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50
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0,8
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HEA
300
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57
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1,6
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„ -
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45
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0,8
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IPE
370
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53
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1,6
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-
„ -
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34
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0,8
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IPE
300
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45
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1,6
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IPE
270
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42
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1,6
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Table 2: Temperature differences in flanges with
„air-gap“-insulation (according to Figure 2b)
The results show that especially whilst warming up the installation, critical stress maxima must be expected. The warming-up gradient has a decisive influence.
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A
comparison of the two designs considered here makes it obvious that the
air-gap-insulation compared to the surface-following insulation results in
smaller temperature differences for both the steady-state and the
non-steady-state conditions. These observations, however, only hold true when
uncontrolled convection influence can be prevented.
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4. Conclusions
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For
the insulation of large-dimensional, hot objects, special thermal conduction
considerations are required. Additionally, investigation of the possible
deformation in the stiffeners as a result of temperature differentials is
needed. This applies specifically to non-steady-state service conditions such
as start-up and shut-down phases and accidents.
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A
mathematical proof of the maximum occurring thermal stresses in the steel
construction of an object is not within the area of responsibility of the
insulation contractor. The static system selected and the static and dynamic
stresses to be born by the construction are in the area of responsibility of
the installation contractor.
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Nevertheless,
this problem should be addressed when discussing contracts and the builder
should be made aware of it. It could be possible that there is a duty to
caution against possible damages, if the thermal stresses to be expected as
result of the layout and size of the reinforcements and the temperature
differences to be expected could lead to damages.
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In
critical cases, the necessity may even occur to ensure an even distribution
of heat at the outer edges of the reinforcement in the warming-up phase of
the installation by installing an extra heating system.
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