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Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-637-
PAPER REF: 5667
EVALUATION OF STAINLESS STEEL PLATES OF HEAT
EXCHANGER DAMAGE
H. Abdel-Aleem1(*)
, B. Zaghloul2, S. A. Khodir
1
1Reasecher at Welding Technology and inspection Lab., Central Metallurgical research & Development
Institute (CMRDI), Egypt 2Prof. Emeritus atWelding Technology and inspection Lab., Central Metallurgical research & Development
Institute (CMRDI), Egypt (*)Email: [email protected]
ABSTRACT
An attempted has been made to unravel the exact reasons for premature damage of stainless
steel plates of plate cooler used as plate heat exchanger (PHE) to cooling down the
temperature of process water using normal cooling water. Analysis suggested that as a result
of presence of some factors such as, harmful corroded element such as chloride ions from
cleaning solution and probably water, in addition to accumulated residual stresses caused by
from water pressure, heavy deformation at protuberance shape and probably over tightening
of cooler plates had led to the failure due to Stress Corrosion Cracking (SCC) failure.
Keywords: Plate heat exchanger, Damage, stainless steel 316, stress crack corrosion.
INTRODUCTION
Plate heat exchangers (PHE) have many uses in different industries such as, fertilizing plants,
milk revival, pre-heater, cooler, heater, regeneration and etc. The Plates Heat Exchanger
(PHE), as shown in Fig.1, is composed of corrugated thin alloy plates, which are hung
between top and bottom guide bars. The plates are compressed by tightening bolts in between
the frame plate and pressure plate until metal - to - metal plate is reached and a channel is
formed. The manner in which the gaskets are fitted enables alternative flow channels to be
created and heat transfer to pass from one side of the plate to the other. The alternative
channels maximize the heat transfer surface in compact manner. Therefore, it can produce the
most effective performance from the compact size (Sunders AED, 1988 and Pearce N, 2001)
The heat exchanger is thermally designed to the required operation and service supplied. The
product, flow rates and required temperature are used to find the required plate arrangement
based on the surface area and allowed pressure drop. Usually, the PHE total heat co-efficiency
is 3 to 10 times greater than the shell and tube heat exchanger (Pearce N, 2001)
316 Stainless steel is a candidate material for manufacturing of PHE's plates due to having its
corrosion resistance properties in cooling water but the parameter of normal cooling water
determine the overall corrosion stability of plate heat exchanger such as temperature, pH,
conductivity, hardness, alkalinity as well as sulphate, nitrate and most importantly Chloride
ion concentration ( Georgiadis MC, 2000 and K.M Dean, 2010).
This paper details the study carried out on twelve stainless plates of PHE having some cracks
after three years in service and recommends certain measures to be taken in term of cleaning
material, operation practice to prolong the life of these plates.
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Modes of Failure
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Cooler plate heat exchanger
Fig.1 - Illustrating diagram for construction of cooler plate heat exchanger.
BACKGROUND INFORMATION
In this study the PHE has set of 132 plates made of 316 stainless steel. These plates are used
as heat exchanger to cooling down the temperature of process water using normal cooling
water. The plates cooler are separated from each other by a gasket. It is reported that, after
three years in service, twelve of total 132 plates have some cracks. During the operation and
as the result of improper cooling due to scale formation in the plate, it was necessary to
perform chemical cleaning with materials containing acid and zinc chloride several times and
the last time was done by injection of Nitric acid to remove the scale. During the plant shut
down all the plates were changed and during cleaning process cracks were visually observed
in some plates.
Two pieces from two different failed plates were investigated to study the cause of the failure.
Table 1 shows the actual operating condition for cooler plate. It is also reported that, during
the operation, the maximum temperature for process side outlet side was raised until 113Co.
Main feature of a heat transfer plate
Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-639-
Table 1 - Operation condition
Condition
Process side Cooling side
inlet outlet inlet outlet
Normal
Operating
Temp.(c)
95 80 30 40
Actual Temp.(co) 104 80 30 35
Normal
Operating
Press.(bar)
10.0 9 3.6 2.8
Actual
Press.(bar) 15 3.6
EPERIMENTAL PROCEDURE AND RESULTS
Visual inspection
The general view of the plates cooler is presented in Fig.2. It is clearly obvious that there was
no mechanical damage. It is also noticed that the cracks are located near to circumference of
the opening holes at each plate and around the areas which were subjected to high
deformation stresses during manufacturing using die pressing process as shown in Fig.3.
Moreover, it is also noticed that there is corrosion losses.
Fig. 2 - General view of the cooler plates after chemical cleaning
Dye penetrant testing (PT) and chemical analysis
The damaged plates showed also crack, pitting and corrosion losses areas as detected by dye
penetrant testing (PT) as shown in Fig.4. The chemical composition done on the received
specimen of the damaged plates is confirmed with the standard 316 stainless steel as given in
the data sheet received.
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Modes of Failure
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Damaged area
Corrosion losses
Fig. 3 - Location of damaged area.
Fig. 4 - Result of dye penetrant test (PT)
Metallographic examinations
Metallographic examinations were conducted on cut pieces from the damaged cooler plates.
Figure 5 shows the macro-photographic appearance of the damaged area using the
stereoscope. It can be noticed that there are some pitting corrosions around the cracks and at
other places as well. The crack started its initiation at the pitting area. Moreover, it is also
Crack area
Proceedings of the 6th International Conference on
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26
noticed that there are some small corrosion spots on the plate near the crack and petting areas.
Figure 6 shows the nature of the crack propagation of
of cooler plate. There is a distinguished main crack propagated in the matrix with small hair
cracks are branched like a tree. The figure indicates also that there are several other cracks
had initiated at the same area.
The cracked area was investigated in the as polish surface condition at high magnification
using optical microscope. Figure 7 shows branching of cracks, the main crack is not
uniformly propagated and it has small branches. The microstructure of the etched surface of
the specimen taken near the crack area is shown in Figs.
morphology of the crack resembles the intergranular
nature ( Metals Handbook ASM Vol. 11 and 13)
Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-641-
noticed that there are some small corrosion spots on the plate near the crack and petting areas.
Figure 6 shows the nature of the crack propagation of a specimen taken at the damaged area
of cooler plate. There is a distinguished main crack propagated in the matrix with small hair
cracks are branched like a tree. The figure indicates also that there are several other cracks
.
Fig. 5 - Pitting and Corrosion losses
Fig.6 - Cracked area as polish
The cracked area was investigated in the as polish surface condition at high magnification
using optical microscope. Figure 7 shows branching of cracks, the main crack is not
pagated and it has small branches. The microstructure of the etched surface of
the specimen taken near the crack area is shown in Figs. 7a and 7b, which reflects that the
morphology of the crack resembles the intergranular stress corrosion cracking (IGSCC)
( Metals Handbook ASM Vol. 11 and 13).
5 mm
(50 X)
noticed that there are some small corrosion spots on the plate near the crack and petting areas.
a specimen taken at the damaged area
of cooler plate. There is a distinguished main crack propagated in the matrix with small hair
cracks are branched like a tree. The figure indicates also that there are several other cracks
The cracked area was investigated in the as polish surface condition at high magnification
using optical microscope. Figure 7 shows branching of cracks, the main crack is not
pagated and it has small branches. The microstructure of the etched surface of
b, which reflects that the
stress corrosion cracking (IGSCC)
5 mm
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Modes of Failure
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(a) Microstructure near the cracked area (50 X)
The micrograph near the cracked area shows partly recrystallized austenite grains, carbide
particles, and remnants of twinning (slip bands) while the matrix is austenite as shown in Fig.
8a. This structure is typically cold worked and annealed structure (Metals handbook ASM
Vol. 17).
In order to investigate the effect of cold working process during the manufacturing of the
plates on the mechanical characteristics at each part of the deformed plate according to the
degree of deformation which was applied on the plate, microhardness measurements were
done on several locations at the plate. The hardness measurements away from the cracked
area (which were exposed to heavy deformation during manufacturing to create curved shapes
on the plate) is in the range of 187-205 Hv, and the hardness values at similar location but
near the tip of the crack is decreased to 157 Hv as the result of stress release due to the
occurrence of the crack at this area as shown in Fig. 8a. While the hardness measurement at
flat areas far from cracked area is 164 Hv, this area was exposed to much less deformation
stresses during the manufacturing process of the plate as compare with the curved cracked
area. The microstructure at the flat area shows normal annealed structure with less twinning
i.e. less residual stresses, as shown in Fig. 8b (Metals handbook ASM Vol. 17)
Fig. 7 - Microstructure near the damaged and cracked areas
(b) Microstructure near the crack area
at higher magnification (100X)
Proceedings of the 6th International Conference on
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26
(a) Microstructure at the cracked area
(sever deformed area) (200X)
Fig. 8
Scanning electron microscopy and scale characterization
Scanning Electron Microscope (SEM) was used to examine the cracked area from the
damaged cooler plate. It has shown a typical intergranular
as shown in Fig. 9 ((Metals handbook ASM Vol. 17)
Due to the chemical cleaning of the cooler plate before receiving the investigated specimens,
no corrosion product could be obtained for chemical or x
precipitates from the cooling water of other cooler plates were removed, in order to be
examined by X-Ray Diffraction (XRD). The results showed the presence of Calcite (Ca CO
and silica SiO2. No indications for any other corrosion products cou
DISCUSSION
It was reported that the cooler plates were cleaned several times using chemical solution
which contained chloride compound
of the cleaning solution and the duration of the cleaning time were increased. Therefore, it can
Hv = 157
Hv = 187
Proceedings of the 6th International Conference on Mechanics and Materials in Design,
Editors: J.F. Silva Gomes & S.A. Meguid, P.Delgada/Azores, 26-30 July 2015
-643-
(a) Microstructure at the cracked area (b) Microstructure far from the crack
(sever deformed area) (200X) area (less severe deformed area) ( 200X)
Fig. 8 - Microstructure variation in the plate surface
Scanning electron microscopy and scale characterization
Scanning Electron Microscope (SEM) was used to examine the cracked area from the
damaged cooler plate. It has shown a typical intergranular stress corrosion cracking behavior
(Metals handbook ASM Vol. 17).
Due to the chemical cleaning of the cooler plate before receiving the investigated specimens,
no corrosion product could be obtained for chemical or x-ray analysis. How
precipitates from the cooling water of other cooler plates were removed, in order to be
Ray Diffraction (XRD). The results showed the presence of Calcite (Ca CO
. No indications for any other corrosion products could clearly be detected.
Fig. 9 - SEM near the cracked area
It was reported that the cooler plates were cleaned several times using chemical solution
which contained chloride compound. In last few cleaning processes, both of the concentration
of the cleaning solution and the duration of the cleaning time were increased. Therefore, it can
Hv = 157
Hv = 187-205
(b) Microstructure far from the crack
area (less severe deformed area) ( 200X)
Scanning Electron Microscope (SEM) was used to examine the cracked area from the
stress corrosion cracking behavior
Due to the chemical cleaning of the cooler plate before receiving the investigated specimens,
ray analysis. However, some
precipitates from the cooling water of other cooler plates were removed, in order to be
Ray Diffraction (XRD). The results showed the presence of Calcite (Ca CO3)
ld clearly be detected.
It was reported that the cooler plates were cleaned several times using chemical solution
In last few cleaning processes, both of the concentration
of the cleaning solution and the duration of the cleaning time were increased. Therefore, it can
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Modes of Failure
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be deduced that the austenitic stainless steel cooler plate has failure due to exposure to
chloride containing solution during chemical cleaning for several times and each time the
concentration of the harmful element, chloride ions was increased. The cracks were developed
at the protuberance shape which reflected the highest hardness values as a result of heavy
deformation during manufacturing process causing relatively high residual stresses. The
Chlorine ions replaced oxygen/hydroxide ions in the protective layer. Usually the cooler
plates are tied together; sometimes they are over-tightened to eliminate a leakage situation,
then cooler plates would have a permanent stress. Moreover, the damaged area is located at
protuberance place at the sheet. This area is expected to have residual stress as indicated from
both microstructure and hardness measurements at damaged area. This condition creates good
atmosphere to cause the intergarnullar stress corrosion cracking. Also, results of XRF for
water cooling precipitates showed presence of silica and calcite which promoted localized
pitting at high flow rate and water pressure.
CONCLUSION
It can be concluded that as a result of presence of some factors such as, harmful corroded
element such as chloride ions from cleaning solution and probably water, in addition to
accumulated residual stresses caused by from water pressure, heavy deformation at
protuberance shape and probably over tightening of cooler plates had lead to the failure due to
Stress Corrosion Cracking (SCC) failure.
ACKNOWLEDGMENTS
The authors thank ALEXFERT Co. for supporting this work.
REFERENCES
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1988.
[2]-Pearce N. Plate Exchanger Defeats Industry Conservatism. Eur Power News 2001 (10) :7-
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[3]-Georgiadis MC, Macchietto S: Dynamic Modeling and Simulation of Plate Heat
Exchanger Under Milk Fouling, CHEM ENG SCI, Vol 55, (2000), 1605-1619.
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