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Development of Innovative Ultra High Temperature
Coatings Provides Long Term Corrosion Protection
of Process Vessels and Piping
Yuguo Cui, Senior Product Development Chemist
Furnace Mineral Products Inc. (FMP Coatings)
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Presentation Contents
Materials in industrial use
High Temperature corrosion – problem
areas
Introduction to polymeric coatings
Limitations with conventional epoxy
materials
Next generation hybridized technology
Vessel linings
Live CUI solutions
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Challenge with Metallic Materials Today
Metals are strong solid materials that can be deformed,
welded or cast into shapes, it is widely used to store
and convey liquids and gases for industrial use
As corrosion engineers, we know that metals are
elements that readily give up electrons (oxidize)
The higher the temperature, chemical concentration,
moisture, and ionic activity the faster the oxidization
rate
Forms of corrosion in industrial settings includes
galvanic attack, crevice corrosion, stress corrosion
cracking (SCC), pitting, bacterial attack and erosion
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High Temperature Corrosion
Industrial processes are operating at higher temperatures and
the corrosion rates are accelerating
Conventional organic coatings are exhibiting limited success above
100 oC in immersion service
Next generation ultra high temperature coatings are maximizing
temperature resistance
These solvent free coatings can withstand temperatures above 180oC while
providing excellent erosion and chemical resistance
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Use of Coatings
Use of polymeric coatings are an
economical and viable approach to
reduce metallic corrosion rates
For industrial assets operating at high
temperature, pressure, in a chemical rich
environment there are limitations to the
use of conventional epoxy based
polymeric coatings
Generic polymer coatings don’t work.
The use of engineered surface
coatings specifically designed for each
end use must be considered
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Epoxy Chemistry – The Basics
• Epoxy coatings are organic thermosetting polymers
• Key properties of epoxy chemistry is molecular
weight, molecular weight distribution, glass
transition (Tg), and solubility
• Cure by chemical reaction
• Reaction between epoxide resin and
an amine curing agent
• 3 main components to epoxy coatings
(resin, hardener and modifier)
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Resin Selection
Type Structure Viscosity Tg
Bisphenol A 15,000 cps 175 oC
Bisphenol F 5,000 cps 150 oC
Novolac Semi Solid at
Room
Temperature
200 oC
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Resin Viscosity
0
10
20
30
40
50
60
70
80
90
Bisphenol A Bisphenol F Novolac 3.6 f
Temperature at 4,000 cps
0
50
100
150
200
250
Bisphenol F Bisphenol A Novolac
Resin Tg (oC)
0
10
20
30
40
50
60
Bisphenol A Bisphenol F Novolac 3.6 f
Percentage%
Diluent Requirement to Drop to 4,000 cps
*Viscosity of water is 1 cps
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Hardener Selection
0
50
100
150
200
250
Amide Aliphatic Cycloaliphatic Aromatic
TemperatureoC
Hardener Curing Temperature
• Types of Epoxy Curatives
– Polyamide
– Aliphatic
– Cycloaliphatic
– Aromatic
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Use of Solvents
• Solvency – viscosity reduction
• Environmental impact
• Sacrifice performance
• Will not survive high
temperature exposure
Autoclave Testing 96 hrs at 120 oC at vapour pressure
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100 % Solids – Solvent Free
• A 100% solids coating system is defined as a coating that
results in no film thickness change during application.
• So how does a formulator of 100% solids coating drive
down the viscosity so that the coating can be sprayed or
rolled ?
• The trick is the use of a high boiling point solvent (ie,
benzyl alcohol) that is volatile but also reacts with the
epoxide group of the coating so that the bulk of the
solvent remains in the coating system.
• In high temperature systems this approach does not work
• To overcome the need for solvent, the system is heated to
reduce viscosity
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Technological Gap
Glass Transition Curve
Cross Link Density
Low Tg Higher Tg
Why traditional epoxies fail
at high temperature
• Low Tg
• Low cross link density
• High free volume
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Inorganic Chemistry
• Ceramic inorganic chemistry has
been used for combustion service
ranging from 370 to 800 oC since the
1980s.
• Upon curing the coating forms an
amorphous layer that bonds the
ceramic matrix to the substrate
surface
• Limitations
– requires post cure at elevated
temperature
– Not suitable for immersion service
– Difficult to apply
– Thin film
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Technology Development - Hybridization
ORGANIC CHEMISTRY
Contains backbones
comprised of chains and/or
rings of carbon (plant
based) and hydrogen
atoms.
INORGANIC CHEMISTRY
Contains backbones
comprised of non carbon
containing elements such as
silicon (mineral based).
Silicon offers extreme
thermal stability and
temperature resistance
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Ultra high temperature resistant coatings – industrial uses
ULTRA HIGH TEMPERATURE LINING
• Two component hybridized thermoset polyermic lining
for ultra high temperature corrosion protection of
process vessel (immersion service)
CUI PROTECTION
• Single component heat activated surface tolerant
composite coating for corrosion under insulation (CUI)
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Two components hybridized thermoset epoxy coating-
Introduction
PROCESS VESSEL LINING
• Corrosion prevention of process vessel (immersion
service)
• High temperature (>100oC) resistance
• Chemical resistance (water, acid, base, solvent,
petroleum)
• Can be easily applied by spray
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Two components hybridized thermoset organic coating-
Formulation
• Hybridized
• Si-O bond
• High functionality novolac epoxy
• Ceramic fillers
• Combination of amine hardener chemistry
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Test Methods
Test Method Description
ASTM D648 Heat Deflection Temperature
ASTM D6137 Sulfuric Acid Resistance of Polymer Linings for Flue Gas
Desulfurization Systems
ASTM D5499 Heat Resistance of Polymer Linings for Flue Gas Desulfurization
Systems
NACE TM 0174 Laboratory Methods for the Evaluation of Protective Coatings and
Lining Materials on Metallic Substrates in Immersion Service
NACE TM 0185 Evaluation of Internal Plastic Coatings for Corrosion Control of
Tubular Goods by Autoclave Testing
ASTM 2485 Evaluating Coating for High Temperature Service
CSA Z245.20 Hot Water Soak Test
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Test Methods
Test Method Description
D3418 Polymers by Differential Scanning Calorimetry (DSC)
ASTM D2240 Standard Test Method for Rubber Property—Durometer Hardness
In House Chemical immersion/heat cycles
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Hybridized thermoset organic coating- Autoclave test
16-1113-01A4
Pre-Test Post-Test Post Test (Angled Lighting)
Figure 1 – Pre-Test and Post-Test Autoclave of Enercote ULX 1
16-1113-01A4
Pre-Test Post-Test Post Test (Angled Lighting)
Figure 1 – Pre-Test and Post-Test Autoclave of Enercote ULX 1
16-1113-01A4
Pre-Test Post-Test Post Test (Angled Lighting)
Figure 1 – Pre-Test and Post-Test Autoclave of Enercote ULX 1
left, pre-test; middle, post-test right, post-test,
angled lighting
NACE TM0185-
2006
Test duration: 7 days
Test temperature: 180±6oC
Test pressure: vapor
pressure
Aqueous phase: deionized
water
Gas phase: water vapor
Release temperature: 64oC
Release pressure: 0 Mpa
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Autoclave test results
Sample #
Testing
Phase
Dry Film
Thickness1
(mil)
Adhesion2 Blistering3 Softening4
Colour4
(Change)
Intercoat
Foam4,5
1
Pre-test 16.3/21.3/18.7 7 No N/A D. Brown Yes
Post-test 15.2/19.3/17.4 10 No No Sl No
2
Pre-test 16.7/23.3/20.4 8 No N/A D. Brown Yes
Post-test 13.2/25.5/19.9 10 No No Sl No
3
Pre-test 19.2/28.7/24.3 10 No N/A D. Brown Yes
Post-test 21.1/27.2/23.0 10 No No Sl No
5
Pre-test 11.9/19.0/15.0 8 No N/A D. Brown Yes
Post-test 9.8/16.9/13.7 10 No No Sl No
6
Pre-test 13.0/19.7/16.8 9 No N/A D. Brown Yes
Post-test 13.6/18.6/16.3 10 No No Sl No
Sample #1, sprayed; #2, sprayed then brushed; #3 brushed; #5 brushed; #6 brushed, post cured at 100oC
1. Film thickness measurement per ASTM D7091-13. Rating is Low/High/Average of at least five measurements.
2. Adhesion performed per NACE TM0185-2006, Section 5.3.2.1. Adhesion rated per ASTM D1654-08
3. Blistering evaluation per ASTM D714-02(2009)
4. Softening, Colour change, and Intracoat Foam per NACE TM0185-2006, Section 5.3.
5. Intercoat foam is determined using a microscope set at 40x magnification
Adhesion (ASTM D1654-08) Softening, Colour Change, Intercoat Foam (NACE TM0185-2006, Section 5.3.1)
Rating: Coating removed (mm): Rating: Description
10 0 (cohesive failure) N No change
9 Over 0.0 up to 0.5 Sl Slight change
8 Over 0.5 up to 1.0 M Moderate change
7 Over 1.0 up to 2.0 Sv Severe change
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Atlas Cell Testing
• NACE TM 0174
• Long term testing
• Great simulation test for chemical exposure at
high temperature
• Provides cold wall effect simulation
• Can also be used under pressure
• Blistering and adhesion loss
• Good wet adhesion testing
• Hybridization improves results
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2K Spray Application Performance Benefits
Lower intercoat porosity
Single coat application reduces the risk of
intercoat failure
Improved edge retention
> 75 %
Improved pit coverage
Improved adhesive strength
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Heated Spray
• Two methods
– Single leg hot pot
– Plural component spray
Characteristic Single Leg (heated) Plural Component (heated)
Ease of Application Requires skilled
technician
Requires skilled technician
Cost of Equipment $7, 000 USD $30,000 - 50, 000 USD
Solvent consumption Flush every 30 min
(dependant of the pot
life and exotherm)
Flush at the end of spray
Pot Life Min 30 min No limit
Max Material Viscosity 20,000 cps 80,000 cps
Max Temperature 38 oC 65 oC
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Plural Component Mixing
A
B
MIX
Dual Heated hose
Proportioner
FluidHeaters
Gravity or pump
feed heated
supply
Volume-balanced hoses
S
Max length depends on pot-life
Mix line
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Single component heat activated composite- Live repair
• Heat Activation
– No product pot life limitations
– Live hot work repair up to 150 oC
– Rapid return to service < 30 minutes
• No Abrasive Blasting Required
– Power tool cleaning
– Hand tool cleaning
• Solvent Free
– No VOC
– Safe to apply to hot surfaces
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Single component heat activated composite- Test
• Surface preparation: hand tool / power tool cleaning
• Application method: brush applied
• Temperature to apply the coating: 75-150 oC
• Final cured temperature: same as temperature to apply the
coating. (example 130oC)
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Single component heat activated composite- Test results
• No blistering was observed during application
• Dry to touch time: 15-6 min for 75-150oC
• Recoat after dry to touch, thickness up to 12-
15 mils
• Pull off strength >3,500 psi (24MPa)
• Thermal stable at 260oC (500oF)
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North American Total Applied Cost per Sqft in USD
Coating Material Solvent
Content by
Volume
Surface
Preparation
Cost per sqft
Actual
Material Cost
per sqft
Material
Application Cost
per sqft
Total Estimated
Cost
Latent Curing
Hybrid Polymer
0% $0.77 $2.98 $0.67 $4.42 per sqft
Solvent Based
Multi-Polymeric
Matrix Coating
49% $2.72 $6.14 $0.67 $9.53 per sqft
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Single component heat activated composite for CUI-
Case study
• Surface preparation: hand tool cleaning
• Application: brushed applied
• Temperature: 120oC
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Conclusion
• Two component hybridized thermoset epoxy coating
with the introduction of silicon-oxide, ceramic fillers,
passed the 180oC autoclave test and can be applied as
corrosion protection for process vessel immersion
service at ultra high temperature.
• Single component heat activated composite can be
applied and cured when the facilities are running at
temperature 75-150oC with minimum surface
preparation for CUI service.
Editor's Notes
The demand for high temperature coating protection is growing in the power generation and oil and gas industry as operations run at higher and higher temperature Conventional polymeric epoxy based chemistries have had limited success in providing corrosion resistance above 100 oC (212 oF) in immersion service.
The requirement for zero solvent, VOC compliant coatings is adding to the formulating complexity. Next generation, high temperature hybrid coatings are pushing the envelope of temperature and wear resistance through the use of inorganic ceramic technology. These solvent free coatings are capable of withstanding temperatures as high as 180 deg C (360 oF) in immersion service while providing excellent erosion and chemical resistance.
The demand for high temperature coating protection is growing in the power generation and oil and gas industry as operations run at higher and higher temperature Conventional polymeric epoxy based chemistries have had limited success in providing corrosion resistance above 100 oC (212 oF) in immersion service.
The requirement for zero solvent, VOC compliant coatings is adding to the formulating complexity. Next generation, high temperature hybrid coatings are pushing the envelope of temperature and wear resistance through the use of inorganic ceramic technology. These solvent free coatings are capable of withstanding temperatures as high as 180 deg C (360 oF) in immersion service while providing excellent erosion and chemical resistance.
Most common generic lining and anti corrosion coating is epoxy based chemistry
Let’s begin by understanding epoxy chemistry. Epoxy coatings are thermosetting polymers. They are typically two component systems. An epoxide resin and an amine hardener.. Both components are in liquid state. They remain in a liquid state until they are mixed together and the polymer reaction begins. As a formulator, we can control the rate of reaction and to make it happen as fast or as slow as possible.
A first step in formulating for high-temperature applications is to select the proper base resin. In making this selection, the main properties of concern are functionality and glass transition temperature (Tg).
One of the approaches to reduce the visicosity of a novolac system is to heat or add a diluent to the resin to reduce the resin system
The second component is the hardener or curing agent. The most important consideration is how volatile the material is and whether is contains ingredients that will be volatile at service temperature. Many curing agents contain a volatile catalyst that will help to speed up the cure reaction.
To overcome the need for solvent we use heat.
A volalite solvent with a high boiling point. The benzyl alcohol acts as a diluent and a catalyst to speed up the reaction.
CTE- coefficient of thermal expansion
Organic epoxy coatings will undergo both physical and chemical changes when heat is applied; this will usually result in undesirable changes to the properties of the coating.
The degradation of epoxy-amine reaction at high temperature proceeds by rupture of the bonds in the cured network, at 240 deg C this is most noticeable.
The primary indicator to determine suitability of a coating system for high temperature service is the glass transition temperature. The glass transition temperature, Tg, can be defined as the temperature at which the coating changes from the rigid state to a rubbery state.
The lower the Tg the more flexible the coating system which means that there is more spacing between the cross linked network and lower cross link density. To optimize Tg it is important to also achieve a very tangled and high cross linked polymer.
The Tg is also strongly affected by the presense of solvents or diluent loading.
The Tg is is function of cross link density of the coating.
The Tg will also change with the cure temperature of the coating Every system, however, will have an ultimate Tg determined by its formulation that cannot be further enhanced by an increase in cure temperature.
We’ve seen how organic chemistry can degrade at higher temperature.
Let’s now explore inorganic chemistry these Icoatings have played an important role in providing protection to combustion equipment such as furnaces and boilers operating at really high temperatures above 480 deg C.
These slurry coatings are formulated as a mixture of ceramic oxides and silica-based polymers.
Upon curing the inorganic ceramic coating forms an amorphous layer that bonds the ceramic matrix to the substrate surface, providing high thermal stability. The addition of an epoxy resin to an inorganic coating would provide the desirable benefit of ambient temperature lower temperature cure with higher thermal stability.
conceive a higher temperature epoxy based coating our approach was to hybridize the coating system with inorganic chemistry aimed to enhance the thermal and mechanical resistance property of the coating film.
To qualify the coatings a methodology for evaluation of high temperature coatings for immersion service needed to be determined. An important consideration for engineers and owners is that the testing requirements for a given coating system should attempt to best simulate the intended service environment. In high temperature service this becomes increasingly important as the polymeric crosslinking and the physical stability of the polymer begins to change with increasing temperature. Therefore, a coating with great chemical resistance and/or abrasion resistance at room temperature may behave very different once exposed to a high temperature environment.
For the purposes of our evaluation we selected a few well recognized test methods including autoclave, atlas cell and taber abrasion.
We have also a modified version of chemical immersion and abrasion testing that to help simulate higher temperature service. The proprietary tests will not be discussed at this time.
Atlas cell testing also measures the ability of the coating to withstand the temperature gradient between the internal and external surface (cold wall effect) under the influence of pressure, temperature, and the internal environment
800 to 1600 micron film build in a single pass
7000 psi – 782 bar
Brushing or trying to trowel down a coating over the pits is a difficult task. You cannot effective wet into the valley of the corrosion pit
Here are two methods to spray heated coatings.
1st is to use a standard single leg airless pump that is equipped with supply containers and paint hose. In this system the coating is fully mixed and the pump dispenses the heated mixed material. The problem withthis approach is the pot life. Most high solids coatings have a short pot life, so as an applicator you run the risk of seizing your equipment if you’re not closely monitoring the pot life and peak exotherm temperature. In this part of the world I’m not sure how feasible this application method can be as the ambient temperature can be very high.
2nd approach is to use a plural component pump. Instead of a single leg this pump consists of two separate pump legs that dispenses the material separately until it hit a static mixer where the two components are mixed together.
Let’s compare the two methods…