hydrogen-bonding surfaces for ice mitigation: the effect
TRANSCRIPT
Hydrogen-Bonding Surfaces for Ice Mitigation: The Effect of Surface Chemical Functionality Upon Ice
Adhesion Joseph Smith 1, Christopher Wohl 1, Jereme Doss2, Destiny Spence3,
Richard Kreeger4, Jose Palacios5, Taylor Knuth5, Kevin Hadley6, and Nicholas McDougal6
1NASA Langley Research Center, Hampton, VA 23681, USA 2National Institute of Aerospace, Hampton, VA 23666, USA
3NASA USRP Researcher, NASA Langley Research Center, Hampton, VA 23681, USA 4 NASA Glenn Research Center, Cleveland, OH 44135, USA
5The Pennsylvania State University, University Park, PA 16802, USA 6South Dakota School of Mines and Technology, Rapid City, SD 57701, USA
NARI 2015 Seedling Technical Virtual Seminar, March 18-‐19, 2015 1
Background
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❄ Icing Ground problem during cold months
• Freezing drizzle/rain In-flight problem year round
• Results from super-cooled water droplets impacting the aircraft surface while flying through a cloud
• Most occurrences are between 0 and -20°C
❄ Icing types encountered in-flight Glaze/Clear, Rime, Mixed Dependent upon
• Air temperature (0 to -20°C) • Liquid water content (0.3-0.6 g/m3) • Droplet size (median volumetric diameter of 15-40 µm)
M.K. Politovich, “Aircraft Icing” in Encyclopedia of Atmospheric Sciences, Academic Press, Oxford, 2003, 68-75. H.E Addy Jr., M.G. Potapczuk, and D.W. Sheldon, “Modern Airfoil Ice Accretions,” NASA TM 107423, 1997.
Background
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M.K. Politovich, “Aircraft Icing” in Encyclopedia of Atmospheric Sciences, Academic Press, Oxford, 2003, 68-75. H.E Addy Jr., M.G. Potapczuk, and D.W. Sheldon, “Modern Airfoil Ice Accretions,” NASA TM 107423, 1997.
Glaze/Clear Rime Mixed
• Small droplets • Brittle and opaque, milky
appearance • Rapid freezing after droplet
impact with growth into the airstream
• Easier to remove than glaze
• Variable droplet size • Combination of glaze
and rime ice
• Large droplets • Clear, nearly transparent,
smooth, waxy thus hard to see • Gradual freezing after droplet
impact can result in runback along surface generating raised edges (i.e. horns)
• Difficult to remove
Background
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❄ Current alleviation strategies Pneumatic boots Heated surfaces De-icing fluids (i.e., ethylene- and propylene-based glycols)
❄ A passive approach mitigating ice adhesion during the entire aircraft flight profile is desirable.
Superhydrophobic surfaces1
Surfaces containing anti-freeze proteins2
Slippery liquid-infused porous surfaces3
Aqueous lubricating layer4
1. S.A. Kulinich et. al., Langmuir, 27 (2011) 25-29. 2. Anitei, S. Fish 'Antifreeze' Against Icy Aeroplanes. Aug. 8, 2007; http://news.softpedia.com/news/Fish-Antifreeze-Against-Icy-Aeroplanes-62189.shtml 3. L. Mishchenko, et. al.,”Design of Ice-free Nanostructured Surfaces Based on Repulsion of Impacting Water Droplets,” ACS Nano, 4 (2010) 7699-7707. 4. R. Dou et.al., “Anti-icing Coating with an Aqueous Lubricating Layer,” ACS Appl. Mater. Interfaces (2014).
Objective
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Investigate coated surfaces having controlled chemical functionality and carbon chain length between the substrate surface and the chemical functionality. ❄ Prepare and characterize substituted alkyldimethylalkoxysilanes containing Hydrogen Bonding (HB) and non-HB groups.
ATR-FTIR, NMR (1H, 13C, 29Si) ❄ Prepare and characterize aluminum (Al) substrates coated with pure and mixtures of alkyldimethylalkoxysilanes containing HB and non-HB groups.
Contact Angle Goniometry ❄ Determine IASS of coated Al substrates in a simulated environment with comparison to uncoated Al.
Adverse Environment Rotor Test Stand
To assess the effect of surface chemical functionalization upon ice adhesion shear strength (IASS).
Approach
Substituted Dimethylalkoxysilanes
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Si
CH3
CH3
O CH2 CH3xH3CH2C
x = 2 (C3A), 6 (C7A), 10 (C11A)
Si
CH3
CH3
O CH2 ORy
H3CH2C
X = -, y = 7 (C7H), 10 (C10H), 11 (C11H)
R = -CH2CH2OCH3, y = 5
X = -OCH2CH2-, y = 2 (EG)
C5MEG
EG
Non-hydrogen bonding
Hydrogen-bonding (donor/acceptor)Hydroxyl
Hydrogen-bonding (acceptor)
Aliphatic
Si
CH3
CH3
O CH2 Xy
Coating Al Substrate I
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Si
CH3
CH3
O CH2 CH3xH3CH2C
x = 2 (C3A), 6 (C7A), 10 (C11A)
R = -CH2CH2OCH3, y = 5C5MEG
HOAc, EtOH, H2O
Hydrogen-bonding (acceptor)
Aliphatic
Si
CH3
CH3
O CH2 ORy
H3CH2CSame method for
Non-hydrogen bonding
CH2Cl2, RTSi
CH3
CH3
HO CH2 CH3x
Si
CH3
CH3
HO CH2 CH3xAl
OH + Si
CH3
CH3
CH2 CH3xAl
O
HOAc, EtOH, H2O
CH2Cl2, RTSi
CH3
CH3
HO CH2 Xy
AlOH + Si
CH3
CH3
CH2 Xy
AlO
Si
CH3
CH3
O CH2 Xy
X = -, y = 7 (C7H), 10 (C10H), 11 (C11H) X = -OCH2CH2-, y = 2 (EG)EG
Hydrogen-bonding (donor/acceptor)Hydroxyl
OH
Si
CH3
CH3
HO CH2 Xy
OH OH
Coating Al Substrate II
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Receding Water Contact Angle
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0
20
40
60
80
100
120
C3A C7A
C11A
C7A (5
0%)/C
3A (5
0%)
C11A (2
5%)/C
3A(75
%)
C11A (5
0%)/C
3A (5
0%)
C11A (7
5%)/C
3A (2
5%)
C11A (5
0%)/C
7A (5
0%)
C7H
C10H
C11H
EG
C7H (5
0%)/C
3A (5
0%)
C7H (5
0%)/C
7A (5
0%)
C10H (5
0%)/C
7A (5
0%)
EG (50%
)/C3A
(50%
)
EG (25%
)/ C3A
(75%
)
C5MEG
C5MEG (5
0%) /C
3A (5
0%)
C5MEG (5
0%)/C
7A (5
0%)
C5MEG (5
0%)/C
7H(50
%)
Wat
er R
eced
ing
Con
tact
Ang
le, °
Al Control
Higher Ice
Adhesion Strength
Lower Ice
Adhesion Strength
x = 2 (C3A), 6 (C7A), 10 (C11A)Si
CH3
CH3
CH2 CH3xAl
O
X = -, y = 7 (C7H), 10 (C10H), 11 (C11H)
X = -OCH2CH2-, y = 2EGSi
CH3
CH3
CH2 Xx
AlO OH
C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O
x = 2 (C3A), 6 (C7A), 10 (C11A)
X = --, y = 7 (C7H), 10 (C10H), 11 (C11H)
X = -OCH2CH2-, y = 2 (EG)
C5MEG
Adverse Environment Rotor Test Stand
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❄ Pennsylvania State University ❄ Testing performed under simulated icing conditions.
Super-cooled water injected into test chamber.
Tests conducted from -8 to -16°C; commenced at -16°C
Icing cloud density (i.e. liquid water content) of 1.9 g/m3
Water droplet mean volumetric diameter of 20 µm
❄ Ice accumulation and subsequent shedding enabled determination of Ice Adhesion Shear Strength after data analysis and visual assessment. ❄ Experimental details discussed in J. Soltis, J. Palacious T. Eden, and D. Wolfe, “Evaluation of Ice Adhesion Strength on Erosion Resistant Materials,” 54th AIAA/ ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, April 8-11, 2013, Boston, MA, AIAA 2013-1509.
Credit: The Pennsylvania State University
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One Component Coatings
0"
50"
100"
150"
200"
250"
Al"Control" C3A" C7A" C11A"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
/8°C" /12°C" /16°C"
Non-HB: Chain Length Effect
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x = 2 (C3A), 6 (C7A), 10 (C11A)Si
CH3
CH3
CH2 CH3xAl
O
0"
20"
40"
60"
80"
100"
120"
140"
160"
180"
200"
Al"Control" C7H" C10H" C11H" EG"
Ice$Ad
hesion
$She
ar$$Str.,$kPa$
38°C" 312°C" 316°C"
Si
CH3
CH3
CH2 Xy
AlO
X = --, y = 7 (C7H), 10 (C10H), 11 (C11H)
X = -OCH2CH2-, y = 2 (EG)
OH
HB (donor/acceptor): Chain Length Effect
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0"
20"
40"
60"
80"
100"
120"
140"
160"
180"
200"
Al"Control" C5MEG"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
38°C" 312°C" 316°C"
HB (acceptor)
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C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O
Functional Group and Chain Length
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0"
50"
100"
150"
200"
250"
C7A" C7H" C11A" C11H"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
*8°C" *12°C" *16°C"
Si
CH3
CH3
CH2 CH3xAl
O x = 6 (C7A), 10 (C11A)
X = --, y = 7 (C7H), 11 (C11H) Si
CH3
CH3
CH2 Xy
AlO OH
Functional Group: Similar Chain Length
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C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O
Si
CH3
CH3
CH2 CH3xAl
O
X = --, y = 10 (C10H), 11 (C11H) Si
CH3
CH3
CH2 Xy
AlO OH
x = 6 (C7A)
C5MEG
0"
50"
100"
150"
200"
250"
Al"Control" C11A" C10H" C11H" C5MEG"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
18°C" 112°C" 116°C"
One Component Coating Summary
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❄ Aliphatic (non-HB) Minimum chain length (C7A) needed to decrease interaction of
ice with the substrate (C3A) Long chain length (C11A) resulted in coating degradation Performance compared to HB series dependent on chain length
x = 2 (C3A), 6 (C7A), 10 (C11A)Si
CH3
CH3
CH2 CH3xAl
O
X = -, y = 7 (C7H), 10 (C10H), 11 (C11H)
X = -OCH2CH2-, y = 2EGSi
CH3
CH3
CH2 Xx
AlO OH
❄ Hydroxy1 and EG (HB donor/acceptor) Not much difference in IASS between test temperatures Long chain (C10H, C11H) performed better EG performance similar to C7H
❄ C5MEG (HB acceptor) Functional group performance similar to C7A Comparable chain length performance
• HB donor/acceptor (C10H, C11H) resulted in lower IASS • C11A (non-HB) degraded
In general, performed better than EG
C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O
x = 2 (C3A), 6 (C7A), 10 (C11A)
X = --, y = 7 (C7H), 10 (C10H), 11 (C11H)
X = -OCH2CH2-, y = 2 (EG)
C5MEG
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Two Component Coatings
Non-HB: Different Chain Lengths
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0"20"40"60"80"100"120"140"160"180"200"
Al"Control" 0" 50" 100"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
C7A$in$C3A/C7A$coa8ngs,$%$
08°C" 012°C" 016°C" Si
CH3
CH3
CH2 CH3xAl
O x = 2 (C3A), 6 (C7A)
Increasing HB Content: Different Chain Lengths
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Si
CH3
CH3
CH2 CH3xAl
O x = 2(C3A)
X = --, y = 7 (C7H) Si
CH3
CH3
CH2 Xy
AlO OH
0"
20"
40"
60"
80"
100"
120"
140"
160"
180"
200"
Al"Control" 0" 50" 100"
Ice$Ad
hesion
$She
ar$$Str.,$kPa$
C7H$in$C3A/C7H$coa9ngs,$%$
08°C" 012°C" 016°C"
Increasing HB Content: Similar Chain Lengths
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0"
20"
40"
60"
80"
100"
120"
140"
160"
180"
200"
Al"Control" 0" 50" 100"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
C7H$in$C7A/C7H$coa8ngs,$%$
08°C" 012°C" 016°C" Si
CH3
CH3
CH2 CH3xAl
O x = 6(C7A)
X = --, y = 7 (C7H) Si
CH3
CH3
CH2 Xy
AlO OH
0"20"40"60"80"100"120"140"160"180"200"
Al"Control" 0" 50" 100"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
C10H$in$C7A/C10H$coa:ngs,$%$
08°C" 012°C" 016°C"
Increasing HB Content: Different Chain Lengths
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Si
CH3
CH3
CH2 CH3xAl
O x = 6(C7A)
X = --, y = 10 (C10H) Si
CH3
CH3
CH2 Xy
AlO OH
Increasing HB Content: Different Chain Lengths
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0"20"40"60"80"100"120"140"160"180"200"
Al"Control" 0" 25" 50" 100"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
EG$in$EG/C3A$coa9ngs,$%$
08°C" 012°C" 016°C" Si
CH3
CH3
CH2 CH3xAl
O x = 2 (C3A)
X = -OCH2CH2-, y = 2 (EG) Si
CH3
CH3
CH2 Xy
AlO OH
Increasing HB (acceptor) Content: Different Chain Lengths
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0"20"40"60"80"100"120"140"160"180"200"
Al"Control" 0" 50" 100"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
C5MEG$in$C3A/C5MEG$coa;ngs,$%$
08°C" 012°C" 016°C" Si
CH3
CH3
CH2 CH3xAl
O x = 2 (C3A)
C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O C5MEG
0"
20"
40"
60"
80"
100"
120"
140"
160"
180"
200"
Al"Control" 0" 50" 100"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
C5MEG$in$C7A/C5MEG$coa;ngs,$%$
08°C" 012°C" 016°C"
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Increasing HB (acceptor) Content: Different Chain Lengths
Si
CH3
CH3
CH2 CH3xAl
O x = 6 (C7A)
C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O C5MEG
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Increasing HB (acceptor) Content: Different Chain Lengths
0"20"40"60"80"
100"120"140"160"180"200"
Al"Control" 0" 50" 100"
Ice$Ad
hesion
$She
ar$Str.,$kPa$
C5MEG$in$C7H/C5MEG$coa<ngs,$%$
08°C" 012°C" 016°C"
C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O
X = --, y = 7 (C7H) Si
CH3
CH3
CH2 Xy
AlO OH
C5MEG
Two Component Coating Summary
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❄ HB (donor/acceptor) and Aliphatic (non-HB) General - Increasing HB component (Hydroxyl) increased
IASS • Exception -16°C where IASS comparable • C7A/C10H suggested degradation, base components
exhibited no degradation
EG/C3A • 25% EG inclusion exhibited comparable performance to
C3A • 50% EG inclusion
ª Better performance than C3A at -8 and -12°C ª Worse performance at -16°C
x = 2 (C3A), 6 (C7A), 10 (C11A)Si
CH3
CH3
CH2 CH3xAl
O ❄ Aliphatic (non-HB) IASS increased with increasing short chain (C3A) component.
x = 2 (C3A), 6 (C7A)
X = -, y = 7 (C7H), 10 (C10H), 11 (C11H)
X = -OCH2CH2-, y = 2EGSi
CH3
CH3
CH2 Xx
AlO OH
x = 2 (C3A), 6 (C7A), 10 (C11A)Si
CH3
CH3
CH2 CH3xAl
O
X = --, y = 7 (C7H), 10 (C10H)
x = 2 (C3A), 6 (C7A)
X = -OCH2CH2-, y = 2 (EG)
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❄ HB (acceptor) and Aliphatic (non-HB) Performance dependent upon non-HB chain length
• C3A afforded lower IASS compared to C7A ª Presumably due to better accessibility of
in-chain ether group to water • C5MEG/C3A overall performance better than
EG/3A 50/50
C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O
x = 2 (C3A), 6 (C7A), 10 (C11A)Si
CH3
CH3
CH2 CH3xAl
O
❄ HB (acceptor) and HB (acceptor/donor) In general - performance not as good as HB
(acceptor) alone Data suggested coating degradation
C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O
X = -, y = 7 (C7H), 10 (C10H), 11 (C11H)
X = -OCH2CH2-, y = 2EGSi
CH3
CH3
CH2 Xx
AlO OH
Two Component Coating Summary
x = 2 (C3A), 6 (C7A)
X = --, y = 7 (C7H)
C5MEG
C5MEG
0
20
40
60
80
100
120
C3A C7A
C11A
C7A (5
0%)/C
3A (5
0%)
C11A (2
5%)/C
3A(75
%)
C11A (5
0%)/C
3A (5
0%)
C11A (7
5%)/C
3A (2
5%)
C11A (5
0%)/C
7A (5
0%)
C7H
C10H
C11H
EG
C7H (5
0%)/C
3A (5
0%)
C7H (5
0%)/C
7A (5
0%)
C10H (5
0%)/C
7A (5
0%)
EG (50%
)/C3A
(50%
)
EG (25%
)/ C3A
(75%
)
C5MEG
C5MEG (5
0%) /C
3A (5
0%)
C5MEG (5
0%)/C
7A (5
0%)
C5MEG (5
0%)/C
7H(50
%)
Wat
er R
eced
ing
Con
tact
Ang
le, °
Al Control
y y, except -16C n degraded
Higher Ice
Adhesion Strength
Lower Ice
Adhesion Strength
Receding Water Contact Angle
NARI 2015 Seedling Technical Virtual Seminar, March 18-‐19, 2015 29
x = 2 (C3A), 6 (C7A), 10 (C11A)Si
CH3
CH3
CH2 CH3xAl
O
X = -, y = 7 (C7H), 10 (C10H), 11 (C11H)
X = -OCH2CH2-, y = 2EGSi
CH3
CH3
CH2 Xx
AlO OH
C5MEGSi
CH3
CH3
CH2 OCH2CH2OCH3 5Al
O
x = 2 (C3A), 6 (C7A), 10 (C11A)
X = --, y = 7 (C7H), 10 (C10H), 11 (C11H)
X = -OCH2CH2-, y = 2 (EG)
C5MEG
Conclusions
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❄ Effect of coating composition on IASS is complex One component coatings
• Chain length effect upon IASS is functional group dependent • No clear trend observed between functional groups
Two component coatings • More relevant when incorporating functionalities into polymeric
systems • General – increasing HB content (HB donor/acceptor) increased
IASS • Mixed chain length effect upon IASS is composition/functional
group dependent
Future Work
NARI 2015 Seedling Technical Virtual Seminar, March 18-‐19, 2015 31
❄ Develop monomers with pendant groups based on non-HB and HB (acceptor) effects
❄ Prepare epoxies based on the developed monomers ❄ Test epoxy coated Al samples in AERTS to determine IASS
Acknowledgements ❄ Ronald Penner (Science Technology Corporation) ❄ Dennis Working (NASA)