radiation damage in resins and composites
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Dave EvansAdvanced Cryogenic Materials Ltd
(davidevans276@btinternet.com)
Radiation Damage in Resins and Composites
1
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Copyright statement and speaker’s release for video publishing
The author consents to the photographic, audio and video recording of this lecture at the CERN Accelerator School. The term “lecture” includes any material incorporated therein including but not limited to text, images and references.
The author hereby grants CERN a royalty-free license to use his image and name as well as the recordings mentioned above, in order to broadcast them online to all registered students and to post them without any further processing on the CAS website.
The author hereby confirms that the content of the lecture does not infringe the copyright, intellectual property or privacy rights of any third party. The author has cited and credited any third-party contribution in accordance with applicable professional standards and legislation in matters of attribution.
Copyright statement and speaker’s release for video publishing
2
Outline
Ø Radiation Units and TypesØ Interaction of Radiation with materialsØ Classification of Plastics Materials
Ø Thermoplastics and ThermosetsØ Structure and Materials Selection Ø Effects of Radiation
Ø Mechanical, gas evolution, dimensional changes?Ø Irradiation Under Load Ø Electrical properties
3
Radiation Units
Ø The S.I. unit of absorbed dose is the Gray (Gy)Ø An energy equivalent of one Joule absorbed in one
Kilogram Ø Non SI Unit – Rad; 1 Rad = 10-5 J/g = 10-2 Gy Ø 1 eV = 1.602 x 10-19 Joules ; 1 MeV = 1.602 x 10-13
Joules
Ø barn: Unit of area (10-28 m2 ) used in measurement of nuclear cross-sections
4
Radiation Types
ØNeutrons - particles with energy but no charge
ØElectromagnetic radiation such as g-rays
ØCharged particles - such as protons, electrons and a-particles (He2+)
5
Interaction of Radiation With Polymers
High energy particles lose energy and transfer it to polymer by:
Ø Ionisation - breaking chemical bondsØ Excitation -Separation of orbital electronsØ Nuclear Displacement Reactions - mainly fast
neutrons - leads also to ionisationØ Nuclear Transformation - Mainly slow neutronsØ Scattering and Emission
Ø Absorbed energy is degraded and appears as heatØ Energy deposition is characterised by LET
6
Linear Energy Transfer
Ø Rate of energy loss of a particle depends only on it's speed and charge and not on it's mass.
Ø Protons and alpha particles will react in a similar manner to electrons of the same velocity and charge.
Ø Difference in mass means that the penetration of a 20 MeV proton is comparable with that of a 10 keV electron.
Ø Since the LET is increased as the particle is slowed, uniform radiation conditions, apply only if the specimen is considerably thinner than the range of the incident particle.
Ø7
Fast Neutrons - 1
Ø Fast Neutrons are intensely damaging
Ø Major result is production of fast protons
Ø Energy transfer to other atoms may break chemical bonds
Ø Re-coiled neutron may still have sufficient energy to break more bonds
8
Fast Neutrons 2
Ø Ø Deposit Energy by collisionsØ Et = 4 x M (E Cos 2 q)
(M+1)2
Nucleus MassEnergy
Transfer (%)Hydrogen 1 100
Carbon 12 28Nitrogen 14 25Oxygen 16 22
9
Slow Neutrons
Ø Most elements have larger capture x - section for slow neutrons than for fast - result is nuclear transformation reactions:
Ø After capture nucleus may be unstable: (capture X-section of hydrogen 80 barns)H(1) (n,g)D(2) N(14) (n,p) C(14)2.2 MeV g 0.66 MeV proton
B(10) (n,a) Li(7) (B capture X-Section 700 barns)Boron gains 1 amu and loses 4 (a high energy alpha
particle) - a net loss 3 amu
10
Methane – A Special Case
Ø Hydrogen rich compound most efficient way to “slow” neutrons
Ø Methane (CH4) often used as a ‘moderator’; fast neutron irradiation leads to hydrogen gas and ‘wax’ like substance –eventually carbon!
Ø Hydrogen gas from hydrogen abstractionØ ESR measurements show H* & C*H3 in solid methane at 4K
after irradiation at that temperatureØ Under similar conditions H* NOT detected in PE or other
polymersØ Activated atoms lead to polymer formation and ultimately
carbonization
11
Neutron Fluence and Dose Conversion –Energy Deposited (1st Collision)
1.E-18
1.E-17
1.E-16
1.E-15
1.E-14
1.E-02 1.E-01 1.E+00 1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06 1.E+07Neutron Energy (eV)
Gy/
n/m
^2
N (capture)TotalHOC
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 12
Polymer Structures(radiation Resistance is related to
structure & Composition)
13
Relative atomic Sizes (Approximately)!
Hydrogen Carbon OxygenMethyl Group
Chlorine
Benzene nucleus
14
Some Thermoplastics
Ø Poly(ethylene) Poly(propylene)
Ø Poly(vinyl chloride)
15
Another Common Thermoplastics Material
16
More Complex Plastics Materials
17
Di-Functional Resins
Ø Typical commercial DGEBA, average value for n = 0.15
CH2 CH CH2
O
NCH2 CH CH2
O
Diglycidyl Aniline
C CH2 CH CH2
O
OCH2CH CH2
O
O
n
CH3
CH3
CH2 CH CH2
OH
C
CH3
CH3
O O
DGEBA
18
Epoxy Novolak Resins
CH2 CH CH2
O
2 O
n
CH2
CH2 CH CH
O
O
CH2
CH2 CH CH
O
O 2
Commercial EPN Resin (n= 0.4 avg) when n = 0, Resin is (pure) DGEBF
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 19
Tri-Functional Epoxy Resins
CH2 CH CH2
O
CH2 CH CH2
O
N
O
CH2 CH CH2
O
Low viscosity - brittle when cured
20
Tetra Functional Resins
H
H
N C
CH2-CH-CH2
O
CH2-CH-CH2
O
N
CH2-CH-CH2
O
CH2-CH-CH2
O
DETGDM
TGDM
H
H
C2H5
C2H5
N C
CH2-CH-CH2
O
CH2-CH-CH2
O
N
CH2-CH-CH2
O
CH2-CH-CH2
O
21
Cyanate Ester ResinTwo Reactive Groups(Di-Functional)
CH3
O CCH2-CH-CH2
O
CH2-CH-CH2
O
O
CH3
CH3
O C O
H
C NN C
Cyanate Ester Monomer (AroCy L-10)
DGEBA shown pure for clarity
Dave Evans – ACM Ltd – CEREN Accelerator School – Radiation Damage 22
Cyanate Ester – Ring Formation
CH3
O C O
H
C NN C
Dicyanate monomer
C
C C
N N
NOO
O Cyan. Est O NC
N OC Cyan. EstCyan. Est O NC
Trimerization
Triazine Ring
Totally cross-linked – leads to Radiation / Thermal Stability and High Tg
23
Solid Aromatic Amines
CH NH2NH2 2 DDM (MDA) (Suspected carcinogen)
S
O
O
NH2NH2DDS
24
Aromatic Amines - Liquids
3
C2H5NH2
C2H5
CH3
NH2
NH2
NH2
CH3
SCH
CH3S
DMTD Hardener AHEW 53.5
DETD Hardener AHEW 44.5
25
Anhydride Hardeners
CH CH
C CHCH3
CH2
CH2C
C
O
O
O
MNA 5 methyl 1,4 endomethylene cyclohexanoic anhydride CH CH
C CHCH3
CH
CHC
C
O
O
O
CH2
MTHPAmethyl tetra hydro phthalic anhydride
26
Results & Test Methodology
Mechanical Changes in Materials
27
Radiation Stability of Various Plastics Materials
0
5
10
15
20
25
30
PTFE
FEP
Butyl Rubber
Si Rubber
PVC
P/E
PETP
Neoprene
EVA
Halar
PP/XPE
EPR/EPDM
G10
G11
PI (Kapton
Material
Usea
ble
Rang
e (M
Gy)
Upper useable range for PTFE is 1000Gy and for FEP and Butyl Rubber is 20,000 GY
28
Radiation Effects in Resins
Ø Changes in Mechanical properties
Ø Particularly matrix dependent properties such as flexural strength and shear strength
Ø Classification of “Damage”
Ø Radiation induced gas evolution / swelling
Ø Effect of Temperature
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 29
Mechanical Changes 1. Flexural Strength
30
Radiation Effects in Materials (1)(Flexural Strength – Gamma Radiation – RT)
0
50
100
150
200
250
300
350
400
450
500
0.1 1 10 100 1000Radiation Dose (MGy)
Flex
ural
Stre
ngth
(MPa
)
DGA
DGEBAEpoxy Novolak
TGPAPTGDM
Anhydride cured Resins
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage
Rutherford Laboratory Report RHEL/R 200
31
Radiation Effects in Materials (2)(Flexural Strength – Gamma Radiation – RT)
0
50
100
150
200
250
300
350
400
450
500
0.1 1 10 100 1000
Radiation Dose (MGy)
Flex
ural
Stre
ngth
(MPa
)
DGADGEBAEpoxy NovolakTGPAPTGDM
Aromatic Amine Cured
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage
Rutherford Laboratory Report RHEL/R 200
32
Radiation Stability and Resin Structure
020406080
100120140160180200
0 1 2 3 4
Number of reactive Groups on Resin
Dos
e to
Red
uce
Stre
ngth
by
25 %
(MGy
)
Acid Anhydride Cured Resin
Aromatic Amine Cured Resin
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 33
Shear Testing
34
Stressful (Working)Lunch
35
Shear Strength Evaluation
Ø Many methods – each has it’s own problemsØ Major Techniques are :
Ø Guillotine – bending & stress concentrations
Ø Short beam shear – variation of 3-point bending test but short span – compression on one face tension on the other
Ø Shear / compression – said to be free of stress concentations – mainly used for adhesive properties
36
ILSS– G10Guillotine Method
0
20
40
60
80
100
120
0.00 0.50 1.00 1.50 2.00
Ratio - Shear Length to Thickness (l/t)
ILSS
(MPa
)
ILSS at 77K
ILSS at 300K
Constant Overlap - 12.7 mm (0.5 inches)
37
Reactor Irradiation at 5K(Short Beam Shear)
0
20
40
60
80
100
120
0.1 1 10 100
Total Dose (Gamma + Neutron) MGy
ILSS
(Sho
rt B
eam)
(MPa
)
DGEBA-AnhydrideTGDM-Aromatic Amine
0.9 E+22 neutrons / m 2̂
1.8 E+22 n/m 2̂
1.5e+201e+20 1e+21
1.5e+21 1e+22
Neutron Fluence (E> 0.1 Mev)
R.P. Reed et al – US ITER Radiation program -sponsored by US Office of Fusion Energy)
38
SBS With and Without Kapton(R.P. Reed et al – US ITER Radiation program - sponsored by US Office of Fusion Energy)
Radiation Dose (n/m2) (Mgy)
ILSS (Mpa) (SBS) No Kapton 0° 90°
ILSS (Mpa) (SBS)
Kapton 0° 90
Ratio UTS/ILSS No Kapton 0° 90°
Ratio UTS/ ILSS
Kapton 0° 90°
0
80
77
81
75
11 4.5
9.3 5.2
5 x 1021
(~25) 44
37
50
45
18 ---
13 ---
1 x 1022
(~50) 31
24
35
27
22 4.8
14 8.0
Tape Wound Samples, partly purified DGEBA – unspecified hardener
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 39
Tests in Shear Compression
Ø Test is ‘free” of stress concentrationsØ Many tests carried out RT and at 4KØ Little data on radiation stable materialsØ No comparison between 4k and RT irradiation (except
for samples with mica barrier) ???Ø For DGEBA cured with Acid Anhydride:
Ø Test at 4K – no irradiation (45 angle) 190 MpaØ Test at 4K irradiated at 4K* (45 angle) 26 MPa* Reactor irradiated 1.8 x 1022 n/m2 (~67 MGy)
40
Gas Evolution & Swelling
41
Radiation – Effectof Temperature
00.05
0.10.150.2
0.250.3
0.350.4
0 100 200 300 400
Temperature (K)
G Va
lue
(micro
moles
/ J
)
Gas evolution from ld polyethylene
8.6 cc/g/MGy (300K)
6.7cc/g/MGy (240K)
Dave Evans - ACM Ltd – CERN Accelerator School – Radiation Damage 42
Gas Evolution & Reactor Irradiation(Evans & Reed, Adv. Cry. Eng. Vol 42, 29 – 35)
Resin Hardener Gas(cc/g/MGy)
DGEBF DETD 0.58DGEBF DMTD 2.32TGPAP DETD 0.58DETGDM DETD 0.91DETGDM DMTD 2.78DGEBA DDM 0.30
For Reference: DGEBF/MTHPA 1.08cc/g/MGy from Reactor Irradiation – polyethylene dosimeter
Dave Evans - ACM Ltd – CERN Accelerator School – Radiation Damage 43
Composition of Radiation Induced Gasses
(Generalised and approximating)
Ø Amine Cured (aliphatic or aromatic):90% hydrogen, 10% carbon monoxide
Ø Acid Anhydride cured:20% hydrogen, 20% carbon monoxide, 60%
carbon dioxide
44
Is Gas Trapped in Bulk Specimens?(Evans & Reed, Adv. Cry. Eng. Vol 42, 29 – 35)
Ø Bulk means ~ 7 mm cube
Material Gas Production Rate Cc’s / g/MGy
True * Bulk**
% Gas Trapped
DGEBF/MTHPA 1.03 0.47 53 DGEBF / DETD 0.58 0.44 24 TGPAP / MTHPA 1.10 0.64 42 TGPAP / DETD 0.58 0.64 0
* Rate from powdered sample ** Rate from 7 x 7 x 7 cubes
Dave Evans – ACM Ltd - CERN Accelerator School – Radiation Damage 45
Swelling & Reactor Irradiation at 5K(Humer et al - Cryogenics, 40 , pp 295-301)
DGEBF / Anhydride
-2
0
2
4
6
8
10
0.1 1 10 100
Calculated Dose (MGy)
Swell
ing %
Thin LaminateThin Sandwich
Thin Tube
1E+21
1.5E+21
1.0E+22
If glass is ~50 vol% - swelling in resin phase is double composite What is stress in composite? (720 MPa if E = 9 GPa)
0.5mm thick specimens
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 46
Swelling and Mass Loss (20 MGy)Reactor Irradiation at 5K – Unfilled Resin
(Evans & Reed, Adv. Cry. Eng. , Vol. 46, pp 211 - 218)
Resin Hardener Change in Properties (%) Diam Length Mass
Mass Change % / MGy
DGEBF MTHPA -0.1 0.0 -0.8 -0.04 EPN MTHPA 0.3 0.0 -1.0 -0.05 DGEBF DETD 0.1 0.2 -0.1 < -0.01 DGEBA DETD 0.0 0.2 -0.1 < -0.01 TGDM DDS 0.0 0.3 -0.1 < -0.01 TGPAP DETD 0.3 0.3 0.0 <-0.01 DGEBA MTHPA -0.1 -0.2 -0.8 -0.04 TGPAP MTHPA 0.5 -0.1 -0.7 -0.04
No Change in Young’s Modulus (compression) after Irradiation
10 mm diam x 10 mm long cast and machined resin samples
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage
0.00.0 0.0
47
The Last Word on Swelling
Ø Available data is very confusing – my viewis that swelling doesn’t occur in epoxies or CE at dose levels reported’
Ø WHY – what happens to gas?Ø No new material created – gas is from atoms already
presentØ Molecules possibly ‘trapped’ in area of formation (‘cage
effect’)Ø Gas is ‘in solution’ – does not occupy a separate volume
within resin
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 48
Creep and Radiation
49
The Real World
“---- that some discussion be focussed on integrating the insulation materials results with magnet design and operation issues. In other words, cover more than just insulation properties but also how these impinge on coil fabrication or operation. How do properties measured on small samples relate to properties in large scale impregnated coil cross-sections under multi-dimensional loads, including combined mechanical, thermal and radiation loads ---“ Joe Minervini
(Assistant Director, MIT Plasma Fusion Center)
50
Irradiation at 5K – DGEBF / Anhydride(Evans & Reed Adv. Cry. Eng. Vol 44, 183 - 190 )
Neutron Fluence (E.0.1 MeV
Stress During Irradiation (MPa)
Failure Stress (MPa)
0 (control) 0 172 5 x 1021 0 124 5 x 1021 30 105 1 x 1022 30 92
Dave Evans – ACM Ltd - CERN Accelerator School – Radiation Damage 51
Irradiation at 5K – TGDM / Aromatic Amine(Evans & Reed Adv. Cry. Eng. Vol 44, 183 - 190 )
Neutron Fluence (E.0.1 MeV
Stress During Irradiation (MPa)
Failure Stress (MPa)
0 (control) 0 162 5 x 1021 0 157 5 x 1021 30 139 1 x 1022 30 122
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 52
Creep at 77K of Irradiated Material(Nishiura T et al - Cryogenics, Vol. 35, No. 11, pp 747 – 749)
Creep of Irradiated GRP (5 MGy)
0.00
0.50
1.00
1.50
2.00
2.50
0.00 50.00 100.00 150.00 200.00 250.00 300.00
Time (Minutes)
Cree
p De
flecti
on (m
m)
403 MPa278 MPa
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 53
Creep During Irradiation at 77K(Nishiura T, et al - Cryogenics, Vol. 35, No. 11, pp 747 – 749)
0.00
0.05
0.10
0.15
0.20
0.25
0.30
0.00 50.00 100.00 150.00 200.00 250.00
T ime (Minutes)
Cree
p De
flect
ion
(mm
) 370 MP a204 MP a
125 MP a
Dose Rate 1.5MGy / Hour
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 54
Creep Rates
Irradiation Conditions
Stress Level (MPa)
Creep Rate (mm/minute)
Pre-Irrad* 278 <5 x 10-5 Pre-Irrad* 403 ~9 x 10-5
During Irrad** 125 1.5 x 10-4
During Irrad** 204 4.5 x 10-4
During Irrad** 370 9.0 x 10-4
* Pre-Irradiated 5 MGY, ** Total during irradiation ~ 6MGy
Dave Evans – ACM Ltd – CEDRN Accelerator School – Radiation Damage 55
A Quick Look at Electrical Properties
56
Electrical Properties and Radiation
0.0
10.0
20.0
30.0
40.0
50.0
60.0
70.0
80.0
90.0
100.0
0.1 1 10 100
Calculated Dose (MGy at 5K)
Diel
ectr
ic S
tren
gth
(kV/
mm)
Laminate
Sandwich
1 x 1021 n/m2 5 x 1021 n/m2 1 x 1022 n/m2
Dave Evans – ACM Ltd – CERN Accelerator School – Radiation Damage 57
Summary
Ø High functionality promotes radiation stability Ø Aromaticity (resin or hardener) also promotes
stabilityØ Best Epoxies -up to 200 MGy – CE even moreØ Some synergism between irradiation under stressØ Gas volumes and composition related to structureØ Results on swelling are scattered and confusing – on
balance no swelling up to 100 MGyØ No significant change in electrical properties – up to
~ 100 MGy – no apparent relationship with structure
58
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