ASTM D7028-07 (2024) 通过动态力学分析(DMA)测定聚合物基复合材料玻璃化转变温度(DMA Tg)的标准试验方法

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Designation: D7028 07 (Reapproved 2024)
Standard Test Method for
Glass Transition Temperature (DMA Tg) of Polymer Matrix
Composites by Dynamic Mechanical Analysis (DMA)
1
This standard is issued under the fixed designation D7028; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope
1.1 This test method covers the procedure for the determi-
nation of the dry or wet (moisture conditioned) glass transition
temperature (T
g
) of polymer matrix composites containing
high-modulus, 20 GPa (> 3 × 10
6
psi), fibers using a dynamic
mechanical analyzer (DMA) under flexural oscillation mode,
which is a specific subset of the Dynamic Mechanical Analysis
(DMA) method.
1.2 The glass transition temperature is dependent upon the
physical property measured, the type of measuring apparatus
and the experimental parameters used. The glass transition
temperature determined by this test method (referred to as
“DMA Tg”) may not be the same as that reported by other
measurement techniques on the same test specimen.
1.3 This test method is primarily intended for polymer
matrix composites reinforced by continuous, oriented, high-
modulus fibers. Other materials, such as neat resin, may require
non-standard deviations from this test method to achieve
meaningful results.
1.4 The values stated in SI units are standard. The values
given in parentheses are non-standard mathematical conver-
sions to common units that are provided for information only.
1.5 This standard does not purport to address all of the
safety concerns, if any, associated with its use. It is the
responsibility of the user of this standard to establish appro-
priate safety, health, and environmental practices and deter-
mine the applicability of regulatory limitations prior to use.
1.6 This international standard was developed in accor-
dance with internationally recognized principles on standard-
ization established in the Decision on Principles for the
Development of International Standards, Guides and Recom-
mendations issued by the World Trade Organization Technical
Barriers to Trade (TBT) Committee.
2. Referenced Documents
2.1 ASTM Standards:
2
D3878 Terminology for Composite Materials
D4065 Practice for Plastics: Dynamic Mechanical Proper-
ties: Determination and Report of Procedures
D4092 Terminology for Plastics: Dynamic Mechanical
Properties
D5229/D5229M Test Method for Moisture Absorption Prop-
erties and Equilibrium Conditioning of Polymer Matrix
Composite Materials
E177 Practice for Use of the Terms Precision and Bias in
ASTM Test Methods
E691 Practice for Conducting an Interlaboratory Study to
Determine the Precision of a Test Method
E1309 Guide for Identification of Fiber-Reinforced
Polymer-Matrix Composite Materials in Databases (With-
drawn 2015)
3
E1434 Guide for Recording Mechanical Test Data of Fiber-
Reinforced Composite Materials in Databases (Withdrawn
2015)
3
E1471 Guide for Identification of Fibers, Fillers, and Core
Materials in Computerized Material Property Databases
(Withdrawn 2015)
3
E1640 Test Method for Assignment of the Glass Transition
Temperature By Dynamic Mechanical Analysis
E1867 Test Methods for Temperature Calibration of Dy-
namic Mechanical Analyzers
3. Terminology
3.1 Definitions—Terminology D3878 defines terms relating
to polymer matrix composites. Terminology D4092 defines
terms relating to dynamic mechanical property measurements
on polymeric materials.
3.2 Symbols: E’ = storage modulus
E” = loss modulus
1
This test method is under the jurisdiction of ASTM Committee D30 on
Composite Materials and is the direct responsibility of Subcommittee D30.04 on
Lamina and Laminate Test Methods.
Current edition approved Jan. 1, 2024. Originally approved in 2007. Last
previous edition approved in 2015 as D7028 – 07
ε1
(2015). Published January 2024.
DOI: 10.1520/D7028-07R24.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website.
3
The last approved version of this historical standard is referenced on
www.astm.org.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the
Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
1
tan δ=E”/E’ = tangent delta
DMA Tg = glass transition temperature defined from dy-
namic mechanical analysis measurement
L= length of specimen
W= width of specimen
T= thickness of specimen
T
t
= peak temperature from tangent delta curve
4. Summary of Test Method
4.1 A flat rectangular strip of laminate is placed in the DMA
equipment and oscillated at a nominal frequency of 1 Hz. The
specimen is heated at a rate of 5 °C ⁄min (9 °F ⁄min). The same
loading frequency and heating rate is used for both dry and wet
specimens (moisture conditioned) to allow for comparison.
The temperature at which a significant drop in storage modulus
(E’) begins is assigned as the glass transition temperature
(DMA Tg). The peak temperature of the tangent delta curve
(T
t
) is identified along with DMA Tg for comparison purposes.
5. Significance and Use
5.1 This test method is designed to determine the glass
transition temperature of continuous fiber reinforced polymer
composites using the DMA method. The DMA Tg value is
frequently used to indicate the upper use temperature of
composite materials, as well as for quality control of composite
materials.
6. Interferences
6.1 The standard testing machine shall be of the Dynamic
Mechanical Analysis (DMA) type of instrument that operates
with forced oscillation and applies a flexural loading mode
(either three-point bend or dual cantilever) to the test specimen.
Refer to Practice D4065 for a summary of various other DMA
practices. Other loading modes (such as tensile, torsion or
shear) may produce different test results. If another equipment
type or loading mode is used the non-standard approach shall
be described in the report and the test result recorded as
non-standard.
6.2 A fixed frequency of 1 Hz is standard in this test method.
In general, for a given material, a higher testing frequency
produces a higher DMA Tg value than this standard, while use
of the resonance mode will yield a different DMA Tg that may
be either higher or lower than the standard. If a non-standard
frequency, or the resonance mode, is used, the non-standard
approach shall be described in the report and the test result
recorded as non-standard.
6.3 A heating rate of 5 °C ⁄min 61 °C ⁄min (9 °F ⁄min 6
2 °F ⁄min) is standard in this test method. A change in heating
rate will affect the glass transition temperature result; the
standard heating rate is the best available compromise for
comparing DMA Tg results of dry and wet laminates. If a
different heating rate is used it shall be described in the report
and the result recorded as non-standard.
NOTE 1—Users should be advised that a heating rate of 5 °C ⁄min
represents a compromise between various issues related to Tg measure-
ment precision and bias. It is widely known that heat transfer limitations
are more pronounced in DMA apparatus compared to other thermal
analysis techniques, such as differential scanning calorimetry (DSC) and
thermomechanical analysis (TMA). For greatest precision, it has been
recommended that heating rates be 2 °C ⁄min or less. Test Method E1640
specifies a heating rate of 1 °C ⁄min. However, in many cases 5 °C ⁄min is
recommended as a compromise between Tg measurement accuracy and
test method convenience, especially for wet laminate measurements, since
the slower heating rate will cause specimen drying that will itself bias the
results.
6.4 Purge gas type and flow rate and the position of the
thermocouple can affect the DMA Tg test result and shall be
noted and reported. The same conditions shall be used for both
calibration and testing runs. Instrumentation manufacturer
recommendations should be followed.
6.5 It is standard in this test method that one of the major
fiber directions shall be parallel to the length of the specimen.
The span-to-depth ratio, ply orientation, and ply stacking
sequence of a specimen with respect to the testing fixture have
a profound effect on the DMA Tg result. A meaningful
comparison of data requires that the specimen configuration be
the same. A non-standard specimen configuration shall be
described in the report and the result recorded as non-standard.
6.6 The standard definition in this test method for DMA Tg
is based on intersecting two tangent lines from a semi-
logarithmic plot of the storage modulus versus temperature.
Other T
g
definitions typically produce different test results. For
example, a linear plot scale will result in a lower value of DMA
Tg. A non-standard DMA Tg definition shall be described in
the report and the result recorded as non-standard. For com-
parison purposes the peak temperature of the tangent delta
curve (T
t
) is identified along with DMA Tg.
7. Apparatus
7.1 Micrometer, suitable for reading to 0.025 mm (0.001 in.)
accuracy for measuring the specimen thickness and width.
7.2 Caliper, suitable for reading to 0.025 mm (0.001 in.)
accuracy for measuring the specimen length and instrument
clamping distance.
7.3 Dynamic Mechanical Analyzer (DMA), with oven ca-
pable of heating to above the glass transition temperature and
of controlling the heating rate to the specified value.
8. Sampling and Test Specimens
8.1 Two specimens shall be tested for each sample. If the
testing is part of a designed experiment, other sampling
techniques may be used if described in the test plan.
8.2 Consult the instrument manufacturers manual for speci-
men size. A span-to-thickness ratio greater than ten is recom-
mended. Specimen absolute size is not fixed by this method as
various dynamic mechanical analyzers require different sizes.
Depending on the analyzer, typical specimen size can range
from 56 64 × 12 61 × 2.0 60.5 mm (2.21 60.16 × 0.47
60.04 × 0.08 60.02 in.) (L × W × T) to 22 61×361 ×
1.0 60.5 mm (0.9 60.04 × 0.12 60.04 × 0.04 60.02 in.).
8.3 One of the major fiber directions in the specimen shall
be oriented along the length axis of the specimen. It is standard
that one of the major fiber directions shall be parallel to the
length of the specimen, and specimens containing only off-axis
D7028 − 07 (2024)
2
plies shall not be used. Any deviations from the standard
orientation shall be reported and the test results noted as
non-standard.
8.4 The specimen surfaces shall be flat, clean, straight, and
dry to prevent slippage in the grips and mitigate any effects due
to moisture. Opposite surfaces must be essentially parallel and
intersecting surfaces perpendicular. Tolerances in thickness and
width must be better than 62 %.
8.5 The selected sample shall be taken from a representative
portion of the laminate. Laminate edges or other irregularities
created in the laminate by mold or bagging techniques should
be avoided.
9. Calibration
9.1 The DMA equipment shall be calibrated in accordance
with Test Method E1867 for temperature signals and in
accordance with the equipment manufacturers recommenda-
tion for the storage modulus. The equipment must be calibrated
in the same loading mode as will be used for testing, either dual
cantilever or three-point bending. The temperature calibration
points must span the DMA Tg result.
10. Conditioning
10.1 Moisture has significant effect on DMA Tg. Therefore,
it is recommended that the test specimens should be weighed
before and after DMA Tg testing to quantify the moisture
change in the specimen resulting from the DMA Tg test.
10.2 Dry Specimens—To minimize the presence of moisture
in the specimens, dry specimens must be conditioned prior to
testing by using either of the following techniques:
10.2.1 Dry the specimens in an oven in accordance with
Test Method D5229/D5229M, Procedure D, then stored until
test in a desiccator or sealed MIL-PRF-131
4
(or equivalent)
aluminized bag, or
10.2.2 Store the material in a desiccator or sealed alumi-
nized bag immediately after material curing (lamination),
where the material shall remain except for the minimum time
required for removal during specimen preparation and testing.
The maximum time between cure (lamination) and testing shall
be 30 days, after which, prior to testing, specimens shall be
oven-dried in accordance with 10.2.1.
10.3 Wet Specimens—Condition in accordance with Test
Method D5229/D5229M, Procedure B. The conditioned speci-
mens shall be tested within 30 minutes after removal from the
conditioning chamber, or stored in sealed MIL-PRF-131 (or
equivalent) aluminized bag until test.
11. Procedure
11.1 Test Specimen—Measure the specimen thickness and
width to 0.025 mm (0.001 in.) and record. Measure the
specimen length to 0.025 mm (0.001 in.) and record. Weigh the
specimen to the nearest milligram (0.001 g) and record.
11.2 Specimen Installation—Install the specimen in the
DMA test equipment oven based upon clamping method to be
employed.
11.3 Positioning of Specimen—Follow the manufacturers
procedure for positioning the specimen in the clamps.
Generally, the specimen should be centered between the clamp
faces and be parallel to the base of the instrument. Mount the
specimen in dual cantilever mode or three-point bending mode.
11.4 Heating Rate—The standard heating rate is 5 °C ⁄min
61 °C ⁄min (9 °F ⁄min 62 °F ⁄min). The same heating rate
shall be used for all samples whose results are to be compared.
Any deviations from this heating rate shall be noted in the
report and the result shall be reported as non-standard.
11.5 Frequency—The standard frequency to be used in this
standard is 1 Hz, and the instrument should be operated in
constant strain mode.
11.6 Strain Amplitude—The maximum strain amplitude
should be kept within the linear viscoelastic range of the
material. Strains of less than 0.1 % are standard.
11.7 Temperature Range—Program the run to begin at room
temperature or a temperature at least 50 °C (90 °F) below the
estimated DMA Tg and to end at a temperature at least 50 °C
(90 °F) above DMA Tg, but below decomposition temperature.
11.8 Purge Gas Flow Rate—Follow the manufacturers
manual or recommendations to set the purge gas flow rate. Five
litres/minute (0.2 CFM) is a typical purge gas flow rate setting.
For some types of dynamic mechanical analyzers, a purge gas
flow setting is not required.
11.9 Thermocouple Positioning—Follow the manufacturers
manual or recommendations to position the thermocouple.
Typically the thermocouple should be as close to the sample as
possible.
11.10 Test—Conduct DMA Tg measurements using the
instrument settings specified and record the load and displace-
ment data as a function of temperature. Allow the oven to cool
before removing the specimen. Weigh the specimen after the
test to the nearest milligram (0.001 g) after the removal from
the oven and record.
11.11 Specimen Examination—Examine the specimen after
the test and inspect for any visual anomalies (that is,
delamination, blisters, cracks, etc.). Record any visual anoma-
lies observed.
12. Interpretation of Results
12.1 Glass Transition Temperature (DMA Tg)—Plot the
logarithm of storage modulus (E’) and linear tangent delta (tan
δ) versus the linear temperature (Fig. 1). During the glass
transition, the storage modulus of the composite material is
significantly reduced. The DMA Tg is determined to be the
intersection of two tangent lines from the storage modulus by
this test method. The first tangent line (Line A, Fig. 1) is
selected at a temperature before the transition. This tempera-
ture is designated as TA. The second tangent line (Line B, Fig.
1) is constructed at the inflection point to approximately the
midpoint of the storage modulus drop. This temperature is
4
MIL-PRF-131, Barrier Materials, Watervaporproof, Greaseproof, Flexible,
Heat-Sealable. Available at http://assist.daps.dla.mil or from the Standardization
Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA
19111-5094.
D7028 − 07 (2024)
3
摘要:

ASTM D7028-07 2024 Standard Test Method for Glass Transition Temperature (DMA Tg) of Polymer Matrix Composites by Dynamic Mechanical Analysis (DMA) 通过动态力学分析(DMA)测定聚合物基复合材料玻璃化转变温度(DMA Tg)的标准试验方法

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