Permeation Investigation of Carbon Fibre Reinforced Polymer Material for LH2 Storage Thermally Shocked and Mechanically Cycled at Cryogenic Temperature
Abstract
:1. Introduction
2. Materials
Samples Preconditioning
3. Methods
3.1. Helium and Hydrogen
3.2. Theoretical Fickian Diffusion
- The concentration at the feed side is referenced as ;
- The concentration at the permeate side is referenced as ;
- At , the concentration is applied as a constant: ;
- For every t, and .
3.3. Test Setup
3.4. Permeation Testing Methodology
- Assemble gaskets and the specimen concentrically in the sample holder.
- Tighten the sample holder assembly and connect the upper and lower chambers to the respective instrumentation tubing.
- Run preliminary checks. Apply vacuum to both the upper and lower chambers and make sure the required pressure is reached (in this case, selected at mbar), so as to make sure that all connections are sufficiently vacuum-tight. Then, run pressure tightness checks in the upper chamber by increasing the pressure within the tubing, closing necessary valves and verifying that the pressure inside the tubing assembly does not drop rapidly. This ensures that no gross leaks are present.
- Evacuate the upper chamber tubing assembly at least 5 times if all previous preliminary checks are successful.
- Start pulling vacuum and testing on the lower chamber with ASM340.
- Increase the tracer gas pressure in the upper chamber assembly to the desired amount, making sure that the same pressure will be delivered for the whole duration of the test.
- Start recording on ASM340.
- Convert the leak rate value from to by dividing if by a factor of 10 [32].
- Convert in the surface area (A) of the specimen exposed to the tracer gas.
- Convert in K the temperature (T) at which the test was carried out.
- Calculate the thickness of the specimen (l) in m.
- Calculate the gas transmission rate (GTR) with the following equation:
- Calculate the difference in partial pressure of the permeating gas between the upper and lower chambers ( in ).
- Calculate permeance () by dividing the GTR by ().
- Calculate the permeation coefficient by multiplying the permeance by the thickness of the specimen.
4. Results
5. Discussion
6. Conclusions
- A Fickian behavior investigation was performed on carbon fiber-reinforced thermoset and thermoplastic materials with specimens subjected to different preconditioning scenarios. Diffusion coefficients were calculated for every preconditioning scenario.
- The Fickian investigation on permeation measurements allowed us to identify material inhomogeneities undetectable by permeation coefficient or leak rate measurements alone and link them to specific preconditioning. This result could aid further research on similar investigations, where other methods to evaluate the material’s homogeneity cannot be implemented.
- The use of coefficient of determination as an objective method to evaluate and categorize Fickian, near-Fickian, and non-Fickian permeation behaviors needs to always be performed in conjunction with subjective evaluation of the main experimental permeation diffusion features (time lag, transient state, steady state) and compared to their respective theoretical ones.
- A methodology to improve the evaluation of correct testing time and steady-state leak rate determination is suggested.
- Cryogenic mechanical loading was demonstrated to be a more effective preconditioning method with respect to cryogenic thermal cycles alone.
Future Work
Author Contributions
Funding
Data Availability Statement
Acknowledgments
Conflicts of Interest
References
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Material ID | Layup | Diameter [mm] | Thickness [mm] | Fiber Content [%] |
---|---|---|---|---|
P1 | 50 ± 0.5 | 2.09 ± 0.14 | 64.5 | |
P2 | - | 50 ± 0.5 | 4 ± 0.10 | 20 |
Material System | Preconditioning ID | Cryogenic Cycles | Mechanical Cycles to 4500 @77 K |
---|---|---|---|
P1 | N0-M0 | 0 | 0 |
P1 | N1-M0 | 1 | 0 |
P1 | N5-M0 | 5 | 0 |
P1 | H0-M50 | 0 | 50 |
P1 | H5-M50 | 5 | 50 |
Behavior | Non-Fickian | Near-Fickian | Fickian |
---|---|---|---|
Range |
Material System | Preconditioning ID | Sample ID | Behavior |
---|---|---|---|
P1 | N0-M0 | S1 | Fickian |
S2 | Near-Fickian | ||
S3 | Fickian | ||
P1 | N1-M0 | S1 | Fickian |
S2 | Fickian | ||
S3 | Fickian | ||
P1 | N5-M0 | S1 | Fickian |
S2 | Fickian | ||
S3 | Fickian | ||
P1 | H0-M50 | S1 | Non-Fickian |
S2 | Fickian | ||
S3 | Near-Fickian | ||
P1 | H5-M50 | S1 | Near-Fickian |
S2 | Near-Fickian | ||
S3 | Non-Fickian | ||
P2 | H0-M0 | S1 | Fickian |
S2 | Fickian |
Material System | Preconditioning ID | Diffusivity Avg. | Diffusivity St. Dev. |
---|---|---|---|
P1 | N0-M0 | 2.72 | 3.97 |
P1 | N1-M0 | 3.08 | 1.03 |
P1 | N5-M0 | 1.85 | 6.6 |
P1 | H0-M50 | 3.24 | 9.74 |
P1 | H5-M50 | 4.12 | 1.49 |
P2 | H0-M0 | 2.36 | 8 |
N0-M0 | N1-M0 | N5-M0 | H0-M50 | H5-M50 | |
---|---|---|---|---|---|
Minimum | 1.49 | 1.83 | 1.49 | 1.01 | 8.74 |
Maximum | 2.28 | 2.89 | 2.07 | 1.87 | 1.91 |
Average | 1.79 | 2.44 | 1.80 | 1.41 | 1.43 |
Standard Deviation | 2.96 | 4.42 | 2.41 | 3.55 | 4.26 |
Coefficient of Variation [%] | 16.6 | 18 | 13.4 | 25.2 | 29.8 |
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Dreossi, G.; Horvat, A.B. Permeation Investigation of Carbon Fibre Reinforced Polymer Material for LH2 Storage Thermally Shocked and Mechanically Cycled at Cryogenic Temperature. Aerospace 2025, 12, 342. https://doi.org/10.3390/aerospace12040342
Dreossi G, Horvat AB. Permeation Investigation of Carbon Fibre Reinforced Polymer Material for LH2 Storage Thermally Shocked and Mechanically Cycled at Cryogenic Temperature. Aerospace. 2025; 12(4):342. https://doi.org/10.3390/aerospace12040342
Chicago/Turabian StyleDreossi, Giacomo, and Andrej Bernard Horvat. 2025. "Permeation Investigation of Carbon Fibre Reinforced Polymer Material for LH2 Storage Thermally Shocked and Mechanically Cycled at Cryogenic Temperature" Aerospace 12, no. 4: 342. https://doi.org/10.3390/aerospace12040342
APA StyleDreossi, G., & Horvat, A. B. (2025). Permeation Investigation of Carbon Fibre Reinforced Polymer Material for LH2 Storage Thermally Shocked and Mechanically Cycled at Cryogenic Temperature. Aerospace, 12(4), 342. https://doi.org/10.3390/aerospace12040342