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Impact of Coating Brittleness on Superalloy Performance

Examining how NiAl coating brittleness affects nickel-based superalloy durability.

― 4 min read


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Table of Contents

Coating materials play a crucial role in protecting superalloys used in high-temperature environments, such as in jet engines. One common type of coating is nickel aluminide (NiAl), which can help preserve the underlying metal. However, the brittleness of the coating can be a concern, especially when subjected to different temperature conditions during their operation. This article discusses how the brittleness of NiAl coatings affects the performance of a specific nickel-based superalloy, Rene 125, under thermomechanical fatigue.

Coating Brittleness and Thermomechanical Fatigue

Thermomechanical fatigue (TMF) occurs when materials are subjected to repeated cycles of heat and mechanical stress. This condition can cause damage over time, leading to failures. The behavior of the coatings under such conditions is critical for ensuring long-lasting materials in high-temperature environments. Investigating how coating brittleness influences the overall performance helps in predicting the lifespan of these components.

Testing Methods

Sample Preparation

To understand how the coating behaves under stress, samples of Rene 125 superalloy coated with NiAl were made. These were treated at 870 degrees Celsius to ensure a well-formed coating. The samples were then subjected to different aging processes to see how varying conditions affect coating performance and Microstructure.

Aging Treatments

The coatings were aged under two conditions: isothermal and thermal cycling. In isothermal aging, the samples were held at a constant temperature. In thermal cycling, samples underwent repeated heating and cooling between low and high temperatures, simulating service conditions.

Observations of Coating Behavior

Initial State

The coatings were found to be brittle at lower temperatures, specifically below 700 degrees Celsius. This brittleness can lead to cracks forming through the thickness of the coating during regular service cycles. Once the temperature exceeds this range, the coatings can become more ductile, showing improved performance.

Microstructure Changes

As the coating ages, its microstructure evolves. This change can either improve or worsen the coating's performance. The main structural change observed was the transformation of the coating from a brittle phase to a more ductile one, which is beneficial for overall durability.

Impact of Aging

Aging treatments helped improve strain-to-failure measures, particularly at room temperature. For low aging conditions, the performance remained similar to the as-received state. However, with increased aging time and temperature, cracks were observed to be less severe and more localized.

Mechanical Testing

Tensile Testing

Tensile tests were carried out to evaluate how stress affected the samples. Differences in performance were noted based on the aging conditions, with greater ductility observed in samples subjected to longer aging times.

Digital Image Correlation

Advanced imaging techniques, such as digital image correlation, were used to monitor the development of cracks during testing. These techniques allowed for precise measurements of strain and helped identify where the first cracks initiated.

Effects of Temperature and Aging

Strain-to-Failure

The studies showed that the strain-to-failure, which is the amount of stress that the coating can withstand before failing, improved significantly after aging. This suggests that the aging process plays a key role in enhancing the coating's ability to resist cracking.

Brittle-to-Ductile Transition

An important aspect is the transition from brittle to ductile behavior as the temperature increases. The observations indicated that as the temperatures rose, the coatings began to show improved ductility, especially after undergoing appropriate thermal aging.

Observations from Aging Treatments

Isothermal Aging

In isothermal aging, the impact of prolonged exposure to high temperatures led to the formation of a more stable microstructure. The coatings exhibited improved resistance to cracking, demonstrating that the aging process has a significant effect on their overall performance.

Thermal Cycling

When subjected to thermal cycling, the coatings underwent significant changes in microstructure, leading to fluctuations in performance. The cycling introduced challenges, particularly with shorter dwell times, which could be detrimental to the coating's integrity.

Conclusion

Coating brittleness has a direct impact on the thermomechanical fatigue behavior of nickel-based superalloys. Through various aging treatments, it is possible to enhance the performance of coatings, shifting them from brittle to ductile behavior, thus improving their long-term durability. Monitoring these changes through mechanical testing and modern imaging techniques provides valuable insights for developing more reliable coatings in high-temperature applications.

Importance of Findings

Understanding the relationship between coating brittleness and thermomechanical fatigue is crucial for designing more effective protective layers. By optimizing the aging conditions, manufacturers can improve the lifespan of components and reduce the risk of failure under operational stresses.

Future Research Directions

Further investigations are needed to explore the long-term effects of aging on various coating materials. By expanding the range of temperatures and testing conditions, more comprehensive data can be gathered to enhance the design of coatings that better withstand harsh environments.

Original Source

Title: Influence of the coating brittleness on the thermomechanical fatigue behavior of a $\beta$-NiAl coated R125 Ni-based superalloy

Abstract: The brittleness of an aluminide diffusion coating protecting a Ren\'e 125 Ni-based polycrystalline superalloy was investigated over a wide range of temperatures in its as-received and thermally aged form. Isothermal and thermal cycled aging were performed on the coated system at a maximum temperature of 1100 {\deg}C. Microstructure evolutions and damage initiation within the coating were characterized. Interrupted tensile tests and thermomechanical fatigue tests were conducted to document critical stress-strain conditions leading to the coating cracking and lifetime for the case of thermo-mechanical fatigue loading. Advanced digital image correlation and acoustic emission techniques were used to detect coating cracking. Isothermal oxidation or cyclic oxidation led to improved strain-to-failure due to metallurgical evolutions and also longer fatigue life under thermomechanical fatigue conditions.

Authors: Capucine Billard, Damien Texier, Matthieu Rambaudon, Jean-Christophe Teissedre, Noureddine Bourhila, Dimitri Marquie, Lionel Marcin, Hugo Singer, Vincent Maurel

Last Update: 2024-06-18 00:00:00

Language: English

Source URL: https://arxiv.org/abs/2406.13070

Source PDF: https://arxiv.org/pdf/2406.13070

Licence: https://creativecommons.org/licenses/by/4.0/

Changes: This summary was created with assistance from AI and may have inaccuracies. For accurate information, please refer to the original source documents linked here.

Thank you to arxiv for use of its open access interoperability.

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