International Journal For Multidisciplinary Research

E-ISSN: 2582-2160   •   Impact Factor: 9.24

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Development of Graphene Reinforced Composite Materials for Turbine Blades - A Review

Author(s) K N Sanjeev Kumar, Sanjeev Sharma, Abdel-Hamid I. Mourad, PB Sharma
Country India
Abstract The study highlights recent advancements in high-performance materials for turbine blades used in gas turbines and jet engines. Key research areas focus on developing materials that can withstand high temperatures (1400°C–1600°C) while resisting oxidation and corrosion, essential for enhancing efficiency and reducing emissions. Inefficiencies arise from the use of coatings and complex cooling systems, increasing the demand for materials with higher temperature tolerance. Weight reduction is another critical area of improvement, particularly in aviation applications. This paper reviews advancements in Intermetallic alloys, Metal Matrix Composites (MMCs), and Ceramic Matrix Composites (CMCs), with a specific focus on graphene composites due to their outstanding mechanical strength at elevated temperatures, lightweight composition, and high oxidative resistance. Additionally, the study explores recent developments in graphene-reinforced composites and Mo-Si-B-based alloys as potential alternatives to Ni-based super alloys, offering promising results for sustaining higher operating temperatures and enhanced performance under high-stress conditions.
Keywords Turbine blades, Ceramic Matrix Composites, Titanium Carbide, Graphene Composites, Nickel-based Super alloys
Field Engineering
Published In Volume 6, Issue 6, November-December 2024
Published On 2024-11-18
Cite This Development of Graphene Reinforced Composite Materials for Turbine Blades - A Review - K N Sanjeev Kumar, Sanjeev Sharma, Abdel-Hamid I. Mourad, PB Sharma - IJFMR Volume 6, Issue 6, November-December 2024. DOI 10.36948/ijfmr.2024.v06i06.30850
DOI https://doi.org/10.36948/ijfmr.2024.v06i06.30850
Short DOI https://doi.org/g8rdzc
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