Tribological Characterization of Carbon Fibre Reinforced Polymer (CFRP) Sliding Against Ti and Al Alloy Counterbodies for Aerospace Applications

Carbon fibre reinforced polymer (CFRP) is a composite material known for its light weight and exceptional durability, composed of carbon fibres within a polymer matrix. Despite its high cost, CFRP is favoured for its outstanding strength-to-weight ratio and rigidity. It is widely used in the aerospace industry and ship superstructures, among others. These components often rub against different materials in various structural and mechanical assemblies. These interactions typically occur where metallic fasteners, bearings, hinges, and sliding components interface with CFRP parts causing, for example, fretting wear. The main novelty of the present study consists of a systematic comparison of titanium (Ti6Al4V) and aluminium (AA2024-T6) alloy spheres under identical test conditions, evaluating how each material interacts with different CFRP configurations. CFRP was tested against titanium and aluminium alloy spheres as counterbodies under reciprocating sliding conditions. Different contact conditions (applied loads) were used for tribotests. The wear volume and coefficient of friction were determined, as well as the wear mechanisms. Different analytical techniques were employed, such as profilometry, optical microscopy (OM), and scanning electron microscopy (SEM/EDS), to characterise the wear tracks. It was possible to determine the coefficient of friction as well as the wear rate on both CFRP specimens and their respective counterbodies. It was found that the coefficient of friction (CoF) depends on load, fibre orientation, and counterbody material, ranging from 0.14 to 0.29. The lowest wear rate coefficient was observed for CFRP sliding against titanium alloy in the layer configuration, at 1.48 × 10<sup>-13</sup> mm<sup>3</sup>/N·m. In contrast, aluminium alloy counterbodies experienced significantly higher wear, with a maximum wear rate of 6.88 × 10<sup>-5</sup> mm<sup>3</sup>/N·m. Wear volume increased with load across all conditions and was highest for the CFRP cross-section against aluminium alloy.

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Journal
Materials
Published
2025-09-13
DOI
https://doi.org/10.3390/ma18184296
Citations
2
Primary Topic
Tribology and Wear Analysis
Type
article
Field-Weighted Citation Impact
1.73
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article

Tribological Characterization of Carbon Fibre Reinforced Polymer (CFRP) Sliding Against Ti and Al Alloy Counterbodies for Aerospace Applications

A. Ramalho, Sharjeel Ahmed Khan, Luís Vilhena, A N C Garcia
2 citations
Materials
Tribology and Wear Analysis
1.73
article

Tribological Characterization of Carbon Fibre Reinforced Polymer (CFRP) Sliding Against Ti and Al Alloy Counterbodies for Aerospace Applications

A. Ramalho, Sharjeel Ahmed Khan, Luís Vilhena, A N C Garcia
article en
2 citations

Abstract

Carbon fibre reinforced polymer (CFRP) is a composite material known for its light weight and exceptional durability, composed of carbon fibres within a polymer matrix. Despite its high cost, CFRP is favoured for its outstanding strength-to-weight ratio and rigidity. It is widely used in the aerospace industry and ship superstructures, among others. These components often rub against different materials in various structural and mechanical assemblies. These interactions typically occur where metallic fasteners, bearings, hinges, and sliding components interface with CFRP parts causing, for example, fretting wear. The main novelty of the present study consists of a systematic comparison of titanium (Ti6Al4V) and aluminium (AA2024-T6) alloy spheres under identical test conditions, evaluating how each material interacts with different CFRP configurations. CFRP was tested against titanium and aluminium alloy spheres as counterbodies under reciprocating sliding conditions. Different contact conditions (applied loads) were used for tribotests. The wear volume and coefficient of friction were determined, as well as the wear mechanisms. Different analytical techniques were employed, such as profilometry, optical microscopy (OM), and scanning electron microscopy (SEM/EDS), to characterise the wear tracks. It was possible to determine the coefficient of friction as well as the wear rate on both CFRP specimens and their respective counterbodies. It was found that the coefficient of friction (CoF) depends on load, fibre orientation, and counterbody material, ranging from 0.14 to 0.29. The lowest wear rate coefficient was observed for CFRP sliding against titanium alloy in the layer configuration, at 1.48 × 10<sup>-13</sup> mm<sup>3</sup>/N·m. In contrast, aluminium alloy counterbodies experienced significantly higher wear, with a maximum wear rate of 6.88 × 10<sup>-5</sup> mm<sup>3</sup>/N·m. Wear volume increased with load across all conditions and was highest for the CFRP cross-section against aluminium alloy.

MaterialsVol. 18(18)
University of Coimbra (PT)
Openalex Percentile: Top 15%
Tribology and Wear Analysis
1.73
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