
Journal of Materials Research and Technology, Journal Year: 2025, Volume and Issue: unknown
Published: April 1, 2025
Language: Английский
Journal of Materials Research and Technology, Journal Year: 2025, Volume and Issue: unknown
Published: April 1, 2025
Language: Английский
Next Sustainability, Journal Year: 2025, Volume and Issue: 6, P. 100105 - 100105
Published: Jan. 1, 2025
Language: Английский
Citations
5Journal of the Air Transport Research Society, Journal Year: 2025, Volume and Issue: unknown, P. 100056 - 100056
Published: Jan. 1, 2025
Language: Английский
Citations
1Journal of Environmental Management, Journal Year: 2025, Volume and Issue: 379, P. 124752 - 124752
Published: March 5, 2025
Language: Английский
Citations
1Thin-Walled Structures, Journal Year: 2024, Volume and Issue: unknown, P. 112899 - 112899
Published: Dec. 1, 2024
Language: Английский
Citations
7Materials Today Communications, Journal Year: 2025, Volume and Issue: unknown, P. 112289 - 112289
Published: March 1, 2025
Language: Английский
Citations
0Sustainability, Journal Year: 2025, Volume and Issue: 17(7), P. 3188 - 3188
Published: April 3, 2025
The aerospace industry is actively seeking sustainable solutions within the aviation sector to mitigate greenhouse gas (GHG) emissions driven by increasing population demands. This study presents first environmental life cycle assessment (LCA) of economy-class seating frames, comparing conventional alloy steel with lightweight alternative materials, including magnesium alloy, aluminum and titanium. Seat frames account for an aircraft’s total weight, making them a critical component innovation toward more solutions. Using SolidWorks V3.1, seat were designed evaluated through cradle-to-grave functional unit (FU) representing interior single aircraft. analysis was conducted using SimaPro V8.4.0 Ecoinvent V3.10 database. GHG associated composed steel, titanium, 208 kt CO2 equivalent (eq.), 120 eq, 71.1 44.9 eq per FU, respectively. identifies titanium be most frame materials relative other considered commercial aircrafts.
Language: Английский
Citations
0Polymers, Journal Year: 2025, Volume and Issue: 17(9), P. 1195 - 1195
Published: April 27, 2025
To address the insufficient bonding performance between TC4 (Ti-6Al-4V) coating and carbon fiber-reinforced thermoplastic (CFRP) matrices that limits engineering applications of composite structures, coatings were fabricated on CFRP polymer composites via laser cladding analyzed using scanning electron microscopy (SEM) transmission (TEM) to examine interface morphology, microstructure, phase composition. The influence processing parameters quality was assessed based mechanical coating. findings revealed power (<230 W) or excessive speed (>1.4 m/min) led incomplete melting powder, preventing formation intermetallic compound (IMC) layers. Conversely, (>270 a low (<1.0 caused thermal decomposition due its limited resistance, leading interfacial defects such as cracks pores. primarily comprised granular TiC acicular α′ martensite, with minor TiS2 detected. Optimal achieved at 250 W 1.2 m/min, yielding maximum shear strength 18.5 MPa. These provide critical insights for enhancing load-bearing capacity TC4/CFRP aeronautical composites, enabling their reliable operation in extreme aerospace environments.
Language: Английский
Citations
0Journal of Materials Research and Technology, Journal Year: 2025, Volume and Issue: unknown
Published: April 1, 2025
Language: Английский
Citations
0