MUMBAI, India, July 24 -- Intellectual Property India has published a patent application (202631078558 A) filed by National Institute Of Technology Rourkela on June 25, 2026, for “development Of W-Reeasistr Ant Light-Weight Al-Based Hybrid Nanocomposites For Aerospace Landing Gear Applications”.
Inventors include Syed Nasimul Alam; Arka Ghosh; Nityananda Sahoo; Pankaj Shrivastava; Ashutosh Das; Parth Patel; and Velaphi Msomi.
The application for the patent was published on July 17, 2026, under issue no. 29/2026.
Abstract: DEVELOPMENT OF WEAR-RESISTANT LIGHT-WEIGHT AL-BASED HYBRID NANOCOMPOSITES FOR AEROSPACE LANDING GEAR APPLICATIONS Abstract A lightweight, high-strength, and wear-resistant aluminium-based hybrid nanocomposite material and an optimized low-temperature spark plasma sintering method for its fabrication are disclosed for high- wear aerospace structural applications. The hybrid nanocomposite comprises a high-purity aluminium metal matrix reinforced with a ternary hybrid nanofiller system consisting of multi-walled carbon nanotubes (MWCNTs), graphite nanoplatelets (GnPs), and hexagonal boron nitride (hBN). The multi-walled carbon nanotubes act as mechanical bridging strands that link planar surfaces of the graphite nanoplatelets and hexagonal boron nitride sheets, establishing an interconnected three-dimensional reinforcing nano- architecture that prevents filler agglomeration and reduces internal porosity down to approximately 3.7%. Consolidating the composite via spark plasma sintering at a low temperature of 400°C and 50 MPa pressure for 10 minutes prevents the formation of brittle intermetallic aluminium carbide (Al_4C_3) phases. Under dry sliding friction, the composite forms a protective, self-lubricating tribo- layer that cuts the volumetric wear rate by approximately 70%, stabilizes the coefficient of friction between 0.55 and 0.60, limits wear depth penetration to under 120 mu m, and changes the primary wear mechanism from severe delamination to mild ploughing. (FIG. 1)
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