Titlebook: Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components; Xiaochong Liu,Longbiao Li Book 2024 The Editor(s) (if a

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Archipelago

Organization

the first flight testing, which verified the feasibility of the SiC/SiC turbine rotor for gas turbine engine application and accumulated valuable experience for the subsequent development of CMC hot-section components.

的事物

Design, Fabrication and Testing of CMC Combustor Liner,Ra = 0.3~0.5. After the inner and outer liners and other components have been densified and processed, the SiC rivets are used for on-line riveting, which achieves a connection result equivalent to “metal riveting” after CVI-SiC deposition, improves the ability of components to maintain the profile,

察觉

Design, Fabrication and Testing of CMC Turbine Blisk, the first flight testing, which verified the feasibility of the SiC/SiC turbine rotor for gas turbine engine application and accumulated valuable experience for the subsequent development of CMC hot-section components.

确保

确保

High-Temperature Mechanical Properties of Ceramic-Matrix Composites,forms, i.e., three-dimensional four-directional (3D4D) braided, two-dimensional plain-woven (2DPW) and stain woven (2DSW) lamination, are investigated at elevated temperature of 1400 °C. The high-temperature mechanical properties of SiC/SiC composites, e.g., tensile strength, compressional strength,

Gobble

Design, Fabrication and Testing of CMC High-Pressure Turbine Guide Vane,nalysis of the turbine guide vane was at first analyzed. The SiC/SiC high-pressure turbine single/twin guide vanes were fabricated using the chemical vapor infiltration (CVI) method. Thermal shock experiments of SiC/SiC high-pressure turbine guide vanes were carried out on the third-generation turbi

Cloudburst

Design, Fabrication and Testing of CMC Combustor Liner, was at first analyzed. The SiC/SiC combustor liner with the dimension of 296.48 mm (maximum diameter of outer liner) × 149.85 mm (minimum diameter of inner liner) × 100.46 mm (height), a wall thickness of 3–10 mm (including splicing structure) was fabricated using the CVI process. The surface of th

Ischemic-Stroke