Due to high melting point, high thermal shock resistance, low dielectric constant and low loss tangents, amorphous silica have received considerable attraction in the field of missile radomes, heat-resistant materials for aerospacecraft, crucibles and so on 1-4. However, the intrinsic brittleness and very low fracture strain restrict in many fields for its further applications. Compared with monolithic ceramics, continuous fiberreinforced ceramic matrix composites (CFCCs) have been improved the fracture resistance greatly 3,5-8. In order to improve the mechanical properties of silica, silica composites reinforced by shorter silica fibers and 2D silica preforms have been investigated. It was showed that the mechanical properties were enhanced. However, there are limits to improve the properties 5. 2.5D composites were studied in literatures 9-14. There are a number of 2.5D structures such as 2.5D shallow bend-joint, shallow straight-joint, deep straight-joint and so on. The characteristics of 2.5D weave technique make the fabric preform particularly suitable for conforming to the mould surface of revolving components and allow net or near-net shaping 9. The 2.5D composites possess higher through-the-thickness mechanical properties as compared to equivalent laminated composites. The 2.5D composites show better delamination resistance and higher interlaminar fracture toughness than traditional laminated composites when subjected to interlaminar