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Phenolic epoxy resin (F51) was first reacted with silane coupling agent (3-aminopropyl)triethoxysilane (KH550) to form a silanized phenolic epoxy resin (SPER); then the SPER was copolymerized with methylphenyl silicone resin (MPS) to synthesize phenolic epoxy modified silicone copolymer (PEMSC). The chemical structure of the PEMSC was characterized by FT-IR. The results of tensile strength and shear strength measurements indicated that the successful introduction of F51 significantly improved the mechanical and adhesive properties of the PEMSC; compared with the PEMSC with 10 phr of F51 added, the tensile strength and shear strength of the PEMSC with 40 phr increased by 8.5 and 3.5 times respectively. The TGA and DTGA analysis showed that the initial thermal decomposition temperature and the residual weight of PEMSC at 800 °C decreased compared to MPS, but the temperature corresponding to the maximum thermal decomposition rate in the second stage increased. Qualitative analysis was conducted on the decomposition products of PEMSC using gas chromatography coupled with mass spectrometry (GC-MS). The results showed that the relative content of aromatic hydrocarbons and their derivatives in the decomposition products of PEMSC was 64.11%, and the relative content of cyclic trimers and higher cyclomers was 20.41%. [ABSTRACT FROM AUTHOR]

Summary: Treatment options for idiopathic multicentric Castleman disease (iMCD) are currently limited, especially for patients who do not respond or are resistant to interleukin‐6 inhibitors. For the first time, we innovatively designed a protocol using rituximab–bortezomib–dexamethasone (RVD) as first‐line consolidation therapy in patients newly diagnosed with iMCD. Furthermore, we adopted a no‐maintenance treatment strategy to simplify post‐remission care. Five patients with iMCD were enrolled (including one with TAFRO syndrome) and underwent the RVD regimen, all of whom achieved partial response (PR) or better. After four cycles of RVD, three (60%) patients achieved PR, while one (20%) achieved a complete response. These five patients, who achieved PR or better, discontinued treatment but remained stable for a median follow‐up of 11 months, with a duration of response of 7, 7, 10, 12 and 13 months, respectively. None of the patients experienced grade ≥3 adverse events during the observation period. Collectively, these findings demonstrated that the RVD regimen may be a promising treatment option for patients with iMCD. It was a safe and effective approach that resulted in lasting responses without the need for ongoing maintenance therapy. [ABSTRACT FROM AUTHOR]

Hypersonic vehicles encounter hostile service environments of thermal/mechanical/chemical coupling, so thermal protection materials are crucial and essential. Ceramizable composites have recently attracted intensive interest due to their ability to provide large-area thermal protection for hypersonic vehicles. In this work, a novel ceramizable composite of quartz fiber/benzoxazine resin modified with fused SiO2 and h-BN was fabricated using a prepreg compression molding technique. The effects of the fused SiO2 and h-BN contents on the thermal, mechanical, and ablative properties of the ceramizable composite were systematically investigated. The ceramizable composite with an optimized amount of fused SiO2 and h-BN exhibited superb thermal stability, with a peak degradation temperature and residue yield at 1400 °C of 533.2 °C and 71.5%, respectively. Moreover, the modified ceramizable composite exhibited excellent load-bearing capacity with a flexural strength of 402.2 MPa and superior ablation resistance with a linear ablation rate of 0.0147 mm/s at a heat flux of 4.2 MW/m2, which was significantly better than the pristine quartz fiber/benzoxazine resin composite. In addition, possible ablation mechanisms were revealed based on the microstructure analysis, phase transformation, chemical bonding states, and the degree of graphitization of the ceramized products. The readily oxidized pyrolytic carbon (PyC) and the SiO2 with a relatively low melting point were converted in situ into refractory carbide. Thus, a robust thermal protective barrier with SiC as the skeleton and borosilicate glass as the matrix protected the composite from severe thermochemical erosion and thermomechanical denudation. [ABSTRACT FROM AUTHOR]