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Given the critical threats to aviation safety induced by electromagnetic interference (EMI), fire hazards, and icing, high‐performance multifunctional materials integrating mechanical flexibility, EMI shielding, fire resistance, and thermal management capabilities are highly desired yet challenging. Herein, a synergistic strategy is developed involving defect engineering and graphitization to enhance EMI shielding and thermal management properties of SiBCNZr nanofiber fabrics. Initially, the SiBCNZr nanofiber fabrics demonstrate excellent mechanical flexibility and intrinsic ceramic fire resistance. Furthermore, after annealing at 1400 °C, t‐ZrO2 nanograins with various types of defects are precipitated from the amorphous matrix, accompanied by the formation of turbostratic graphite C. The synergistic effects of defect engineering of t‐ZrO2 nanograins and graphitization of turbostratic C enhance conductivity and polarization loss, leading to a specific shielding effectiveness (SSE/t) of 2718 dB cm2 g−1. Additionally, the fabrics also demonstrate remarkable electrothermal conversion capability with a rapid electrothermal response. This work provides valuable insights into designing multifunctional EMI shielding ceramic nanofiber fabrics for aviation safety.
Given the critical threats to aviation safety induced by electromagnetic interference (EMI), fire hazards, and icing, high‐performance multifunctional materials integrating mechanical flexibility, EMI shielding, fire resistance, and thermal management capabilities are highly desired yet challenging. Herein, a synergistic strategy is developed involving defect engineering and graphitization to enhance EMI shielding and thermal management properties of SiBCNZr nanofiber fabrics. Initially, the SiBCNZr nanofiber fabrics demonstrate excellent mechanical flexibility and intrinsic ceramic fire resistance. Furthermore, after annealing at 1400 °C, t‐ZrO2 nanograins with various types of defects are precipitated from the amorphous matrix, accompanied by the formation of turbostratic graphite C. The synergistic effects of defect engineering of t‐ZrO2 nanograins and graphitization of turbostratic C enhance conductivity and polarization loss, leading to a specific shielding effectiveness (SSE/t) of 2718 dB cm2 g−1. Additionally, the fabrics also demonstrate remarkable electrothermal conversion capability with a rapid electrothermal response. This work provides valuable insights into designing multifunctional EMI shielding ceramic nanofiber fabrics for aviation safety.
Lignocellulose‐mediated liquid metal (LM) composites, as emerging functional materials, show tremendous potential for a variety of applications. The abundant hydroxyl, carboxyl, and other polar groups in lignocellulose facilitate the formation of strong chemical bonds with LM surfaces, enhancing wettability and adhesion for improved interface compatibility. Beyond serving as a supportive matrix, lignocellulose can be tailored to optimize the microstructure of the composites, adapting them for diverse applications. This review comprehensively summarizes the fundamental principles and recent advancements in lignocellulose‐mediated LM composites, highlighting the advantages of lignocellulose in composite fabrication, including facile synthesis, versatile interactions, and inherent functionalities. Key modulation strategies for LMs and innovative synthesis methods for functionalized lignocellulose composites are discussed. Furthermore, the roles and structure–performance relationships of these composites in electromagnetic shielding, flexible sensors, and energy storage devices are systematically summarized. Finally, the obstacles and prospective advancements pertaining to lignocellulose‐mediated LM composites are thoroughly scrutinized and deliberated upon. This review is expected to provide basic guidance for researchers to boost the popularity of LMs in diverse applications and provide useful references for design strategies of state‐of‐the‐art LMs.
Constructing effective conductive networks within polymer composites has proven to be a successful strategy for fabricating electromagnetic interference (EMI) shielding materials. Herein, we present a novel approach for creating high‐temperature EMI shielding materials by integrating 3D printing with compression molding. First, a thermoplastic polyurethane (TPU) framework was printed using fused deposition modeling (FDM), enabling customization of the composite's conductivity. This framework was subsequently treated with solution immersion to load carbon nanotubes (CNTs) onto the TPU surface, followed by compression molding to form TPU/CNTs composites with a segregated conductive network. The effects of coating cycles and hot‐pressing temperature on the conductive network and EMI shielding performance were systematically studied. The results revealed that hot pressing temperature significantly influences the development of the conductive network. At 130°C, a weak conductive network was formed due to spatial confinement within the TPU frame, yielding an EMI shielding effectiveness (SET) of 44 dB. However, at 190°C, a more extensive conductive network was developed as the CNTs‐rich phase overcomes spatial constrains, achieving an impressive SET of 52 dB. This high‐performance material, coupled with its simple and versatile fabrication process, holds promise for the development of advanced EMI shielding materials.Highlights Integrating 3D printing and compression molding, segregated conductive networks was established in TPU/CNTs composites, achieving up to 52 dB X‐band EMI SE. Hot‐pressing temperature plays a critical role in constructing effective networks. A weak conductive network formed at 130°C due to spatial confinement, resulting in a lower SET value. At 190°C, CNTs‐rich phase formed a robust conductive network, yielding a SET of 52 dB. TPU/CNTs composites demonstrates excellent electrical properties with a low R of 0.22, enabling next‐gen EMI shielding for high‐performance applications.
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