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梯度结构热防护涂层增材制造成形与性能研究

蔡思凡 周童 刘滔 王波 方淦 吴文杰 曹良成

固体火箭技术2025,Vol.48Issue(2):281-290,10.
固体火箭技术2025,Vol.48Issue(2):281-290,10.DOI:10.7673/j.issn.1006-2793.2025.02.013

梯度结构热防护涂层增材制造成形与性能研究

Additive manufacturing and properties of gradient structured heat protection coatings

蔡思凡 1周童 1刘滔 1王波 1方淦 2吴文杰 2曹良成2

作者信息

  • 1. 中国科学院 重庆绿色智能技术研究院,重庆 400714||中国科学院大学,北京 100049
  • 2. 中国科学院 重庆绿色智能技术研究院,重庆 400714
  • 折叠

摘要

Abstract

The development of hypersonic vehicles necessitates the creation of novel heat protection structure and technology that can survive in extreme thermal conditions.Advances in its"discrete-accumulation"characteristics,additive manufacturing(AM)technique of"online metering-in situ mixing-variable-component extrusion-additive manufacturing"was proposed to deposit anti-ab-lation/thermal insulation components at specific spatial locations,offering a customization method of gradient structured heat protec-tion coatings.The rheological behavior and thermal protection performance of resin,anti-ablation,and thermal insulation components were studied,along with the high-throughput mixing capacity and gradient-structure preparation ability of the AM system.Continuous lines with gradient structure,radial gradient structures,and axial alternating/continuous gradient structures were successfully fabri-cated.A gradient heat shielding sample(100 mm×100 mm×5.5 mm)with porosities ranging from 0.8%to 47.8%was prepared.The results show that the peak temperature on the surface of the specimen is 616℃,the peak temperature on the back is 45℃,and the ablation depth is-0.81 mm.The surface of the specimen is flat and the coating does not fall off.Compared to homogeneous coat-ings,the gradient-structured coatings exhibit superior ablation resistance,with a 24.6%reduction in density.

关键词

热防护/梯度结构/增材制造/多材料/涂层

Key words

heat protection/additive manufacturing/gradient structure/multi-material/coating

引用本文复制引用

蔡思凡,周童,刘滔,王波,方淦,吴文杰,曹良成..梯度结构热防护涂层增材制造成形与性能研究[J].固体火箭技术,2025,48(2):281-290,10.

基金项目

中国科学院西部青年学者项目. ()

固体火箭技术

OA北大核心

1006-2793

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