Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
文献类型：期刊论文
| 作者 | Qu DD(屈丹丹) ; Lin X(林鑫); Zhang K(张坤); Li ZY(李志永); Wang ZZ(王泽众); Liu GL(刘国亮); Meng Y(孟洋); Luo GX(罗耕星); Wang RY(王若岩); Yu XL(余西龙)
|
| 刊名 | VIRTUAL AND PHYSICAL PROTOTYPING
 |
| 出版日期 | 2023-12-31 |
| 卷号 | 18期号:1页码:e2235680 |
| 关键词 | Hybrid rocket engine additive manufacturing three-dimensional printing breathable blade composite fuel grain mechanical and combustion properties porous structure > |
| ISSN号 | 1745-2759 |
| DOI | 10.1080/17452759.2023.2235680 |
| 英文摘要 | Hybrid rocket engines suffer from the restricted mechanical properties and low regression rates of current polymeric fuel grains. We propose a three-dimensional printed aluminium (Al) nested composite fuel grain with millimetre-scale lattice pores (referred to as Al-L). In this study, breathable Al blades with micrometer-scale interconnected pores (Al-B) and blades combining millimetre-scale and micrometer-scale pores (Al-B & L) are designed. The formation mechanisms, characteristics, and effects of the breathable blades are analysed in simulations, micro-computed tomography, and cyclic compression tests. The mechanical properties of the composite fuel grains are investigated numerically and in compression tests. Al-B has the highest Young's modulus at more than 15 times that of a paraffin-based fuel grain and Al-B & L has the highest yield stress at 4 times that of the paraffin-based fuel grain. Referring to combustion properties, the regression rates of the Al-B and Al-B & L grains are respectively 63.3% and 58.2% greater than the regression rate of the paraffin-based fuel grain. |
| 分类号 | 一类 |
| WOS研究方向 | Engineering ; Materials Science |
| 语种 | 英语 |
| WOS记录号 | WOS:001049681600001 |
| 资助机构 | National Natural Science Foundation of China [11802309, 92271117, 11802315] ; Youth Innovation Promotion Association of CAS [2022018] |
| 其他责任者 | Lin, X (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China. |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/92605]  |
| 专题 | 宽域飞行工程科学与应用中心 力学研究所_高温气体动力学国家重点实验室 |
| 作者单位 | 1.{Li, Zhiyong} Cranfield Univ, Welding & Addit Mfg Ctr, Cranfield, England 2.{Lin, Xin} Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China 3.{Zhang, Kun, Yu, Xilong} Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China 4.{Lin, Xin, Wang, Zezhong, Wang, Ruoyan, Yu, Xilong} Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China 5.{Qu, Dandan, Zhang, Kun, Li, Zhiyong, Liu, Guoliang, Meng, Yang, Luo, Gengxing} Chinese Acad Sci, Inst Mech, Wide Range Flight Engn Sci & Applicat Ctr, Beijing, Peoples R China |
| 推荐引用方式 GB/T 7714 | Qu DD,Lin X,Zhang K,et al. Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades[J]. VIRTUAL AND PHYSICAL PROTOTYPING,2023,18(1):e2235680. |
| APA | 屈丹丹.,林鑫.,张坤.,李志永.,王泽众.,...&余西龙.(2023).Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades.VIRTUAL AND PHYSICAL PROTOTYPING,18(1),e2235680. |
| MLA | 屈丹丹,et al."Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades".VIRTUAL AND PHYSICAL PROTOTYPING 18.1(2023):e2235680. |
入库方式： OAI收割
来源：力学研究所
浏览0
下载0
收藏0
其他版本
除非特别说明，本系统中所有内容都受版权保护，并保留所有权利。