Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades

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...

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Main Authors: Dandan Qu, Xin Lin, Kun Zhang, Zhiyong Li, Zezhong Wang, Guoliang Liu, Yang Meng, Gengxing Luo, Ruoyan Wang, Xilong Yu
Format: Article
Language:English
Published: Taylor & Francis Group 2023-12-01
Series:Virtual and Physical Prototyping
Subjects:
Online Access:http://dx.doi.org/10.1080/17452759.2023.2235680
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author Dandan Qu
Xin Lin
Kun Zhang
Zhiyong Li
Zezhong Wang
Guoliang Liu
Yang Meng
Gengxing Luo
Ruoyan Wang
Xilong Yu
author_facet Dandan Qu
Xin Lin
Kun Zhang
Zhiyong Li
Zezhong Wang
Guoliang Liu
Yang Meng
Gengxing Luo
Ruoyan Wang
Xilong Yu
author_sort Dandan Qu
collection DOAJ
description 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.
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spelling doaj.art-8bf6c53a402544aa9faf096f547c9f992023-09-21T14:38:04ZengTaylor & Francis GroupVirtual and Physical Prototyping1745-27591745-27672023-12-0118110.1080/17452759.2023.22356802235680Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable bladesDandan Qu0Xin Lin1Kun Zhang2Zhiyong Li3Zezhong Wang4Guoliang Liu5Yang Meng6Gengxing Luo7Ruoyan Wang8Xilong Yu9Institute of Mechanics, Chinese Academy of SciencesInstitute of Mechanics, Chinese Academy of SciencesInstitute of Mechanics, Chinese Academy of SciencesInstitute of Mechanics, Chinese Academy of SciencesInstitute of Mechanics, Chinese Academy of SciencesInstitute of Mechanics, Chinese Academy of SciencesInstitute of Mechanics, Chinese Academy of SciencesInstitute of Mechanics, Chinese Academy of SciencesInstitute of Mechanics, Chinese Academy of SciencesInstitute of Mechanics, Chinese Academy of SciencesHybrid 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.http://dx.doi.org/10.1080/17452759.2023.2235680hybrid rocket engineadditive manufacturing/three-dimensional printingbreathable bladecomposite fuel grainmechanical and combustion propertiesporous structure
spellingShingle Dandan Qu
Xin Lin
Kun Zhang
Zhiyong Li
Zezhong Wang
Guoliang Liu
Yang Meng
Gengxing Luo
Ruoyan Wang
Xilong Yu
Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
Virtual and Physical Prototyping
hybrid rocket engine
additive manufacturing/three-dimensional printing
breathable blade
composite fuel grain
mechanical and combustion properties
porous structure
title Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
title_full Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
title_fullStr Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
title_full_unstemmed Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
title_short Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
title_sort additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
topic hybrid rocket engine
additive manufacturing/three-dimensional printing
breathable blade
composite fuel grain
mechanical and combustion properties
porous structure
url http://dx.doi.org/10.1080/17452759.2023.2235680
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