In situ temperature‐controlled rotational molding for self‐building ribs in <scp>PA6</scp> liner for type <scp>IV</scp> hydrogen storage tanks

Abstract Type IV hydrogen storage tank liners must exhibit optimal appearance, stiffness, and lightweight construction to maximize hydrogen storage density while also serving as a platform for carbon fiber winding. However, the inherent weakness in stiffness, particularly in larger structures, necessitates the incorporation of localized reinforcements. Internal rib reinforcement is a key strategy for addressing this challenge. This study analyzes the effect of circumferential ribs on the performance of PA6‐based liners, demonstrating a significant increase in the critical buckling load by up to 15.2%. Furthermore, the study introduces a novel in situ, temperature‐controlled rotational molding (ITRM) platform that enables the one‐step creation of local inner reinforcements. By precisely controlling both the temperature and heating rates, we successfully manufactured a PA6 liner with stainless‐steel inserts and three reinforcing ribs, achieving a volume exceeding 600 L. The ITRM platform represents a significant advancement in addressing the weak stiffness of large‐capacity liners and offers promising potential for further innovation in liner development. Highlights Development of in situ temperature‐controlled rotational molding equipment Analysis of the impact of the position and number of ribs on the structural stiffness Proposed inner circumferential ribs design method in liners to enhance stiffness Manufactured large‐diameter and thin‐walled PA6 liner with stainless‐steel insert

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Publication Details

Journal
Polymer Engineering and Science
Published
2025-03-23
DOI
https://doi.org/10.1002/pen.27194
Citations
2
Primary Topic
Spacecraft and Cryogenic Technologies
Type
article
Field-Weighted Citation Impact
9.99

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article

In situ temperature‐controlled rotational molding for self‐building ribs in PA6 liner for type IV hydrogen storage tanks

Xiulei Wang, Pengcheng Xie, Yitao Ma, Gonghan Liu et al.
2 citations
Polymer Engineering and Science
Spacecraft and Cryogenic Technologies
9.99
article

In situ temperature‐controlled rotational molding for self‐building ribs in PA6 liner for type IV hydrogen storage tanks

Xiulei Wang, Pengcheng Xie, Yitao Ma, Gonghan Liu, Jianzhen Li, Weimin Yang, Xuedong Chen, Qianyi Wang, Zhichao Fan, Wenhong Cao
article en
2 citations

Abstract

Abstract Type IV hydrogen storage tank liners must exhibit optimal appearance, stiffness, and lightweight construction to maximize hydrogen storage density while also serving as a platform for carbon fiber winding. However, the inherent weakness in stiffness, particularly in larger structures, necessitates the incorporation of localized reinforcements. Internal rib reinforcement is a key strategy for addressing this challenge. This study analyzes the effect of circumferential ribs on the performance of PA6‐based liners, demonstrating a significant increase in the critical buckling load by up to 15.2%. Furthermore, the study introduces a novel in situ, temperature‐controlled rotational molding (ITRM) platform that enables the one‐step creation of local inner reinforcements. By precisely controlling both the temperature and heating rates, we successfully manufactured a PA6 liner with stainless‐steel inserts and three reinforcing ribs, achieving a volume exceeding 600 L. The ITRM platform represents a significant advancement in addressing the weak stiffness of large‐capacity liners and offers promising potential for further innovation in liner development. Highlights Development of in situ temperature‐controlled rotational molding equipment Analysis of the impact of the position and number of ribs on the structural stiffness Proposed inner circumferential ribs design method in liners to enhance stiffness Manufactured large‐diameter and thin‐walled PA6 liner with stainless‐steel insert

Polymer Engineering and ScienceVol. 65(6)
Hefei General Machinery Research Institute (China) (CN), Zhejiang Medicine (China) (CN), Beijing University of Chemical Technology (CN)
National Key Research and Development Program of China
Openalex Percentile: Top 3%
Spacecraft and Cryogenic Technologies
9.99
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