Airworthiness verification of additive manufacturing technology for large integral metallic structure

In order to solve the problems existing in airworthiness verification of the large integral metallic structure for civil aircraft main bearing part, the airworthiness verification of the metallic structure additive manufacturing technology was carried out. Through the analysis of applicable airworth...

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Main Authors: JIANG Wu, LIU Mujun, HAO Xiaoning, LUO Linyin
Format: Article
Language:zho
Published: Journal of Aeronautical Materials 2019-02-01
Series:Journal of Aeronautical Materials
Subjects:
Online Access:http://jam.biam.ac.cn/CN/Y2019/V39/I2/90
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spelling doaj-46d99d67ee1a45f5a9b8aaea120d11bf2020-11-25T01:17:02ZzhoJournal of Aeronautical MaterialsJournal of Aeronautical Materials1005-50531005-50532019-02-01392909810.11868/j.issn.1005-5053.2018.000078201902000078Airworthiness verification of additive manufacturing technology for large integral metallic structureJIANG Wu0LIU Mujun1HAO Xiaoning2LUO Linyin3China Aviation Industry General Aircraft Co., Ltd, Zhuhai 519040, Guangdong, ChinaChina Aviation Industry General Aircraft Co., Ltd, Zhuhai 519040, Guangdong, ChinaChina Aviation Industry General Aircraft Co., Ltd, Zhuhai 519040, Guangdong, ChinaChina Aviation Industry General Aircraft Co., Ltd, Zhuhai 519040, Guangdong, ChinaIn order to solve the problems existing in airworthiness verification of the large integral metallic structure for civil aircraft main bearing part, the airworthiness verification of the metallic structure additive manufacturing technology was carried out. Through the analysis of applicable airworthiness clauses of additive manufacturing technology, the general idea of airworthiness verification of the metallic structure additive manufacturing technology of civil aircraft is given, including the establishment of material specification, the determination of material strength properties, the selection of structural special factor, and the verification of structural performance. Each verification method gives a specific implementation approach. Taking outer cylinder of the nose landing gear pillar which is made by additive manufacturing technology with A-100 ultrahigh strength steel as an example, a specific implementation plan for airworthiness verification of additive manufacturing technology for large integral metallic structure is given.http://jam.biam.ac.cn/CN/Y2019/V39/I2/90additive manufacturingairworthiness verificationmaterial specificationmaterial strength propertiesstructural special factorstructural verification
collection DOAJ
language zho
format Article
sources DOAJ
author JIANG Wu
LIU Mujun
HAO Xiaoning
LUO Linyin
spellingShingle JIANG Wu
LIU Mujun
HAO Xiaoning
LUO Linyin
Airworthiness verification of additive manufacturing technology for large integral metallic structure
Journal of Aeronautical Materials
additive manufacturing
airworthiness verification
material specification
material strength properties
structural special factor
structural verification
author_facet JIANG Wu
LIU Mujun
HAO Xiaoning
LUO Linyin
author_sort JIANG Wu
title Airworthiness verification of additive manufacturing technology for large integral metallic structure
title_short Airworthiness verification of additive manufacturing technology for large integral metallic structure
title_full Airworthiness verification of additive manufacturing technology for large integral metallic structure
title_fullStr Airworthiness verification of additive manufacturing technology for large integral metallic structure
title_full_unstemmed Airworthiness verification of additive manufacturing technology for large integral metallic structure
title_sort airworthiness verification of additive manufacturing technology for large integral metallic structure
publisher Journal of Aeronautical Materials
series Journal of Aeronautical Materials
issn 1005-5053
1005-5053
publishDate 2019-02-01
description In order to solve the problems existing in airworthiness verification of the large integral metallic structure for civil aircraft main bearing part, the airworthiness verification of the metallic structure additive manufacturing technology was carried out. Through the analysis of applicable airworthiness clauses of additive manufacturing technology, the general idea of airworthiness verification of the metallic structure additive manufacturing technology of civil aircraft is given, including the establishment of material specification, the determination of material strength properties, the selection of structural special factor, and the verification of structural performance. Each verification method gives a specific implementation approach. Taking outer cylinder of the nose landing gear pillar which is made by additive manufacturing technology with A-100 ultrahigh strength steel as an example, a specific implementation plan for airworthiness verification of additive manufacturing technology for large integral metallic structure is given.
topic additive manufacturing
airworthiness verification
material specification
material strength properties
structural special factor
structural verification
url http://jam.biam.ac.cn/CN/Y2019/V39/I2/90
work_keys_str_mv AT jiangwu airworthinessverificationofadditivemanufacturingtechnologyforlargeintegralmetallicstructure
AT liumujun airworthinessverificationofadditivemanufacturingtechnologyforlargeintegralmetallicstructure
AT haoxiaoning airworthinessverificationofadditivemanufacturingtechnologyforlargeintegralmetallicstructure
AT luolinyin airworthinessverificationofadditivemanufacturingtechnologyforlargeintegralmetallicstructure
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