激光选区熔化航空发动机制件适航符合性验证方法研究

郭婧; 何歆; 周晨阳; 付秋菊; 刘伟; 王天元; 吴宇

doi:10.13224/j.cnki.jasp.20230765

激光选区熔化航空发动机制件适航符合性验证方法研究

doi: 10.13224/j.cnki.jasp.20230765

1.
中国航发湖南动力机械研究所基础技术研究部，湖南株洲 412002
2.
中国民用航空局适航审定中心结构审定室，北京 100102
3.
中国航发北京航空材料研究院 3D打印研究与工程技术中心，北京 100095

详细信息

作者简介:
郭婧（1987-），女，高级工程师，硕士，主要从事材料及工艺应用研究。E-mail：guojing20040510@126.com

中图分类号: V37
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- 文章访问数: 44
- HTML浏览量: 19
- PDF量: 15
- 被引次数: 0
出版历程
- 收稿日期: 2023-12-04
- 网络出版日期: 2024-04-17

Study on airworthiness compliance demonstration method of aeroengine components fabricated through selective laser melting technique

1.
Fundamental Technology Research Department，Hunan Aviation Powerplant Research Institute，Aero Engine Corporation of China，Zhuzhou Hunan 412002，China
2.
Structural Certification Division，Airworthiness Certification Center，Civil Aviation Administration of China，Beijing 100102，China
3.
3D Printing Research and Engineering Technology Center，Beijing Institute of Aeronautical Materials，Aero Engine Corporation of China，Beijing 100095，China

摘要

摘要:
针对民用航空发动机激光选区熔化制件适航符合性验证需求，总结了激光选区熔化技术在航空发动机中的应用现状，分析了激光选区熔化制件适航符合性验证相关参考资料要求，研究了激光选区熔化航空发动机制件适航符合性验证方法。目前，国外已有激光选区熔化航空发动机制件通过了适航审定，而我国在该领域仍处于起步阶段。基于相关参考资料及传统工艺适航符合性验证方法，认为激光选区熔化航空发动机制件的适航符合性验证方法主要应包括：建立激光选区熔化材料规范、认证激光选区熔化工艺、鉴定激光选区熔化成形材料是否合格及确定设计用材料性能。
- 激光选区熔化 /
- 航空发动机 /
- 制件 /
- 适航 /
- 符合性验证方法
Abstract:
Motivated by the demand of airworthiness compliance of civil aeroengine components fabricated using selective laser melting (SLM) technique, the applications of SLMed aeroengine components were summarized. Additionally, reference related to airworthiness compliance of SLMed components were analyzed. Meanwhile, airworthiness compliance demonstration method of SLMed aeroengine components was investigated. Presently, some SLMed aeroengine components have passed the airworthiness certification in foreign countries. However, China is still in the initial stage in this field. According to the related reference and airworthiness compliance demonstration method of aeroengine components manufactured through traditional processing techniques, the airworthiness compliance demonstration method of SLMed aeroengine components should mainly contain the following parts: establishment of selective laser melted material specifications, certification of selective laser melting process, identification of material quality and determination of material properties.
- selective laser melting /
- aeroengine /
- component /
- airworthiness /
- compliance demonstration method

HTML

图 1 GE公司增材制造零件发展过程

Figure 1. Development progress of additively manufactured components of GE company

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图 2 激光选区熔化航空发动机零件照片

Figure 2. Photograph of SLMed aeroengine components

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图 3 ASTM F2971-13规定的力学性能测试取样方向

Figure 3. Directions of mechanical properties testing samples according to ASTM F2971-13

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图 4 基板分区示意图

Figure 4. Schematic illustration of platform part

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