MGH956合金板材基本成形性能研究

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MGH956合金板材基本成形性能研究

更新时间：2025-10-30

- MGH956合金板材基本成形性能研究
- Aeronautical Manufacturing Technology Vol. 58, Issue 16, Pages: 85-89(2015)
- 作者机构：
  
  中航工业沈阳黎明航空发动机（集团）有限责任公司
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2015.16.085
  CLC：
- Published：2015
- 稿件说明：
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杨踊，曹一超，周勇. MGH956合金板材基本成形性能研究[J]. 航空制造技术, 2015, 58(16): 85-89.

[J]. Aeronautical Manufacturing Technology, 2015, 58(16): 85-89.
杨踊，曹一超，周勇. MGH956合金板材基本成形性能研究[J]. 航空制造技术, 2015, 58(16): 85-89. DOI： 10.16080/j.issn1671-833x.2015.16.085.

[J]. Aeronautical Manufacturing Technology, 2015, 58(16): 85-89. DOI： 10.16080/j.issn1671-833x.2015.16.085.

MGH956合金为国内仿MA956合金研制的一种氧化物弥散强化高温合金，对MGH956合金板材进行了埃里克森杯突、拉深、扩孔、弯曲、锥杯和成形极限图等试验。通过试验，对于MGH956合金板材，建议采用具有拉深、胀形或拉胀复合成形特征零件的热成形，减少或避免用于具有较多翻边特征的零件加工。

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