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ZL205A上臂铸件低压充型工艺设计

樊振中 阮磊 杨天杰 孙刚 王胜强

铸造2017,Vol.66Issue(8):882-887,6.
铸造2017,Vol.66Issue(8):882-887,6.

ZL205A上臂铸件低压充型工艺设计

Design of Low Pressure Filling Process for ZL205A Upper Arm Casting

樊振中 1阮磊 2杨天杰 3孙刚 4王胜强1

作者信息

  • 1. 中国航发北京航空材料研究院,北京 100095
  • 2. 北京市先进铝合金材料及应用工程技术研究中心,北京 100095
  • 3. 中国运载火箭技术研究院,北京100076
  • 4. 中航飞机股份有限公司汉中飞机分公司,陕西汉中723213
  • 折叠

摘要

Abstract

The ZL205A alloy is a high strength and tough aluminum-copper material, which can be used as medium load bearing parts for aerospace and other military equipment field after the T6 heat treatment. In this paper, four different low-pressure solidification forming processes of ZL205A upper arm casting are designed, the runner cross-section area ratio is selected to 1:1.8:4.4, combining with the 20 mm/s and 40 mm/s of liquid rise and filling speed, together with 25 kPa and 30 kPa of liquid rise and filling pressure, an order filling sequence from bottom to top and solidification process from top to bottom are achieved. The average tensile strength, yield strength and elongation of T6 bulk specimen are 484 MPa, 354.5 MPa and 6.9%respectively, lots of Al2Cu and Al6Mn precipitate strengthening phases distribute nearby the grain boundaries diffusely after the aging process. The dimple rupture appears as the main fracture mechanism, accompanying with some intergranular fracture zone.

关键词

ZL205A合金/凝固工艺/低压充型/力学性能/微观组织

Key words

ZL205A alloy/solidificationprocess/lowpressurefilling/mechanicalproperties/microstructure

分类

矿业与冶金

引用本文复制引用

樊振中,阮磊,杨天杰,孙刚,王胜强..ZL205A上臂铸件低压充型工艺设计[J].铸造,2017,66(8):882-887,6.

基金项目

中国航发北京航空材料研究院新产品研发基金(KJSC160206). (KJSC160206)

铸造

OA北大核心CSCDCSTPCD

1001-4977

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