交替盐雾环境下Ti-15-3钛合金与MT700/603B连接件的接触腐蚀行为
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1.海装北京局驻北京地区第一军事代表室,北京 100076;2.航天材料及工艺研究所,北京 100076;3.大连理工大学材料科学与工程学院,大连 116024

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TG174.1

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Contact Corrosion of Ti-15-3 Titanium Alloy and MT700/603B Joints in Alternate Salt Spray Environment
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1.The First Military Representative Office of Beijing Bureau of the Ministry of Naval Equipment, Beijing 100076;2.Aerospace Research Institute of Materials & Processing Technology, Beijing 100076;3.School of Materials Science and Engineering, Dalian University of Technology, Dalian 116024

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    摘要:

    研究交替盐雾环境下Ti-15-3钛合金与MT700/603B碳纤维复合材料的接触腐蚀行为,分析碳纤维表面状态、缝隙宽度、腐蚀时间等对腐蚀敏感性和腐蚀特征影响。结果表明,缝隙宽度为0.06 mm时钛合金腐蚀最为严重。缝隙腐蚀和接触腐蚀相比,在相同腐蚀条件下后者的腐蚀失重速率、腐蚀氧化层面积均显著大于前者,表明钛合金接触腐蚀的腐蚀程度较缝隙腐蚀更为严重。Cr分布不均匀区域腐蚀更为严重。

    Abstract:

    The galvanic corrosion behavior of Ti-15-3 titanium alloys and MT700/603B carbon fiber reinforced resin composites in alternate salt spray environment was studied. The effects of carbon fiber surface state, gap width and corrosion time on corrosion sensitivity and corrosion characteristics were analyzed. The results show that titanium alloy suffers the most serious degradation when the gap width is 0.06 mm. Compared with crevice corrosion, the corrosion weight loss rate and corrosion oxide area of galvanic corrosion are significantly larger under the same corrosion conditions, which indicates that the corrosion degree of galvanic corrosion is more destructive than crevice corrosion. The corrosion damage is more drastic in Cr region with nonuniform distribution.

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曹阳,邹士文,林启皓,付雪松,梁洪涛.交替盐雾环境下Ti-15-3钛合金与MT700/603B连接件的接触腐蚀行为[J].宇航材料工艺,2021,51(4):147-153.

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历史
  • 收稿日期:2021-04-02
  • 最后修改日期:2021-07-27
  • 录用日期:2021-05-26
  • 在线发布日期: 2021-08-25
  • 出版日期: 2021-08-30
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