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電液束加工對DD6單晶合金氣膜孔損傷行為研究
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北京航空材料研究院

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中圖分類號:

TG132.3

基金項目:

航空科學基金(KZ43150734)


Damage behavior of electro-stream machining on the film holes ofDD6 single crystal superalloy
Author:
Affiliation:

Beijing Institute of Aeronautical Materials

Fund Project:

Aeronotical Science Foundation of China

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    摘要:

    國內對于先進型號發(fā)動機渦輪轉子單晶葉片已主要采用電液束加工。電液束加工主要是電化學陽極溶解的過程,對單晶高溫合金會造成孔邊材料的腐蝕損傷,進而在服役條件下影響單晶葉片的性能。采用微觀觀察、金相分析等研究電液束加工對單晶高溫合金氣膜孔的損傷行為,通過高溫原位疲勞試驗分析打孔損傷對疲勞裂紋萌生機制的影響。結果表明:在入口側孔邊及孔壁的腐蝕區(qū)域形貌均為DD6單晶高溫合金電解腐蝕組織的特征,部分γ相被腐蝕掉,γ′相突出。入口側孔邊的電解腐蝕層厚度在15~30μm范圍內,中間孔壁的電解腐蝕層厚度在6~9μm范圍內;帶單孔的DD6單晶高溫合金試樣疲勞裂紋萌生有兩種情況:一是從孔邊的疏松缺陷處萌生裂紋;二是從孔邊的電解腐蝕損傷層附近起源。

    Abstract:

    Electro-stream machining is mainly a process of electrochemical anode dissolution, which causes corrosion damage to the single-crystal material and affects the performance of the film holes under service conditions. Based on the microscopic analysis and in-situ fatigue test, the damage behavior of electro-stream machining on the film holes of DD6 single crystal superalloy were investigated. The results show that the corrosion zones of the film hole are all characteristics of electrolytic corrosion of DD6 single crystal superalloy, which a part of the γ phase is eroded and the γ′ phase is prominent. In addition, there are two ways of fatigue crack initiation of the DD6 single crystal superalloy specimen with a single hole: one is originate from the porous defect at the edge of the hole and the other is that from the electrolytic corrosion damage layer at the edge of the hole.

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胡春燕,劉新靈,陶春虎.電液束加工對DD6單晶合金氣膜孔損傷行為研究[J].稀有金屬材料與工程,2019,48(10):3190~3194.[huchunyan, liuxinling, taochunhu. Damage behavior of electro-stream machining on the film holes ofDD6 single crystal superalloy[J]. Rare Metal Materials and Engineering,2019,48(10):3190~3194.]
DOI:10.12442/j. issn.1002-185X.20180416

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  • 收稿日期:2018-04-24
  • 最后修改日期:2018-06-22
  • 錄用日期:2018-06-27
  • 在線發(fā)布日期: 2019-11-01
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