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激光沉積修復GH738合金時效熱處理組織及性能研究
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1.沈陽航空航天大學航空制造工藝數(shù)字化國防重點實驗室;2.沈陽黎明航空發(fā)動機(集團)有限公司焊接研究所;3.沈陽航空航天大學航空制造工藝數(shù)字化國防重點學科實驗室

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國家自然科學基金項目(面上項目,重點項目,重大項目)


Study on Aging-treatment Microstructure and Properties of GH738 Alloy by Laser Deposition Repair
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Key Laboratory of Fundamental Science for National Defence of Aeronautical Digital Manufacturing Process, Shenyang Aerospace University

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    摘要:

    研究了雙極時效熱處理對激光沉積修復GH738合金顯微組織及力學性能的影響。結(jié)果顯示:沉積態(tài)顯微組織為典型的外延柱狀枝晶,枝晶間距為約10 μm。經(jīng)過時效處理后,修復區(qū)組織開始長大、合并。沉積態(tài)未發(fā)現(xiàn)γ'相,枝晶間存在立方狀的MC型碳化物,枝晶干存在顆粒狀M23C6型碳化物。經(jīng)雙級時效處理后,修復區(qū)析出γ'相:穩(wěn)定化溫度為820℃時,γ'相平均尺寸約為37nm,碳化物在晶界處呈斷續(xù)狀析出。隨著穩(wěn)定化溫度升高,γ'相及碳化物尺寸均有所增大,其中穩(wěn)定化溫度為840 ℃時,γ'相平均尺寸約為76 nm,碳化物呈項鏈狀析出;穩(wěn)定化溫度為860℃時,γ'相平均尺寸無明顯增大,部分γ'相發(fā)生明顯粗化,尺寸達到150 nm,晶界處碳化物開始呈包膜狀析出。力學性能測試結(jié)果顯示:時效處理后試樣抗拉強度明顯提高,隨著穩(wěn)定化溫度升高,抗拉強度先升高后降低,斷后伸長率不斷降低。

    Abstract:

    The effects of bipolar aging heat treatment on the microstructure and mechanical properties were studied on GH738 alloy repaired by laser deposition repair technology.The results show that :the microstructure of repair area present typical characteristics of the epitaxial growth of columnar crystals and the dendrite spacing is about 10μm.After the aging treatment, the repair area begins to grow and merge .The results of SEM analysis show that :There is no γ'appear at the as-deposited , and the cubic MC type carbide is formed at the interdendritic, and the M23C6 type carbide at the dendrite arm ; After the aging treatment, γ'phase precipitated at the repair area: γ'phase with an average size of 37nm was found in the repair area, and the carbide precipitates in the grain boundary with the character of discontinued when the temperature of the stabilization step is 820℃; With the increase of the stabilization temperature, the size of the γ' and carbide increases ;When the temperature is 840℃, the average size of the γ'is about 76nm, and the carbide is precipitated in the form of necklace ;Adding the temperature of the stabilization step to 860℃ , the average size of the γ'does not increase obviously, and part of the γ' of is obviously coarsening and the size reach 150nm, meanwhile the carbides at the grain boundaries begin to form the closed. The results of mechanical property show that :the tensile strength of the sample increases obviously after aging treatment,and with the increase of the temperature, the tensile strength increases first and then decreases, and the elongation decreases continuously.

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卞宏友,翟泉星,曲伸,楊光,王偉,王維.激光沉積修復GH738合金時效熱處理組織及性能研究[J].稀有金屬材料與工程,2019,48(1):317~322.[bianhonhyou, zhaiquanxing, Qu Shen, yangguang, wangwei, wangwei. Study on Aging-treatment Microstructure and Properties of GH738 Alloy by Laser Deposition Repair[J]. Rare Metal Materials and Engineering,2019,48(1):317~322.]
DOI:10.12442/j. issn.1002-185X.20170424

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  • 收稿日期:2017-05-23
  • 最后修改日期:2017-07-23
  • 錄用日期:2017-08-18
  • 在線發(fā)布日期: 2019-02-18
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