不同热处理制度对GH706高温合金持久性能影响的研究结果表明,固溶加低温时效的两段热处理使合金中析出的η相呈胞状紧密排列于晶界,强化晶界,获得较长的持久寿命.增加稳定化处理的三段热处理合金,晶界η相以长针状析出,并在其周围形成γ',γ"相贫化区,贫化区强度较低,弱化了晶界,使得裂纹易于萌生,且易于连通形成扩展通道,降低了持久寿命.直接时效(DA)处理的合金中η相在晶界呈短棒状分散排列,可以起到强化晶界的作用,而η相间的无析出区可以钝化裂纹的萌生和扩展,从而获得最长的持久寿命和最高的持久塑性.
参考文献
[1] | P.W.Schilke,J.J.Pepe,R.C.Schwant,Alloy 706 metallurgy and turbine wheel application,in:Superalloys 718,625,706 and Various Derivatives,E.A.Loria ed.,(Warrendale,PA,TMS-AIME,1994) p.l |
[2] | P.W.Schilke,R.C.Schwant,Alloy 706 use,process optimization,and future directions for GE gas turbine rotor materials,in:Superalloys 718,625,706 and Various Derivatives,E.A.Loria ed.,(Warrendale,PA,TMS-AIME,2001)p.25 |
[3] | LONG Zhengdong,The progress of Inconel 706 alloy abroad,Materials Review,5,14(1995)(龙正东,国外Inconel 706合金的研究进展,材料导报,5,14(1995)) |
[4] | XU Zhichao,QU Bo,XIE Xishan.Direct aging of alloy GH169,Journal of University of Science and Technology Beijing,13(3),239(1991)(徐志超,屈波,谢锡善,GH169合金的DA处理,北京科技大学学报,13(3),239(1991)) |
[5] | O.Matsumoto,T.Honjo,Y.Yasumoto,T.Moriyama,T.Tsuchiyama,Grain boundary precipitates and mechanical properties of alloy 706,in:Superalloys 718,625,706 and Various Derivatives,E.A.Loria ed.,(Warrendale,PA,TMS-AIME,1997) p.389 |
[6] | T.Takahashi,T.Ishiguro,K.Orita,J.Taira,T.Shibata,S.Nakata,Effects of grain boundary precipitation on creep rupture properties of alloys 706 and 718 turbine disk forg-ings,in:Superalloys 718,625,706 and Various Derivatives,E.A.Loria ed.,(Warrendale,PA,TMS-AIME,1994) p.557 |
[7] | J.H.Moll,G.N.Maniar,D.R.Muzyka,Heat treatment of 706 alloy for optimum 1200(F) stress-rupture properties,Metallurgical Transactions,2,2153(1971) |
[8] | LI Xiuyan,ZHANG Jian,RONG Lijian,LI Yiyi,The precipitation mechanism of secondary η phase in a FeNi-based alloy,Chinese Journal of Materials Research,20(2),113(2006)(李秀艳,张建,戎利建,李依依,Fe-Ni基合金中次生η相的析出机理,材料研究学报,20(2),113(2006)) |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%