回顾了低膨胀高温合金的发展历史."因瓦效应"和"时效硬化"现象的发现奠定了低膨胀高温合金发展的基础.20世纪70年代航空航天事业的迅猛发展以及能源危机的爆发为低膨胀高温合金在航空航天业的实际应用提供了宝贵的契机, 最早的商用Fe-Ni-Co(IN9××)系列合金,经过用Nb、Ti强化,去Al,加Si等一系列成分上的变化,显著改善其应力加速晶界氧化脆性(SAGBO性能),从此低膨胀高温合金在航空航天领域得到大量应用.为改善此类合金的抗氧化和降低裂纹扩展速率等性能,又进行了新合金系的研究,即以Inconel 783合金为代表的Fe-Ni-Co-Al-Cr系合金和以Haynes 242合金为代表的Ni-Mo-Cr系合金的研究,这些合金在750℃仍能达到完全抗氧化,为新一代飞机发动机的发展提供了优质材料.
参考文献
[1] | Smith D F;SMITHJS.A history of controlled low thermal expansion superalloys[A].,1990:253-272. |
[2] | SCOTT Howard .Expansion properties of low-expansion Fe-Co-Ni Alloys[J].Transactions of The American Institute of Mining and Metallurgical Engineers,1930,89:506-537. |
[3] | HUNSICKER H Y;STUMPF H C.History of precipitation hardening[A].New York: Gordon and Breach Science Publishers,1965:271-311. |
[4] | Pilling N B;TALBOT A M .Age Hardenable,Nickel - Iron - Chromium - Titanium Alloy Possessing Controlled Thermoelastic Properties[P].US 2266482,1941. |
[5] | Eiselstein H L;BELL J K .Alloy Characterized by Controlled Thermoelasticity at Elevated Temperatures[P].US 3157495,1964. |
[6] | Huntington Alloys .INCOLOY alloy 903[R].5M 7-78 s-51 |
[7] | SMITH D F;WENSCHHOF D E.A Survey of Progress in Controlled-Expansion[A].,1971:18-21. |
[8] | WANNER E A;DEANTONIO D A;SMITH D F et al.The current status of controlled thermal expansion superalloys[J].Journal of Metals,1991,43(03):38-43. |
[9] | SMITH D F;TILLACK D J.燃汽涡轮用的低膨胀超级合金[A].北京,1985 |
[10] | BRICKNELL R H;WOODFORD D A .Grain-boundary embrittlement of the iron-base Superalloy IN903A[J].Metallurgical and Materials Transactions,1981,12:1673-1679. |
[11] | Inco Alloys International .INCOLOY alloy 907[R].Publication No. IAI-22 |
[12] | Smith J S;SMITH D F .Controlled Expansion Alloy[P].US:4487743,1984. |
[13] | Inco Alloys International .INCOLOY alloy 909[R].Publication No. IAI-18,1987. |
[14] | HECK K A;SMITH D F;SMITH J S.The Physical Metallurgy of a Silicon-Containing Low Expansion Superalloy[A].,1988:151-160. |
[15] | SATO Koji;OHNO Takehiro.Development of Low Thermal Expansion Superalloys[A].,1992:247-255. |
[16] | EDWARD A Wanner;DANIEL A DeAntonio.Development of A New Controlled Thermal Expansion Superalloy with Improved Oxidation Resistance[A].,1992:237-246. |
[17] | HECK K A;SMITH D F;HOLDERBY M A.Three-Phase Controlled Expansion Superalloys with Oxidation Resistance[A].,1992:217-226. |
[18] | TUNDERMANN J H .Development of INCONEL alloy 783, A Low Thermal Expansion, Crack growth resistant Superalloys[R].Inco alloys International. Inc. Huntington 25705-1771 |
[19] | SMITH John S;HECK Karl A.Development of A Low Thermal Expansion, Crack Growth Resistant Superalloy[A].,1996:91-100. |
[20] | HAYNES Home .HAYNESR 242TM alloy[R].Haynes International, Inc |
[21] | SRIVASTAVA S K.A Low-Thermal Expansion, High Strength Ni-Mo-Cr Alloy[A].,1992:227-236. |
[22] | MA L Z;CHANG K-M;MANNAN S K.Effect of Heat Treatment on Fatigue Crack Propagation in Inconel Alloy 783[A].,2000:131-139. |
[23] | 张绍维 .低膨胀高温合金的发展与应用[J].航空制造工程,1994,9:5-8. |
[24] | CARPENTER H W.Alloy 903 Helps Space Shuttle Fly[J].Metal Progress,1976:25-29. |
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%