期刊文献+

钛合金基体EB-PVD热障涂层的制备与初步研究 被引量:1

Preparing and Study of EB-PVD Thermal Barrier Coatings on Titanium Substrates
下载PDF
导出
摘要 在TC11钛合金上制备两种以NiCoCrAlY为粘结层,8wt%Y2O3-ZrO2(YSZ)为陶瓷层的热障涂层,粘结层制备技术分别为电子束物理气相沉积(EB-PVD)和超音速火焰喷涂(HVOF),陶瓷层由EB-PVD同炉沉积。两种热障涂层的微结构、显微硬度及热循环测试表明,EB-PVD制备的粘结层均匀致密,上层YSZ组织细密,硬度较高,而HVOF获得的粘结层疏松不均,上层YSZ晶粒粗大,硬度较低;前者有较好的抗热冲击性能,裂纹较分散,防护性能较好,而后者易开裂剥落,裂纹密集,防护性能较差。 Two kinds of thermal barrier coatings with NiCoCrAlY bond coatings deposited by electron beam-physical vapor deposition (EB-PVD) and high velocity oxy-fuel thermal spraying (HVOF), respectively, as well as 8wt% Y2O3-ZrO2 ceramic layers deposited in one batch by EB-PVD were prepared on near-α titanium alloys. The field emission scanning electronic microscopy and microhardness indentation were used in comparatively study of microstructures, microhardness of samples. Cracking modes and crack characteristics in TBCs were investigated after thermal cycling in atmosphere, along with the discussion of roles of residual stresses, bonding strengths and mechanical properties of bonding coats in different failure extents. It is found that morphologies of BCs deposited by different methods (EB-PVD and HVOF) resulted in the different microstructures and microhardness of their upper YSZ. The denser and more homogeneous BC prepared by EB-PVD led to the YSZ with slim and dense columnar clusters and higher microhardness, and the inhomogeneous and porous latter resulted in the upper YSZ with coarse and loose bonded columnar grains and lower microhardness, and the TBC with BC deposited by EB-PVD was more protective, which was synthetically induced by residual stresses, bonding strengths and mechanical properties of bonding coats.
出处 《航空材料学报》 EI CAS CSCD 2007年第4期25-30,共6页 Journal of Aeronautical Materials
关键词 近Α钛合金 热障涂层 电子束物理气相沉积 超音速火焰喷涂 near-α titanium alloy thermal barrier coatings electron beam-physlcal vapor deposition high velocity oxy-fuel
  • 相关文献

参考文献21

  • 1LEYENS C,PETERS M,KAYSSER W A.Oxidation-resistant coatings for application on high-temperature titanium alloys in aeroengines[J].Advanced Engineering Materials,2000,2 (5):265-269.
  • 2LONG M,RACK H J.Titanium alloys in total joint replacement-a materials science perspective[J].Biomaterials,1998,19(18):1621-1639.
  • 3LEYENS C,PETERS M,KAYSSER W A.Intermetallic Ti-Al coatings for protection of titanium alloys:oxidation and mechanical behavior[J].Surface & Coatings Technology,1997,94 -5(1 -3):34 -40.
  • 4LEYENS C,BRAUN R,FROHLICH M,et al.Recent progress in the coating protection of gamma titaniumm aluminides[J].Jom,2006,58(1):17 -21.
  • 5LEYENS C,PETERS M,HOVSEPIAN P E,et al.Novel coating systems produced by the combined cathodic arc/unbalanced magnetron sputtering for environmental protection of titanium alloys[J].Surface & Coatings Technology,2002,155 (2 -3):103-111.
  • 6LEYENS C,VAN LIERE J W,PETERS M,et al.Magnetron-sputtered Ti-Cr-Al coatings for oxidation protection of titanium alloys[J].Surface & Coatings Technology,1998,109(1 -3):30 -35.
  • 7唐兆麟,王福会,吴维.高温钛合金及钛铝金属间化合物腐蚀与防护[J].稀有金属,1996,20(4):291-296. 被引量:9
  • 8PADTURE N P,GELL M,JORDAN E H.Materials science-thermal barrier coatings for gas-turbine engine apptications[J].Science,2002,296 (5566):280-284.
  • 9DOBBINS T A,KNIGHT R,MAYO M J.HVOF thermal spray deposited Y2O3 -stabilized ZrO2 coatings for thermal barrier applications[J].Journal of Thermal Spray Technology,2003,12(2):214 -225.
  • 10EVANS A G,MUMM D R,HUTCHINSON J W,et al.Mechanisms controlling the durability of thermal barrier coatings[J].Progress in Materials Science,2001,46(5):505 -553.

二级参考文献25

  • 1王福会,楼翰一,吴维(山文).CoCrAl微晶涂层对TiAl金属间化合物抗高温氧化性能的影响[J].金属学报,1993,29(3). 被引量:5
  • 2张亚明,周龙江,王卫林,李铁藩,陈崇伟.钛合金表面渗铝的研究[J].稀有金属材料与工程,1993,22(1):27-30. 被引量:12
  • 3王福会,楼翰一,吴维欱.高温合金微晶涂层研究之进展[J].真空科学与技术,1994,14(4):287-293. 被引量:6
  • 4[1]Zhou Y C, Hashida T. Thermal fatigue failure induced by delamination in thermal barrier coating[J]. International J Fatigue, 2002, 24(4): 407-417.
  • 5[2]Karlsson A M, Xu T, Evans A G, et al. The effect of the thermal barrier coating on the displacement instability in thermal barrier systems[J]. Acta Materialia,2002, 50: 1211- 1218.
  • 6[3]Kokini K, DeJonge J, Ranqarai S, et al. Thermal shock of functionally graded thermal barrier coatings with similar thermal resistance[J]. Surf Coat Technol,2002, 154(2): 223-231.
  • 7[4]Khor K A, Gu Y W. Thermal properties of plasmasprayed functionally graded thermal barrier coatings[J]. Thin Solid Films, 2000, 372(1): 104 - 113.
  • 8[5]Gao Y, Chen M C, Shi C X. Study on EB-PVD zirconia thermal barrier coatings for gas turbine blade protection[J]. Materials and Manufacturing Processes,1999, 14(5): 691-696.
  • 9[6]Zhu D M, Miller R A, Nagaraj B A, et al. Thermal conductivity of EB-PVD thermal barrier coatings evaluated by a steady-state laser heat flux technique[J].Surf Coat Technol, 2001, 138(1): 1 - 8.
  • 10[7]Herr W, Broszeit E. The influence of a heat treatment on the microstructure and mechanical properties of sputtered coatings[J]. Surf Coat Technol, 1997, 97(2): 335 - 340.

共引文献12

同被引文献16

引证文献1

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部