A comparison between the erosion behaviour of thermal spray and electron beam physical vapour deposition thermal barrier coatings

被引:152
作者
Nicholls, JR
Deakin, MJ
Rickerby, DS
机构
[1] Rolls Royce PLC, Derby DE2 8BJ, England
[2] Cranfield Univ, Cranfield MK43 0AL, Beds, England
关键词
erosion behaviour; thermal spray; EB-PVD;
D O I
10.1016/S0043-1648(99)00214-8
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Thermal barrier coating (TBC) technology is used in the hot sections of gas turbines to extend component Life. To maximise these benefits, the TBC has to remain intact through the life of the turbine. High velocity ballistic damage can lead to total thermal barrier removal, while erosion may lend to progressive loss of thickness during operation. This paper compares the erosion behaviour of thermally sprayed and electron beam physical vapour deposited (EB-PVD) TBCs. A unique high velocity gas Sun has been developed with the capability of impacting TBCs at particle velocities up to 300 m/s at test temperature up to 920 degrees C. Using this facility it was found, both at room temperature and 910 degrees C, that EB-PVD ZrO2-8 wt.% Y2O3 thermal barriers are significantly mon erosion-resistant than the equivalent plasma spray coating, when impacted with either alumina or silica in the particle size range 40-100 mu m. Examination of tested hardware reveals that cracking occurs within the near surface region of the columns for EB-PVD ceramic and that erosion occurs by removal of these small blocks of material. In stark contrast, removal of material for plasma sprayed ceramic occurs through poorly bended splat boundaries. This difference in material removal mechanism accounts for the seven- to 10-fold improvement, in erosion resistance observed for EB-PVD TBCs over those produced by plasma spraying. At both room temperature and 910 degrees C, erosion rates are linear with velocity for both types of coating. When impacted with hard particles (alumina at room temperature and 910 degrees C, silica at room temperature) peak erosion rates occur for normal impact, with impact angle dependence scaling similarly for the air plasma sprayed (APS) and EB-PVD coatings. At high temperatures, erosion rates are increased over these measured at room temperature, consistent with the higher test velocities achieved at 910 degrees C. (C) 1999 Published by Elsevier Science S.A. All rights reserved.
引用
收藏
页码:352 / 361
页数:10
相关论文
共 24 条
[1]  
*AGARD, 1998, R823 AGARD
[2]  
Bose S., 1995, THERM BARR COAT WORK, P63
[3]  
HANSCHUH RF, 1984, TP2406 NASA
[4]  
JAMES EAJ, 1984, GAS DYNAMIOCS
[5]  
LAWSON KJ, 1997, ADV SURF ENG, V1, P83
[6]  
MEIER SM, 1992, J ENG GAS TURBINES P, V114
[7]  
MEIER SM, 1994, J ENG GAS TURBINES P, V116
[8]   CURRENT STATUS OF THERMAL BARRIER COATINGS - AN OVERVIEW [J].
MILLER, RA .
SURFACE & COATINGS TECHNOLOGY, 1987, 30 (01) :1-11
[9]  
MILLER RA, 1989, IMPROVED DURABILITY
[10]  
MORRELL P, 1998, THERMAL BARRIER COAT