Revisiting the Birth of 7YSZ Thermal Barrier Coatings: Stephan Stecura

被引:49
|
作者
Smialek, James L. [1 ]
Miller, Robert A. [2 ]
机构
[1] NASA, Glenn Res Ctr, Cleveland, OH 44135 USA
[2] Vantage Partners LLC, Brookpark, OH 44142 USA
来源
COATINGS | 2018年 / 8卷 / 07期
关键词
thermal barrier coatings; 7YSZ; turbine blades; TETRAGONAL ZIRCONIA; MECHANISMS; DEGRADATION; FAILURE; ENGINES; SYSTEMS; SCIENCE;
D O I
10.3390/coatings8070255
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Thermal barrier coatings are widely used in all turbine engines, typically using a 7 wt.% Y2O3-ZrO2 formulation. Extensive research and development over many decades have refined the processing and structure of these coatings for increased durability and reliability. New compositions demonstrate some unique advantages and are gaining in application. However, the 7YSZ (7 wt.% yttria stabilized zirconia) formulation predominates and is still in widespread use. This special composition has been universally found to produce nanoscale precipitates of metastable t' tetragonal phase, giving rise to a unique toughening mechanism via ferro-elastic switching under stress. This note recalls the original study that identified superior properties of 6-8 wt.% yttria stabilized zirconia (YSZ) plasma sprayed thermal barrier coatings, published in 1978. The impact of this discovery, arguably, continues in some form to this day. At one point, 7YSZ thermal barrier coatings were used in every new aircraft and ground power turbine engine produced worldwide. 7YSZ is a tribute to its inventor, Dr. Stephan Stecura, NASA retiree.
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页数:6
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