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Thermal Conductivity and Water Vapor Stability of Ceramic HfO2-Based Coating Materials PDF

2004·15.7 MB·English
by  ZhuDong-Ming
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A paper abstract to be submitted to The 105th Annual Meeting & Exposition of The American Ceramic Society April 27 - 30,2003, Nashville, Tennessee Thermal Conductivity and Water Vapor Stability of Ceramic Coating Materials A Dongming Zhu, Dennis S. Fox, Narottam P. Bansal and Robert A. Miller NASA John H. Glenn Research Center Cleveland, Ohio 44135 HfQ-Y203 and La2Zr207 are candidate thermal/environmentalb arrier coating materials for gas turbine ceramic matrix composite (CMC) combustor liner applications because of their relatively low thermal conductivity and high temperature capability. In this paper, thermal conductivity and high temperature phase stability of plasma-sprayed coatings and/or hot-pressed Hf02-5mol%Y203, HiQ- 15 mol%Y203a nd La2Zr207 were evaluated at temperatures up to 1700°C using a steady-state laser heat-flux technique. Sintering behavior of the plasma-sprayed coatings was determined by monitoring the thermal conductivity increases during a 20-hour test period at various temperatures. Durability and failure mechanisms of the Hf02-Y203 and LazZr207 coatings on mullite/SiC Hexoloy or CMC substrates were investigated at 1650°C under thermal gradient cyclic conditions. Coating design and testing issues for the 1650°C themal/FtnulmnmF?ntnlharrip.~ ~ ~ ~ 1 i c a t i o n s ~ e~di~scu~ssaedl, s o - b A- cn .0- E P 2 a, 0 U t a, 0 Q) S w B = C rn m t Q) i ) a Q) cn rn m I 0" L. r I. 0 . .- . z m .X- U cn m II m I cn - 0 0" L a, 0 .a, CSE"I E" .5 ccnn .S- a .8- ca, II P 0h .a, CmI .S- > I L 0 c cn a, cn L 0 m + S a 0 3 c u ca, II S -0- .0- I S .a-, L n 0 0 a, cn > E II c U m til 0 h m S a a 0 -a, aL, m L0. 00 ..S- 12 U.m z -0L \E" 0 0, . b 5 U a, 0 a, .A r. cn E" .S- .aL, L L c.v- ) . 0 r.S-n .E 8 L . c 0 m 5 a, 0 A c 0 cn a, a, -0 + cm 0m .a, S .0S- Ua, 0 5 . cn X I v, ie0 I .cn m3 Uc .aL, cS vm, a0, aL, ca, US 0 S m S 0 3 S II .0- La, cn in cn Sm 0.- 0 I- m E L .c r.n v, S a, 0 a, .-0- a, a .S- 0 4L& .Q a, -E.-- -.E- *-. a, a 7 a, cn m c 0 .a, 0 .na-, E" c .a- aa, 0 0 +m c cn m S X n0 .23, z U 2.c-4n U. US S0 U*a, .S- 0 Sm a, . 0 cn m mav>, m J .A U m .a, 0 .el ..0S- cn 0 m 12 0 .>- m> .S- m a>, uj I S 0" .cn I 0 4-J 0 a, v, 0 .0- III .55L- E0" USS aLa,, U.ma, .aa, .a, *aX, 0" 5a, U.4S--J 0 0 c c S >-" 0 12 0 0 3 cn II 3 0 a 6 0 L a m S W 'I i= D 0 'CJ 0 Q) 0 0 C m > 'CJ m S CCI 5.- 3 n 0 U c r , A $r" Y Ea, W 0 tn W i= CI 3 0 5 '5 O E hm 4 w .I m > Q a v) m S .I .c, L m - 50"' \ c 8 I- I 0N- L r . a m S B- c1 rn 0 m n 0 L 0 S 0 0 m- cn cn 0 L 2- m 0 Q) Urc n 0 0 W E - _ -e!-! m- > 0 m - CI CI 0 Q m S S 0 L cn 0 L a 0 0 L - - 0 Q S m CI m > E 0 L h L L 0 Q) CI Q) 2 Q) c +c 8- E U a, m .4m-J a CI Ul cn .I v, L a a, > -cn .- fa S 0 IT3 - v, S L - m m $ Q Qc) U 0" I.I (3 I I- >r S 13 a, IT3 S a 0 L S E 8- E .0 L 0 a .- -I U h, i IT3 U a, 0 S m > U m - I - . 0 W : E" L a, E I- - m S 9 0L I-- . F 0 0 0 0 0 0 0 0 0 0 In 0 0 T 3 d & IA 0 I 0 0 0 00 L3 9 N 0 3 - 9 L? 9 v! 9 v! 9 rcr N N d 0 0

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