Strain tolerant aggregate material
View Patent ↗A material ( 100 ) formed of a sintered aggregation of ceria particles ( 106 ), mullite particles ( 108 ) and an alumina matrix material ( 110 ). Differential thermal expansion of the ceria and mullite particles generates thermal stress sufficient to create micro-cracking of the ceria particles. The ratio of ceria to mullite may be selected to achieve a desired coefficient of thermal expansion for matching the thermal growth of a mating CMC material ( 102 ). The micro cracks provide the material with a desired degree of strain tolerance useful in high temperature applications such as a solid core gas turbine vane ( 20 ).
1. A material comprising:
an aggregation of first particles comprising a network of microcracks and second particles within a binding matrix comprising a ceramic material;
wherein the first particles and the second particles are selected to have sufficiently different coefficients of thermal expansion so that thermal stresses generated there between during heating of the material result in micro cracking within at least the first particles, wherein the first particles comprise ceria and the second particles comprise mullite.
2. The material at claim 1 , wherein the difference in coefficients at thermal expansion between the first particles and the second particles is at least 3×10 −6 /°K at 850° C.
3. The material of claim 1 , wherein the difference in coefficients of thermal expansion between the first particles and the second particles is at least 4×10 −6 /°K at 850° C.
4. The material of claim 1 , wherein the difference in coefficients of thermal expansion between the first particles and the second particles is at least 5×10 −6 /°K at 850° C.
5. The material of claim 1 , wherein the binding matrix material has a coefficient of thermal expansion between that of the first particles and that of the second particles.
6. The material of claim 1 , wherein the binding matrix material comprises alumina.
7. The material of claim 1 , further comprising a volume ratio of ceria to mullite of about 1:2.
8. The material of claim 1 , further comprising a volume of ceria to mullite of at least 30%.
9. The material of claim 1 , further comprising a volume of ceria to mullite of up to about 50%.
10. The material of claim 1 , wherein the aggregation further comprises third particles of alumina within the binding matrix material.
11. The material of claim 10 , wherein the volume of The third particles to that of the first and second particles is no more than 20%.
12. The material of claim 1 , wherein at least one of the first particles and the second particles comprise hollow spheres.
13. The material of claim 1 , wherein the ceria particles have a nominal size that is larger than a nominal size of the mullite particles.
14. The material of claim 1 having a ratio of ceria content to mullite content selected to provide a coefficient of thermal expansion of at least 5.6 ×10 −6 /K at 850° C.
15. The material of claim 1 having a ratio of ceria content to mullite content selected to provide a coefficient of thermal expansion of approximately 6.5×10 −6 /°K at 850° C.
16. The material of claim 1 , wherein the thermal stresses also result in micro-cracking of the second particles.
17. A composite material comprising:
a ceramic matrix composite material;
an aggregate material comprising first particles comprising a network of microcracks and second particles within a binding matrix comprising a ceramic material bonded to a first surface of the ceramic matrix composite material;
wherein the first particles and the second particles are selected to have sufficiently different coefficients of thermal expansion so that thermal stresses generated there between during heating of the aggregate material result in a degree of micro cracking within at least one of the group consisting of the first particles and the second particles sufficient to achieve a desired degree of strain tolerance in the aggregate material, wherein the first particles comprise and the second particles comprise mullite.
18. The composite material of claim 17 , wherein the aggregate material exhibits a coefficient of thermal expansion at least 7% greater than a coefficient of thermal expansion of the ceramic matrix composite material at the same temperature.
19. The composite material of claim 17 , further comprising a layer of ceramic thermal insulating material bonded to a second surface of the ceramic matrix composite material, the ceramic thermal insulating material having an outside surface defining an airfoil shape.
20. A material comprising a sintered aggregation of ceria particles and mullite particles within a binding matrix comprising a ceramic material, wherein the ceria particles comprise a network of microcracks.
21. The malarial of claim 20 , wherein the sintered aggregation further comprises alumina particles within the binding matrix material.
22. The material of claim 20 , wherein the binding matrix material comprises alumina.
23. The material of claim 20 , further comprising a volume ratio of ceria particles to mullite particles of about 1:2.
24. The material of claim 20 , further comprising a volume of ceria particles to mullite particles of at least 30%.
25. The material of claim 20 , further comprising a volume of ceria particles to mullite particles of up to about 50%.
26. The material of claim 20 , wherein at least one of the ceria particles and the mullite particles comprise hollow spheres.
27. The material of claim 20 , wherein the ceria particles have a nominal size that is larger than a nominal size of the mullite particles.
28. The material of claim 20 , having a ratio of ceria content to mullite content selected to provide a coefficient of thermal expansion of at least 5.6×10 −6 /K at 850° C.
29. The material of claim 20 , having a ratio of ceria content to mullite content selected to provide a coefficient of Thermal expansion of approximately 6.5×10 −6 /°K at 850° C.