Thermal barrier coating material with RF absorption capabilities at elevated temperatures

Patent metadata

Field	Value
Publication number	US-8945729-B1
Application number	US-201113241118-A
Country	US
Kind code	B1
Filing date	Sep 22, 2011
Priority date	Sep 22, 2010
Publication date	Feb 3, 2015
Grant date	Feb 3, 2015

Abstract

Embodiments disclosed herein include compositions that serve, among other things, the dual function of a thermal barrier and an RF absorber. The compositions can be applied as a single layer to an aircraft engine component, thus reducing the weight of the aircraft and eliminating an extra coating step in the manufacturing process. The coating materials are designed to protect the metal underneath from the high temperatures generated during engine operation, and also to absorb or scatter radiation which may incumbent on the metal during operation. In some implementations, the compositions comprise a two phase mixture of perovskite and magnetoplumbite.

First claim

What is claimed is:

1. A coating composition comprising a two phase mixture of LnAl 11(1-x-y) Fe x M y O 18 and LnAl 1-x-y Fe x M y O 3 , x and y both being greater than 0, x being less than 1, and y being less than or equal to 0.5, the coating composition providing the dual function of a thermal barrier and an RF absorber, Ln being selected from the group consisting of La, Pr, Nd, Sm, and combinations thereof, and M being selected from the group consisting of Co, Ni, Cu, and combinations thereof.

2. An aircraft component incorporating the composition of claim 1 .

3. The composition of claim 2 wherein the coating composition has a thermal expansion matching the aircraft component.

4. An engine turbine blade incorporating the coating composition of claim 1 .

5. The composition of claim 1 wherein the coating composition has magnetic activity in the temperature range of about 800° C.-1000° C.

6. The composition of claim 5 wherein the magnetic activity is paramagnetic or ferromagnetic activity.

7. The composition of claim 1 wherein the coating composition has a thermal expansion coefficient of about 10×10 −6 /° C. or greater.

8. The composition of claim 1 wherein the coating composition is configured to melt congruently.

9. The composition of claim 1 wherein the coating composition has a thermal conductivity equal to or less than that of yttria stabilized zirconia.

10. The composition of claim 1 wherein the coating composition further comprises perovskites or magnetoplumbites, or combinations thereof.

11. The composition of claim 1 wherein the coating composition is compatible with thermally grown aluminum oxide on bonded nickel based superalloys.

12. The composition of claim 1 wherein the coating composition does not include an Ln 3 Al 5 O 12 aluminate garnet.

13. The composition of claim 1 wherein the coating composition is configured to be used in plasma spraying.

14. The composition of claim 1 wherein the coating composition further comprises Fe and Co having octahedral co-ordination.

15. The composition of claim 1 wherein the coating composition does not decompose through peritectic melting.

16. The composition of claim 1 wherein the coating composition scatters RF.

Assignees

• Hill Michael David
• Skyworks Solutions Inc

Inventors

• Hill Michael David

Classifications

• C23C4/134 Primary

  Plasma spraying · CPC title

• C23C4/11

  Oxides · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title