Synthetic diamond overlays for gas turbine engine parts having t

Details Synthetic diamond overlays for gas turbine engine parts having t Synthetic diamond overlays for gas turbine engine parts having t

1997-09-11

2000-08-08

King, Roy V.

Stock material or miscellaneous articles

All metal or with adjacent metals

Composite; i.e., plural, adjacent, spatially distinct metal...

428629, 428634, 428678, 416241B, B21D 3900

Patent

active

060999764

ABSTRACT:
This invention discloses new and improved multi-layer coatings for gas turbine engine parts that are exposed to elevated temperatures, such as blades and vanes in the high pressure compressor and turbine of multi-stage aircraft engines, by applying a diamond film over columnar thermal barrier coatings such as yttria-stabilized zirconia, improving the erosion resistance of the thermal barrier coating.

REFERENCES:
patent: 4321311 (1982-03-01), Strangman
patent: 4676994 (1987-06-01), Demaray
patent: 5800879 (1998-09-01), Moran et al.
Kanetkar et al, Appl. Phys. lett. 63(6), pp. 740-742, Aug. 1993.

Affiliated with

Also associated with

Rating

Synthetic diamond overlays for gas turbine engine parts having t does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Synthetic diamond overlays for gas turbine engine parts having t, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Synthetic diamond overlays for gas turbine engine parts having t will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1148384