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High Temperature Solid Lubricant Coatings

Coating Cross-section

PS304 Coating Cross-section

During start-up and shut down, prior to developing a gas film, sliding occurs between the shaft and top (inner) foil surfaces. Solid lubrication must be provided to reduce friction and wear. Traditional solid lubricants (e.g., graphite, Teflon®) readily solve this problem at low temperature. High temperature operation, however, had been a key obstacle. Without a suitable high temperature coating, foil air bearing use is limited to about 300°C (570°F). A new chrome oxide based journal coating, designated PS300, has been shown to provide good friction and wear properties in foil bearings at least to 650°C (1200°F). Subsequent development of PS304 coating has promise of enabling the turbomachinery foil bearing coating objectives:

  • Provide start/stop wear protection for foil bearings
  • Operate from cold start to 815°C (1500°F)
  • No vaporization or emissions
  • Machineability

PS300 Patent(Download Accessible GIF Plug-in)

NASA PS304 - US Patent No. 5866518

U.S. Patent No. 5,866,518 'Self-Lubricating Composite Containing Chromium Oxide', awarded 2 February 1999

bulletWide temperature spectrum solid lubricant coating
bulletPS304 has successfully lubricated foil bearings at high loads for 100,000 start/stop cycles from 25° to 650°C (75° to 1200°F)

PS300 Series Development

Coating Process Development

Plasma Spraying

Processing Steps

Plasma spray coating is a well established thermal spray process in which the powder form of the desired coating material is injected into an electrically ionized Argon plasma in a plasma spray gun. The injected powders melt and are accelerated onto the substrate to be coated. Substrate preparation typically consists of undercutting the surface to accept the coating (usually 0.005-0.010" thick). The coating is oversprayed and then finish ground to achieve a specified or desired surface finish and dimension. Plasma sprayed coatings can be polished or put into use in the as ground condition. Porosity levels are low, typically less than 15%. Following repeated rubbing contact, wear debris often "fills in" surface pits and voids yielding mirror smooth surfaces.

Undercut shaft

Undercut shaft

Sandblast finish

Sandblast finish

Plasma spray

Plasma sprayed finish

Finish grind

Finish grind

After initial use

After initial use


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Note: The listings on this page do not constitute an endorsement by the Federal Government (also see the NASA Website Disclaimer Statement). Rather, they are used as a means to foster greater dissemination of information and use of foil bearing technology. Companies wishing to be added should contact the web page curator shown below.


Responsible NASA Official: Dr. Christopher DellaCorte
Curator: Michelle L. Beagle
Last Update: April 7, 2008
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