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Experimental evaluation of foil-supported resilient-pad gas-lubricated thrust bearing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nemeth, Z. N. |
| Copyright Year | 1977 |
| Description | A new type of resilient-pad gas thrust bearing was tested to determine the feasibility of the design. The bearing consists of carbon graphite pads mounted asymmetrically on foil beams. Two bearing configurations were tested at thrust loads from 27 to 80 newtons at speeds to 9000 rpm. The outside diameter of the bearing was 8.9 centimeters. |
| File Size | 982138 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770024558 |
| Archival Resource Key | ark:/13960/t90912g4s |
| Language | English |
| Publisher Date | 1977-09-01 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Pad Performance Tests Torque Gas Lubricants Thrust Bearings Graphite Turbomachinery Thrust Loads Foil Bearings Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
