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Progress toward determining the potential of ods alloys for gas turbine applications
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hoppin II, G. Sheffler, K. Dreshfield, R. L. |
| Copyright Year | 1983 |
| Description | The Materials for Advanced Turbine Engine (MATE) Program managed by the NASA Lewis Research Center is supporting two projects to evaluate the potential of oxide dispersion strengthened (ODS) alloys for aircraft gas turbine applications. One project involves the evaluation of Incoloy (TM) MA-956 for application as a combustor liner material. An assessment of advanced engine potential will be conducted by means of a test in a P&WA 2037 turbofan engine. The other project involves the evaluation of Inconel (TM) MA 6000 for application as a high pressure turbine blade material and includes a test in a Garrett TFE 731 turbofan engine. Both projects are progressing toward these engine tests in 1984. |
| File Size | 3178362 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830014116 |
| Archival Resource Key | ark:/13960/t86h9d10v |
| Language | English |
| Publisher Date | 1983-01-01 |
| Access Restriction | Open |
| Subject Keyword | Metallic Materials Gas Turbines Turbine Blades Engine Tests Combustion Chambers Dispersion Inconel Trademark Oxide Dispersion Strengthening 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 |
