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Third-generation tial alloy tested: exhibits promising properties for rotating components
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Draper, Susan L. |
| Copyright Year | 2004 |
| Description | The Revolutionary Turbine Accelerator/Turbine-Based Combined Cycle (RTA/TBCC) Program for the next-generation launch vehicle has targeted gamma titanium aluminide as a potential compressor and structural material. Because of the high compressor inlet and exit temperatures, the TBCC engine requires higher temperature materials than conventional Ti alloys, and because of its stringent thrust-to-weight requirements, the engine requires low-density material to be utilized wherever possible. Third-generation gamma alloys offer higher temperature capability along with low density and high stiffness. A high-temperature, high-strength *-TiAl alloy with a high Nb-content (Gamma MET PX1) was selected for evaluation. The microstructure and mechanical properties of Gamma Met PX (GMPX) in both the as-extruded and a lamellar heat-treated condition and the influence of the microstructure on the tensile, creep, and fatigue properties were investigated in-house. |
| File Size | 109521 |
| Page Count | 3 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20050192158 |
| Archival Resource Key | ark:/13960/t6k121t9b |
| Language | English |
| Publisher Date | 2004-05-01 |
| Access Restriction | Open |
| Subject Keyword | Metals And Metallic Materials Titanium Alloys Creep Properties Heat Resistant Alloys Combined Cycle Power Generation Turbomachinery Titanium Aluminides High Strength Alloys Microstructure Niobium 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 |
