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Cost/benefit analysis of advanced materials technologies for future aircraft turbine engines
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bisset, J. W. |
| Copyright Year | 1976 |
| Description | The cost/benefits of advance commercial gas turbine materials are described. Development costs, estimated payoffs and probabilities of success are discussed. The materials technologies investigated are: (1) single crystal turbine blades, (2) high strength hot isostatic pressed turbine disk, (3) advanced oxide dispersion strengthened burner liner, (4) bore entry cooled hot isostatic pressed turbine disk, (5) turbine blade tip - outer airseal system, and (6) advance turbine blade alloys. |
| File Size | 3192185 |
| Page Count | 39 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770007083 |
| Archival Resource Key | ark:/13960/t6xw96k9n |
| Language | English |
| Publisher Date | 1976-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Cost Estimates Systems Engineering Materials Handling Product Development Aircraft Engines Cost Analysis Turbine Engines Technology Utilization Oxide Dispersion Strengthening Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |