| タイトル | Cost/benefit analysis of advanced materials technologies for future aircraft turbine engines |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770007083 |
| 著者（英） | Bisset, J. W. |
| 著者所属（英） | United Technologies Corp. |
| 発行日 | 1976-11-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 77N14026
PWA-5453
NASA-CR-135107 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/183684 |
