| タイトル | Further industrial tests of ceramic thermal barrier coatings |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830001775 |
| 著者（英） | Liebert, C. H.; Levine, S. R. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1982-09-01 |
| 言語 | eng |
| 内容記述 | The NASA Lewis Research Center made technical assistance arrangements (contracts) with several commercial organizations under which Lewis designed plasma-sprayed thermal-barrier coatings (TBC) for their products. Lewis was then furnished with the test conditions and evaluations of coating usefulness. The coating systems were developed and sprayed at Lewis. All of the systems incorporated a two-layer, ceramic-bond coating concept. Coating thickness and chemical composition were varied to fit three applications: the leading edges of first-stage turbine vanes for an advanced gas turbine engine; the flame impingement surfaces of a combustor transition section; and diesel engine valves and head surfaces. The TBC incorporated yytria-stabilized zirconia, which lowered metal temperatures, protected metal parts, and increased metal part life. In some cases metal burning, melting, and warping were eliminated. Additional benefits were realized from these endeavors: hands-on experience with thermal-barrier coatings was provided to industry; the success of these endeavors encourages these and other organizations to accelerate the implementation of TBC technology. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 83N10045
NAS 1.60:2057
E-1184
NASA-TP-2057 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/164636 |
