| タイトル | Containment of composite fan blades |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790023177 |
| 著者（英） | Stotler, C. L.; Coppa, A. P. |
| 著者所属（英） | General Electric Co. |
| 発行日 | 1979-07-01 |
| 言語 | eng |
| 内容記述 | A lightweight containment was developed for turbofan engine fan blades. Subscale ballistic-type tests were first run on a number of concepts. The most promising configuration was selected and further evaluated by larger scale tests in a rotating test rig. Weight savings made possible by the use of this new containment system were determined and extrapolated to a CF6-size engine. An analytical technique was also developed to predict the released blades motion when involved in the blade/casing interaction process. Initial checkout of this procedure was accomplished using several of the tests run during the program. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 79N31348
NASA-CR-159544
R79AEG197 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/174670 |
