| タイトル | Ceramic composite protection for turbine disc bursts |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780002140 |
| 著者（英） | Gardner, P. B. |
| 著者所属（英） | Norton Co. |
| 発行日 | 1977-03-01 |
| 言語 | eng |
| 内容記述 | Ceramic composite turbine disc protection panels for the A300B were developed using armor technology. Analytical predictions for modifying the ballistic projectile armor system were verified by a test program conducted to qualify the rotor containment system. With only a slight change in the areal density of the armor system a more than two-fold increase in kinetic energy protection level was achieved. Thickness of the fiberglass reinforced plastic backing material was increased to achieve an optimum ratio of ceramic thickness to backing thickness for the different ballistic defeat condition. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 78N10083 |
| 権利 | No Copyright |
