| タイトル | Design and evaluation of a sensor fail-operational control system for a digitally controlled turbofan engine |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760006007 |
| 著者（英） | Arpasi, D. J.; Hrach, F. J.; Bruton, W. M. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1975-12-01 |
| 言語 | eng |
| 内容記述 | A self-learning, sensor fail-operational, control system for the TF30-P-3 afterburning turbofan engine was designed and evaluated. The sensor fail-operational control system includes a digital computer program designed to operate in conjunction with the standard TF30-P-3 bill-of-materials control. Four engine measurements and two compressor face measurements are tested. If any engine measurements are found to have failed, they are replaced by values synthesized from computer-stored information. The control system was evaluated by using a realtime, nonlinear, hybrid computer engine simulation at sea level static condition, at a typical cruise condition, and at several extreme flight conditions. Results indicate that the addition of such a system can improve the reliability of an engine digital control system. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 76N13095
NASA-TM-X-3260
E-8401 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/187841 |
