| タイトル | Control of turbofan lift engines for VTOL aircraft. |
| 著者（英） | Sellers, J. F.; Szuch, J. R. |
| 発行日 | 1973-04-01 |
| 言語 | eng |
| 内容記述 | This paper presents the results of an analytical study of the dynamics and control of turbofan lift engines, and proposes methods of meeting the response requirements imposed by the VTOL aircraft application. Two types of lift fan engines are discussed: the integral and remote. The integral engine is a conventional two-spool, high bypass ratio turbofan designed for low noise and short length. The remote engine employs a gas generator and a lift fan which are separated by a duct, and which need not be coaxial. For the integral engine, a control system design is presented which satisfies the VTOL response requirements. For the remote engine, two unconventional methods of control involving flow transfer between lift units are discussed. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 73A33496
ASME PAPER 73-GT-20 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/457064 |
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