| 摘要 |
<p>This invention relates to aircraft turbine engine for preventing an aviation accident by segregating F.O.D. entering the engine during air intake. It is to provide protection apparatus for an turbine engine that does not interfere with the intake air flow while providing means to separate birds, hail and sands etc. The centrifuge (2) is disconnected with the shaft of turbine engine (10) for avoiding engine failure due to extreme vibration shock and rotated freely with the flow of intake air to generate a centrifugal power by utilizing several fans (3) on the surface of elliptical shell (4), and it can be operated only at the time of landing, take-off or emergency with an automatic controlled hydraulic system for avoiding aerodynamic drag and waist of fuel during cruise. Also, it has advantages to increase mechanical life of turbine engine with clean air and thrust power with improving compression effect on the structure of centrifuge.</p> |
