摘要 |
A protective deflector for airplane engines system is disclosed herein comprising a turbine-covering screen assembly which may be installed to an airplane engine turbine housing by a securable fastening device. The turbine-covering screen assembly comprises a protruded bell-shaped extrusion member having a plurality of apertures which may serve to prevent birds, objects and other debris from penetrating a turbine housing air-intake opening thereby protecting an airplane engine from interference during flight. The turbine-covering screen assembly does not appreciably affect the performance of the turbine engine it serves to protect.
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