Protective cover for aircraft engines

Abstract

A protective cover for protecting aircraft engines is disclosed, the protective cover comprising a generally circular cross-section, a circumference, an outer side, and an inner side; said circumference being defined by a frame element having generally circular ring shape formed by a rod unit; said frame element comprising a plurality of attaching mechanisms being dispersed around said ring shaped frame, and being sized and configured to releasably attach said protective cover to an engine; said generally circular cross-section comprising one or more fabric layers contained in said ring shaped frame element. The protective cover is easily installed due to its attaching mechanisms and its breathable and durability protects the engine from damage.

Dependencies are inferred from the claim text.