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.


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    Titel :

    PROTECTIVE COVER FOR AIRCRAFT ENGINES


    Weitere Titelangaben:

    COUVERCLE DE PROTECTION POUR MOTEURS D~AERONEF


    Beteiligte:

    Erscheinungsdatum :

    2024-06-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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