According to the present invention, an apparatus for protecting an engine of an aircraft includes: a protective net attached to an inlet arranged on a front surface of the engine of the aircraft; and a hanger fixing the protective net along a surface of a side portion of the engine. The apparatus for protecting an engine of an aircraft implements flight in a state of fastening the protective net made of a high elasticity and high strength material to a front portion of the engine of the aircraft, thereby minimizing impact applied to the engine to protect the engine.

    본 발명에 따른 항공기 엔진 보호 기구는 항공기의 엔진 전면에 배치된 흡입구에 부착되는 보호망과 상기 보호망을 상기 엔진의 측부 표면을 따라 고정시키는 행거를 포함하며, 항공기의 엔진 앞부분에 고탄성력과 고강도 재질로 이루어진 보호망을 체결한 상태에서 비행이 이루어질 수 있기 때문에 엔진에 가해지는 충격을 최소화하여 엔진을 보호할 수 있다.


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    Title :

    Engine protecting tool for aircraft


    Additional title:

    항공기 엔진 보호 기구


    Contributors:
    BAEK YOON KI (author) / BAEK YU DAM (author)

    Publication date :

    2020-11-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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