The invention belongs to an auxiliary helicopter detection method, and particularly relates to a method for identifying tail rotor blade air bag types through air bag separating face traces. On the premise of not damaging tail rotor blades, by means of an existing inspection method, which one of French finished silica gel air bags, French tool self-manufactured silica gel gags and domestic tool self-manufactured silica gel air bags are used as the tail rotor blades can not be distinguished. Thus, the method for accurately identifying the air bag type on the premise of not damaging the tail rotor blades is needed. In order to go aground as quick as possible and avoiding great economic loss, which one of the French finished silica gel air bags, the French tool self-manufactured silica gel gags and the domestic tool self-manufactured silica gel air bags are used as silica gel air bags used for tail rotor blade forming needs to be identified and determined. By means of the method, the silica gel air bag state used for tail rotor blade forming can be easily, conveniently, visually, rapidly and accurately identified, the go-around requirement of users can be met to the maximum extent, the user aircraft attendance rate is increased, and completion of user flying tasks is ensured.


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    Title :

    Method for identifying tail rotor blade air bag types through air bag separating face traces


    Contributors:
    LI FUPIAO (author) / CHEN GUANG (author) / LI PENG (author) / WANG YAN (author) / DENG YUBAO (author)

    Publication date :

    2015-08-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / 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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