본 발명은, 항공우주 운송수단의 유체 수송 시스템 내에서 야기되는 전기적 방전의 강도를 감소시키기 위한 방법 및 장치를 개시한다. 하나의 실례로 되는 실시예에 있어서, 장치는 수송 부재를 구비하여 구성된다. 수송 부재는 유체 수송 시스템에서 이용하기 위해 구성된다. 수송 부재가, 수송 부재를 따라, 전자기 사건에 응답하여 유도된, 전압 및 전류를 감소시키도록 구성된 재료로 이루어진다.

    A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. The aerospace vehicle is operated. The fluid transport system in the aerospace vehicle is comprised of materials selected such that the fluid transport system has an electrical configuration. The intensity of the electrical discharge that occurs within the fluid transport system during operation of the aerospace vehicle is reduced to within selected tolerances by the electrical configuration of the fluid transport system.


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    Title :

    COMPOSITE TUBES FOR A FLUID TRANSPORT SYSTEM


    Additional title:

    유체 수송 시스템용 복합재 튜브


    Publication date :

    2020-01-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    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 / B64G Raumfahrt , COSMONAUTICS / F16L PIPES , Rohre



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