항공우주 운송수단의 유체 수송 시스템 내에서 야기되는 전기적 방전의 강돌르 감소시키기 위한 방법 및 장치가 개시된다. 항공우주 운송수단이 동작한다. 항공우주 운송수단의 유체 수송 시스템은 유체 수송 시스템이 전기적 구성을 갖도록 선택된 재료로 이루어진다. 항공우주 운송수단의 동작 동안 유체 수송 시스템 내에서 야기되는 전기적 방전의 강도가 유체 수송 시스템의 전기적 구성에 의한 선택된 내성 내로 감소된다.
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.
FLUID TRANSPORT SYSTEM FOR PREVENTING ELECTRICAL DISCHARGE
전기적 방전을 방지하기 위한 유체 수송 시스템
2020-01-22
Patent
Elektronische Ressource
Koreanisch
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 / B67D Ausschenken, Abgeben oder Überleiten von Flüssigkeiten, soweit nicht anderweitig vorgesehen , DISPENSING, DELIVERING, OR TRANSFERRING LIQUIDS, NOT OTHERWISE PROVIDED FOR / F16L PIPES , Rohre |
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