The present invention relates to a hydrogen recycle flight system and a flight method for the same. The hydrogen recycle flight system includes: an aerial moving body having at least a pair of wings on both sides of a body; a hydrogen gas balloon tightly connected to the aerial moving body; a hydrogen fuel cell installed inside or outside the aerial moving body and connected to the hydrogen gas balloon; a secondary battery charged with electricity produced by the hydrogen fuel cell, electricity produced by a solar cell installed on the outer circumference of the aerial moving body, or electricity of an outer electrical grid; a water tank converting the hydrogen fuel cell into a water electrolysis device or the water electrolysis device into the hydrogen fuel cell by a switch and storing water generated by the hydrogen fuel cell; the water electrolysis device performing electrolysis on the water stored; a switch control device for changing the functions of the hydrogen fuel cell and the water electrolysis device; and a high pressure gas container for storing hydrogen gas and oxygen gas produced from the water electrolysis device at a high pressure. The volume of the hydrogen gas balloon which is a floating force of the aerial moving body is controlled by the operation of the hydrogen fuel cell or the high pressure gas container so that the hydrogen recycle flight system can flight.

    본 발명은 수소 리싸이클 비행 시스템 및 비행방법에 관한 것으로, 몸체의 양측에 적어도 한 쌍의 날개를 갖는 비행동체와, 상기 비행동체에 기밀 연결되는 수소가스벌룬과, 상기 수소가스벌룬과 연결되고, 상기 비행동체 외부 또는 내부에 설치되는 수소연료전지와, 상기 수소연료전지로부터 생산된 전기 또는 비행동체 외주부에 구비된 태양전지로부터 생산된 전기 또는 외부 전력망 전기로 충전되는 2차전지를 포함하며, 스위치 전환으로 수소연료전지를 물전기분해장치로 또는 물전기분해장치를 수소연료전지로 전환하고, 상기 수소연료전지로부터 생성된 물을 저장하는 물탱크, 상기 저장된 물을 전기분해하는 상기 물전기분해장치와, 수소연료전지와 물전기분해장치의 기능전환을 위한 스위치 제어장치와, 물전기분해장치에서 생산된 수소가스와 산소가스를 고압저장하기 위한 고압가스통과, 비행체의 부양동력인 상기 수소가스벌룬의 부피가 상기 수소연료전지의 작동 또는 상기 고압가스통에 의해 제어되어 비행하는 것을 특징으로 한다.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aerial vehicle system using water electrolysis-hydrogen fuel cell


    Weitere Titelangaben:

    수소 리싸이클 비행시스템 및 비행방법


    Beteiligte:
    YU BYUNG DEOK (Autor:in) / MIN HYUN SOO (Autor:in) / JEON JUN JIN (Autor:in)

    Erscheinungsdatum :

    2017-04-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / C01B NON-METALLIC ELEMENTS , Nichtmetallische Elemente / F17C Behälter zum Aufnehmen oder Speichern verdichteter, verflüssigter oder verfestigter Gase , VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES



    - Energy Self-Contained Unmanned Aerial Vehicle using Electrolysis and Hydrogen Fuel Cell

    KWON SOON PYO | Europäisches Patentamt | 2021

    Freier Zugriff

    ENERGY-INDEPENDENT WATER ELECTROLYSIS FUEL CELL WATER VEHICLE SYSTEM

    KWON YONG-JIN / JO NAM-JU | Europäisches Patentamt | 2021

    Freier Zugriff

    Hydrogen fuel cell unmanned aerial vehicle

    ZHENG JINJIN / SONG KE / MU JINPENG | Europäisches Patentamt | 2023

    Freier Zugriff

    ENERGY-INDEPENDENT WATER ELECTROLYSIS FUEL CELL WATER VEHICLE SYSTEM

    KWON YONG JIN / CHO NAM JU | Europäisches Patentamt | 2020

    Freier Zugriff

    Hydrogen fuel cell unmanned aerial vehicle

    FENG BO / HAN WENYUAN / WANG HAO et al. | Europäisches Patentamt | 2023

    Freier Zugriff