To provide a temperature control device for an unmanned aircraft platform.SOLUTION: A platform includes a base and a hatch cover, and the hatch cover includes a first vent hole and a second vent hole. A temperature control device includes a first temperature control part and a second temperature control part, and a heating part. The first temperature control part includes a first airflow opening and a second airflow opening, and the second temperature control part includes a third opening and a fourth airflow opening. A first airflow path is formed in following order of the first airflow opening, the first vent hole, the second vent hole, the third airflow opening, the fourth airflow opening, and the second airflow opening; or a second airflow path is formed in following order of the first airflow opening, the first vent hole, a third vent hole of the hatch cover, and the second airflow opening; or a third airflow path is formed in following order of the first airflow opening, the first vent hole, the second vent hole, the third airflow opening, the fourth airflow opening, a fourth vent hole of the hatch cover, the third vent hole, and the second airflow path. The heating part is located on the first airflow path, the second airflow path, or the third airflow path.SELECTED DRAWING: Figure 1A

    【課題】無人航空機プラットフォームの温度制御装置を提供する。【解決手段】プラットフォームは基部及びハッチカバーを含み、ハッチカバーは第1通気孔及び第2通気孔を含む。温度制御装置は、第1温度制御部、第2温度制御部及び加熱部を含む。第1温度制御部は第1空気流孔及び第2空気流孔を含み、第2温度制御部は第3空気流孔及び第4空気流孔を含む。第1空気流孔、第1通気孔、第2通気孔、第3空気流孔、第4空気流孔及び第2空気流孔の順に第1空気流経路が形成され、或いは第1空気流孔、第1通気孔、ハッチカバーの第3通気孔及び第2空気流孔の順に第2空気流経路が形成され、或いは第1空気流孔、第1通気孔、第2通気孔、第3空気流孔、第4空気流孔、ハッチカバーの第4通気孔、第3通気孔及び第2空気流孔の順に第3空気流経路が形成され、加熱部は、第1空気流経路、第2空気流経路又は第3空気流経路に位置する。【選択図】図1A


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    TEMPERATURE CONTROL DEVICE


    Weitere Titelangaben:

    温度制御装置


    Beteiligte:
    CHEN YING-CHIEH (Autor:in) / YANG YI DA (Autor:in) / ZHENG XU ZHI (Autor:in) / XIE QI DONG (Autor:in)

    Erscheinungsdatum :

    2019-10-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    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 / E01F ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE , Zusätzliche Baumaßnahmen, wie die Ausstattung von Straßen oder die bauliche Ausbildung von Bahnsteigen, Landeplätzen für Hubschrauber, Wegweisern, Schneezäunen oder dgl.



    Temperature control method and temperature control device

    YU YUE / YI ZHUSONG | Europäisches Patentamt | 2022

    Freier Zugriff

    TEMPERATURE CONTROL METHOD AND TEMPERATURE CONTROL DEVICE

    YU YUE / YI ZHUSONG | Europäisches Patentamt | 2020

    Freier Zugriff

    TEMPERATURE CONTROL DEVICE AND TEMPERATURE CONTROL SYSTEM

    WATANABE TATSUYA | Europäisches Patentamt | 2016

    Freier Zugriff

    TEMPERATURE CONTROL DEVICE AND TEMPERATURE CONTROL METHOD

    NODERA TAKAFUMI | Europäisches Patentamt | 2016

    Freier Zugriff

    TEMPERATURE CONTROL DEVICE

    YUI NOBUAKI | Europäisches Patentamt | 2021

    Freier Zugriff