PROBLEM TO BE SOLVED: To provide a balloon comprising a light concentration type photovoltaic power generator and using a solar battery cell arrangement optimized for power supply to the balloon in flight.SOLUTION: A balloon (202) comprises: an air sac (4) for storing floating gas (6); and a light concentration type photovoltaic power generator (8). The photovoltaic power generator (8) comprises: a reflection mirror (10); and one or two arrays (204) of the solar battery cell for forming a first active face (208) directed to the reflection mirror (210) direction, and a second active face (36) directed to an outside direction of the air sac (4) of the balloon. The reflection mirror (10), the first active face (208) and the second active face (210) of the array(s) (204) of a photovoltaic cell (206) are configured so that, both of the first active face (208) and the second active face (210) on the array(s) (204) surely generate power, if sun positioning failure in a roll direction of the reflection mirror (10) is 10 degree or lower in an absolute value.SELECTED DRAWING: Figure 3

    【課題】集光型太陽光発電機を装備し、かつ飛行時に前記気球に動力を供給するための最適化された太陽電池セル配列を用いる気球を提供する。【解決手段】気球(202)は、浮揚ガス(6)を収容している気嚢(4)と、集光型太陽光発電機(8)とを備える。太陽光発電機(8)は、反射鏡(10)と、反射鏡(210)の方向に向いた第1の活性面(208)および気球の気嚢(4)の外部の方向に向いた第2の活性面(36)を形成する、太陽電池セルの1つまたは2つのアレイ(204)とを含む。反射鏡(10)、光起電力セル(206)のアレイ(204)の第1の活性面(208)および第2の活性面(210)は、反射鏡(10)のロール方向の太陽の位置合わせ不良が絶対値で10度以下であれば、アレイ(204)の第1の活性面(208)および第2の活性面(210)の両方が確実に発電するように構成されている。【選択図】図3


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    Title :

    BALLOON COMPRISING LIGHT CONCENTRATION TYPE PHOTOVOLTAIC POWER GENERATOR AND USING SOLAR BATTERY CELL ARRANGEMENT OPTIMIZED FOR POWER SUPPLY TO THE BALLOON IN FLIGHT


    Additional title:

    集光型太陽光発電機を装備し、かつ飛行時に前記気球に動力を供給するための最適化された太陽電池セル配列を用いる気球


    Contributors:

    Publication date :

    2017-02-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02S GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRA-RED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, E.G. USING PHOTOVOLTAIC [PV] MODULES , Erzeugung elektrischer Energie durch Umwandlung von Infrarot-Strahlung, sichtbarem Licht oder ultraviolettem Licht, z.B. unter Verwendung von Photovoltaik [PV]-Modulen



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