JP7030683B2 - 宇宙空間品質の太陽電池アレイの製造方法 - Google Patents
宇宙空間品質の太陽電池アレイの製造方法 Download PDFInfo
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Description
述べられたように、システムは、小さく(例えば15-20cm2未満など)単一の及び多接合太陽電池を利用し、ここで、正と負の端子は、太陽電池の裏面に提供され、またはそうでなければ配置される。例は、シリコンの単及び多結晶セル、量子セル、CdTeセル、CIGSセル及びIII-V族セルを含む。
これに限定されない例において、パネルは、CTE効果を最小化してパネルの硬さを最大化するために、PCB層の中にカーボンファイバ補強材を組み込む、改良したPCB形態を利用する。
セルを敷設する工程は、標準のエレクトロニクス工業のPnP設備に適合するように構成される。はんだペースト及び/または予備成形物は、太陽電池とPCBの間の電気的な接続を達成するために利用される。相互接続材料の構成は、ペースト形態及び予備成形物において、例えば、Sn96、Sn63、及びAuSnを含む。
組み立て工程は、標準のエレクトロニクス製造及び検査工程を利用する。PCBにおけるセルのパッキングの因子は、セルのX及びY方向の両方の空間を、従来の実用の0.030インチから0.003インチほどの空間に対して、減らすことによって最適化された。
個々の電力モジュールは、PCBと最も大きい許されることができる組み立て工程の大きさの工業の最もよい実用を利用することによって、生み出される。電力モジュールの中の電圧モジュールの設計は、NREと設計コストを最小限にするために標準の形態に基づくことができる。電力モジュールは、アレイ電力を増加するように、大きなパネルの組み立て品の中に配置される。これらの電力モジュールは、それぞれの電力モジュールの中に一体化されるコネクタ/接続を備える全電力アレイを形成するために、接続される。
PCBに連結される複数の太陽電池によって、形成される、電力モジュールは、大きなアレイを形成するために、硬い下地構造の上に配置される。下地構造は、電力モジュールの支持体、押し下げ機構の配置、及びヒンジ取り付け部の機構を提供する。別の実施形態において、柔軟な構造またはパネルは、お互いに複数の硬い支持構造を取り付けて使われることができる。これにより、1つの硬い構造は、さまざまな動作を提供する柔軟な構造を備える別の硬い構造に対して、動作し、関節となることを許す。
Claims (9)
- 宇宙空間品質の太陽電池アレイを製造した後に修理する方法であって、
複数の多接合太陽電池を有する多接合太陽電池ウェハを供給するステップであって、それぞれの多接合太陽電池は、太陽電池アレイの全電力性能の5%未満というわずかなパーセンテージを形成する、供給するステップと、
保護カバーガラスで多接合太陽電池ウェハを覆うステップと、
多接合太陽電池ウェハと保護カバーガラスの両方を複数の多接合太陽電池に切り出すステップであって、それぞれの多接合太陽電池は、対応する電気の端子に大きさを合わせ、形作られ、そして配置された正の電気の端子と負の電気の端子を有し、正の電気の端子と負の電気の端子の両方は、多接合太陽電池の共通の裏面に配置されて、切り出すステップと、
それぞれの多接合太陽電池の正の電気の端子と負の電気の端子が、プリント回路基板の対応する電気の端子に電気的に連結するように、それぞれの多接合太陽電池の裏面がプリント回路基板の前面と接触して、プリント回路基板の上に多接合太陽電池を配置するステップであって、プリント回路基板は、プリント回路基板層の中にカーボンファイバ補強材が組み込まれ、多接合太陽電池から多接合太陽電池への相互接続配線及びバイパス、及びブロッキングダイオードを含む電気の配線を有し、それぞれの多接合太陽電池の正の電気の端子と負の電気の端子は、プリント回路基板の電気端子の熱膨張係数と合致する熱膨張係数を有して、配置するステップと、
前記プリント回路基板から単一の多接合太陽電池のみを取り外す及び置き換えるステップと、
を備える宇宙空間品質の太陽電池アレイを製造した後に修理する方法。 - 保護カバーガラスは、多接合太陽電池ウェハを複数の多接合太陽電池に切り出す前に多接合太陽電池ウェハ上に配置される、請求項1に記載の方法。
- プリント回路基板は、硬い、請求項1に記載の方法。
- プリント回路基板は、柔軟性がある、請求項1に記載の方法。
- 多接合太陽電池ウェハは、20cm 2 程度の大きさの多接合太陽電池に切り出される、請求項1に記載の方法。
- さらに、プリント回路基板の裏面へ、バイパスとブロッキングダイオードを設置することを備える、請求項1に記載の方法。
- ピックアンドプレースロボットが、プリント回路基板の上に多接合太陽電池を配置するために使われる、請求項1に記載の方法。
- ピックアンドプレースロボットが、人が干渉することなく、プリント回路基板の上に多接合太陽電池を配置するために自動的に使われる、請求項1に記載の方法。
- 多接合太陽電池ウェハと保護カバーガラスの両方を複数の多接合太陽電池に切り出すステップは、切削工具を使って、切削工具の一回の動作で、多接合太陽電池ウェハと保護カバーガラスの両方を切り開くことを備える、請求項1に記載の方法。
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PCT/US2016/042223 WO2017019308A1 (en) | 2015-07-27 | 2016-07-14 | Solar array system and method of manufacturing |
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JP2019050351A (ja) * | 2017-06-12 | 2019-03-28 | ザ・ボーイング・カンパニーThe Boeing Company | 迂回させたソーラーセルを有するソーラーセルアレイ |
JP6790265B2 (ja) | 2017-06-30 | 2020-11-25 | 三菱電機株式会社 | 太陽光発電装置、太陽電池パドル、宇宙構造物および太陽光発電装置の製造方法 |
CN107919852A (zh) * | 2017-12-15 | 2018-04-17 | 武汉工程大学 | 一种以pcb板为底板的集成式光伏组件 |
EP3959748A1 (en) | 2019-04-26 | 2022-03-02 | Pharos Solar LLC | Half-cell photovoltaic modules |
DE102019006095A1 (de) * | 2019-08-29 | 2021-03-04 | Azur Space Solar Power Gmbh | Vereinzelungsverfahren zur Vereinzelung einer mehrere Solarzellenstapel umfasssenden Halbleiterscheibe |
EP3884526B1 (fr) | 2019-12-19 | 2022-01-19 | Airbus Defence and Space SAS | Générateur solaire flexible de satellite et son procédé de fabrication |
CN111416010B (zh) * | 2020-03-04 | 2021-11-26 | 上海空间电源研究所 | 一种太阳电池电路高压防护设计结构及其制备方法 |
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EP3329521B1 (en) | 2022-07-06 |
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US20200357940A1 (en) | 2020-11-12 |
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US10770606B2 (en) | 2020-09-08 |
US20180097133A1 (en) | 2018-04-05 |
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