{"title":"用于超轻型飞机的高功率密度(1040 W/kg)砷化镓电池","authors":"S. Wojtczuk, K. Reinhardt","doi":"10.1109/PVSC.1996.563943","DOIUrl":null,"url":null,"abstract":"Ultralight 5 /spl mu/m thick PIN GaAs solar cells were bonded to 3 mm coverglass with 1 mm of adhesive to create very high power density cells for use in ultralight aircraft. Cells were first made on a thick GaAs wafer and then bonded to a coverglass. The GaAs wafer was removed by selectively etching through the wafer to a buried etch stop in the cell epilayers. The cell was completed with a final nonalloyed back metal contact to prevent heat damage to the adhesive, as opposed to a high temperature alloyed contact used in a normal thick p-n GaAs cell. Prototype 1/spl times/1 cm cells were measured by microbalance at an average weight of 0.0228 g/cm/sup 2/ with a one-Sun AMO efficiency up to 17.3% at 28 /spl deg/C (V/sub oc/ 1.024 V, J/sub sc/ 29.9 mA/cm/sup 2/, fill factor 77.4%) for a solar cell power density of 1040 W/kg (weight including coverglass, adhesive and cell).","PeriodicalId":410394,"journal":{"name":"Conference Record of the Twenty Fifth IEEE Photovoltaic Specialists Conference - 1996","volume":"14 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1996-05-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"8","resultStr":"{\"title\":\"High-power density (1040 W/kg) GaAs cells for ultralight aircraft\",\"authors\":\"S. Wojtczuk, K. Reinhardt\",\"doi\":\"10.1109/PVSC.1996.563943\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Ultralight 5 /spl mu/m thick PIN GaAs solar cells were bonded to 3 mm coverglass with 1 mm of adhesive to create very high power density cells for use in ultralight aircraft. Cells were first made on a thick GaAs wafer and then bonded to a coverglass. The GaAs wafer was removed by selectively etching through the wafer to a buried etch stop in the cell epilayers. The cell was completed with a final nonalloyed back metal contact to prevent heat damage to the adhesive, as opposed to a high temperature alloyed contact used in a normal thick p-n GaAs cell. Prototype 1/spl times/1 cm cells were measured by microbalance at an average weight of 0.0228 g/cm/sup 2/ with a one-Sun AMO efficiency up to 17.3% at 28 /spl deg/C (V/sub oc/ 1.024 V, J/sub sc/ 29.9 mA/cm/sup 2/, fill factor 77.4%) for a solar cell power density of 1040 W/kg (weight including coverglass, adhesive and cell).\",\"PeriodicalId\":410394,\"journal\":{\"name\":\"Conference Record of the Twenty Fifth IEEE Photovoltaic Specialists Conference - 1996\",\"volume\":\"14 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1996-05-13\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"8\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Conference Record of the Twenty Fifth IEEE Photovoltaic Specialists Conference - 1996\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/PVSC.1996.563943\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Conference Record of the Twenty Fifth IEEE Photovoltaic Specialists Conference - 1996","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PVSC.1996.563943","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
High-power density (1040 W/kg) GaAs cells for ultralight aircraft
Ultralight 5 /spl mu/m thick PIN GaAs solar cells were bonded to 3 mm coverglass with 1 mm of adhesive to create very high power density cells for use in ultralight aircraft. Cells were first made on a thick GaAs wafer and then bonded to a coverglass. The GaAs wafer was removed by selectively etching through the wafer to a buried etch stop in the cell epilayers. The cell was completed with a final nonalloyed back metal contact to prevent heat damage to the adhesive, as opposed to a high temperature alloyed contact used in a normal thick p-n GaAs cell. Prototype 1/spl times/1 cm cells were measured by microbalance at an average weight of 0.0228 g/cm/sup 2/ with a one-Sun AMO efficiency up to 17.3% at 28 /spl deg/C (V/sub oc/ 1.024 V, J/sub sc/ 29.9 mA/cm/sup 2/, fill factor 77.4%) for a solar cell power density of 1040 W/kg (weight including coverglass, adhesive and cell).