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1. 发明申请

WO2010096709A3 SOLAR CHARGEABLE BATTERY FOR PORTABLE DEVICES 审中-公开
标题翻译：便携式设备的太阳能充电电池
公开(公告)号：WO2010096709A3
公开(公告)日：2011-04-21
申请号：PCT/US2010024810
申请日：2010-02-19
申请人： SUNCORE INC , ENGLISH PETER , BRIMMER STEVEN R
发明人： ENGLISH PETER , BRIMMER STEVEN R
IPC分类号： H02J7/35 , H01M10/46
CPC分类号： H02J7/35 , H01L31/02021 , H01M10/052 , H01M10/443 , H01M10/465 , H02S40/38 , Y02E10/566 , Y02E60/122
摘要： A solar chargeable battery comprises a built-in photovoltaic array and a programmable battery charging circuit. The photovoltaic array provides a variable power source in response to light. The battery charging circuit receives the variable power source and operates in different modes to charge the battery over a range of lighting conditions. For example, the battery charging circuit charges the battery to a substantially fixed regulated voltage level in a first mode when a voltage level of the variable power source is above a predefined threshold. The battery charging circuit charges the battery to an adjustable regulated voltage level in a second mode when the voltage level of the variable power source is below the predefined threshold.
摘要翻译：太阳能可充电电池包括内置光伏阵列和可编程电池充电电路。光伏阵列响应于光提供可变电源。电池充电电路接收可变电源并以不同的模式操作，以在一定范围的照明条件下对电池充电。例如，当可变电源的电压水平高于预定阈值时，电池充电电路在第一模式中将电池充电至基本固定的调节电压电平。当可变电源的电压水平低于预定阈值时，电池充电电路在第二模式中将电池充电到可调节的调节电压电平。

2. 发明申请

WO2010096715A2 PHOTOVOLTAIC MULTI-JUNCTION WAVELENGTH COMPENSATION SYSTEM AND METHOD 审中-公开
标题翻译：光伏多功能波长补偿系统及方法
公开(公告)号：WO2010096715A2
公开(公告)日：2010-08-26
申请号：PCT/US2010024818
申请日：2010-02-19
申请人： SUNCORE INC , ENGLISH PETER
发明人： ENGLISH PETER
IPC分类号： H01L31/0224
CPC分类号： H01L31/022425 , H01L31/02021 , H01L31/0504 , H01L31/0687 , H01L31/06875 , H01L31/0725 , H01L31/076 , H02S50/10 , Y02E10/544 , Y02E10/548 , Y10T307/729
摘要： Systems and methods are disclosed for current loss compensation in multi-junction photovoltaic cells. The use of direct electrical contact with the interconnect layers in a multi-junction PV cell can improve cell efficiency over variable lighting conditions. Electrical contact with some or all of the interconnect layers can advantageously permit disconnection of subcells operating at low current or voltage. The result is multi-junction PV cells that can adapt to variable lighting conditions and compensate for a decrease in current in certain subcells, thereby advantageously improving a multi-junction PV cell's total output current.
摘要翻译：公开了用于多结光伏电池中的电流损耗补偿的系统和方法。在多结PV太阳能电池中使用与互连层的直接电接触可以在可变照明条件下提高电池效率。与一些或所有互连层的电接触可以有利地允许以低电流或电压工作的子电池的断开。结果是可以适应可变照明条件并补偿某些子电池中的电流降低的多结PV电池，从而有利地改善多结PV电池的总输出电流。

3. 发明申请

WO2011092480A3 ELECTRICAL APPARATUS FOR AN ELECTROTHERMAL ICE PROTECTION SYSTEM 审中-公开
标题翻译：电热保护系统的电气设备
公开(公告)号：WO2011092480A3
公开(公告)日：2011-09-29
申请号：PCT/GB2011000122
申请日：2011-01-31
申请人： GKN AEROSPACE SERVICES LTD , LEWIS STUART MARTIN , ENGLISH PETER
发明人： LEWIS STUART MARTIN , ENGLISH PETER
IPC分类号： B64D15/12 , H05B3/36
CPC分类号： B64D15/12 , H05B3/18 , H05B3/36 , H05B2203/013 , H05B2203/016 , H05B2203/017 , H05B2203/033 , H05B2214/02 , Y10T29/49083
摘要： Electrical apparatus such as a heater (2) for an ice protection system for an aircraft (1) comprises a laminate such as a heater mat (3) and a connector (41-49). The laminate (3) comprises dielectric layers (50-58) and an electrical element such as a heater element (501), and each dielectric layer of the laminate comprises thermoplastic material. The connector (41-49) comprises a ribbon having first and second ends and a metal conductor (413, 423, 433). The ribbon comprises thermoplastic material and its first end (415, 425, 435, 445, 455, 465, 475, 485) is embedded in the laminate and is laminated to adjacent first and second ones of the dielectric layers (50-58) of the laminate. Because the thermoplastic material of the ribbon is the same as or is compatible with the thermoplastic material of the first and second dielectric layers, the formation of an undesirable discontinuity at the interfaces between the first end of the ribbon and the first and second dielectric layers is prevented. Thus, cracks are less likely to be initiated at the interfaces during the use of the electrical apparatus, and de- lamination is less likely to occur.
摘要翻译：用于飞机（1）的用于冰保护系统的加热器（2）的电气设备包括诸如加热垫（3）和连接器（41-49）的层压体。层压体（3）包括电介质层（50-58）和诸如加热元件（501）的电气元件，层压体的每个电介质层包括热塑性材料。连接器（41-49）包括具有第一和第二端的金属带和金属导体（413,423,433）。该带包括热塑性材料，并且其第一端（415,425,435,445,455,465,475,485）嵌入在层压体中并被层压到邻近的第一和第二电介质层（50-58）的相邻的第一和第二电介质层层压板。由于带的热塑性材料与第一和第二介电层的热塑性材料相同或相容，因此在带的第一端和第一和第二介质层之间的界面处形成不期望的不连续性是预防。因此，在使用电气设备期间，在界面处不太可能发生裂纹，并且不太可能发生剥离。

4. 发明申请

WO2011092479A3 DIELECTRIC COMPONENT WITH ELECTRICAL CONNECTION 审中-公开
标题翻译：具有电气连接的电介质元件
公开(公告)号：WO2011092479A3
公开(公告)日：2011-10-06
申请号：PCT/GB2011000121
申请日：2011-01-31
申请人： GKN AEROSPACE SERVICES LTD , WINTER NICHOLAS JOHN , LEWIS STUART MARTIN , ENGLISH PETER
发明人： WINTER NICHOLAS JOHN , LEWIS STUART MARTIN , ENGLISH PETER
IPC分类号： B64D15/12 , H05B3/36
CPC分类号： B64D15/12 , H05B3/36 , H05B2203/013 , H05B2203/017 , H05B2203/033 , H05B2214/02 , Y10T29/49082
摘要： A dielectric component with electrical connection is provided for a laminated heater mat (3) for an ice protection system for an aircraft (1). The dielectric component with electrical connection comprises at least one dielectric layer (50, 55) comprising thermoplastic material, and the dielectric layer (50) or a stack of the dielectric layers (50, 55) has first and second main surfaces and a hole (505) extending between the first and second main surfaces. A first sprayed metal coating (501) comprises a first portion (503) deposited on the first main surface (502) adjacent to the hole (505) and a second portion (5014) which projects into the hole. A second sprayed metal coating (5013, 5513) comprises a third portion deposited on the second main surface (506, 552) adjacent to the hole (505) and a fourth portion (5015) which projects into the hole (505). The second portion (5014) overlaps the fourth portion (5015) to form a continuous conductive path between the first main surface and the second main surface. This provides a cheap, neat and thin connection through the dielectric layer or the stack of dielectric layers.
摘要翻译：为用于飞机（1）的防冰系统的层叠加热器垫（3）提供具有电连接的电介质部件。具有电连接的电介质部件包括至少一个包含热塑性材料的电介质层（50,55），并且电介质层（50）或电介质层（50,55）的叠层具有第一和第二主表面和孔 505），其在第一和第二主表面之间延伸。第一喷涂金属涂层（501）包括沉积在与孔（505）相邻的第一主表面（502）上的第一部分（503）和伸入孔中的第二部分（5014）。第二喷涂金属涂层（5013,5513）包括沉积在与孔（505）相邻的第二主表面（506,552）上的第三部分和突出到孔（505）中的第四部分（5015）。第二部分（5014）与第四部分（5015）重叠以在第一主表面和第二主表面之间形成连续的导电路径。这提供了通过电介质层或电介质层叠层的便宜，整齐和薄的连接。

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