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1. 发明授权

US6027076A Method for powering a spacecraft with extended-life battery operation 失效
标题翻译：为延长使用寿命的电池操作的航天器供电的方法
公开(公告)号：US6027076A
公开(公告)日：2000-02-22
申请号：US112484
申请日：1998-07-09
申请人： Stanley J. Krause
发明人： Stanley J. Krause
IPC分类号： B64G1/42 , B64G1/44 , H01M10/44 , H02J7/00 , H02J7/35 , B64G1/10
CPC分类号： H02J7/35 , B64G1/425 , B64G1/428 , H02J7/0024 , B64G1/443
摘要： A spacecraft, such as a satellite in geosynchronous orbit, is powered using at least two independently controllable batteries, such as lithium ion batteries, operably connected to the power-consuming components of the spacecraft. Each battery is operable in a higher-temperature range and inactivated in a lower-temperature range. The first battery and the second battery are operated in the higher-temperature range during a first period of time. The first battery is thereafter operated in the higher-temperature range during a second period of time, with the second battery being non-operational and in the lower-temperature range during the second period of time. The first battery and the second battery are thereafter operated in the higher-temperature range during a third period of time. The second battery is thereafter operated in the higher-temperature range during a fourth period of time, with the first battery being non-operational and in the lower-temperature range during the fourth period of time. The operable battery or batteries may be operated through a partial charging/discharging cycle. This alternating operation prolongs the lifetimes of the batteries.
摘要翻译：诸如地球同步轨道中的卫星的航天器使用至少两个可操作地连接到航天器的功率消耗部件的独立可控的电池（例如锂离子电池）供电。每个电池可在较高温度范围内工作，并在较低温度范围内灭活。第一电池和第二电池在第一时间段内在较高温度范围内操作。此后，第一电池在第二时间段内在较高温度范围内操作，第二电池在第二时间段内不可操作，而在较低温度范围内。此后，第一电池和第二电池在第三时间段内在较高温度范围内操作。此后，第二电池在第四时间段内在较高温度范围内操作，第一电池不工作，在第四时间段内处于较低温度范围。可操作的电池或电池可以通过部分充电/放电循环来操作。这种交替操作可延长电池的使用寿命。

2. 发明授权

US5614033A Rigid solar panel with discrete lattice and carrier structures bonded together 失效
标题翻译：具有离散晶格和载体结构的刚性太阳能电池板结合在一起
公开(公告)号：US5614033A
公开(公告)日：1997-03-25
申请号：US512727
申请日：1995-08-08
申请人： Stephen A. Robinson , Stanley J. Krause
发明人： Stephen A. Robinson , Stanley J. Krause
IPC分类号： B64G1/50 , H01L31/048 , H01L31/052
CPC分类号： H01L31/048 , B64G1/50 , H01L31/052 , H02S20/00 , H02S20/30 , H02S40/42 , Y02E10/50 , Y10T428/236
摘要： Discrete carrier and lattice structures are bonded together to form a lightweight rigid solar panel. The carrier includes a pair of electrically inert face sheets bonded on opposite sides of a thin thermoconductive honeycomb core. The face sheets provide an electrically inert surface for receiving a solar cell array and the honeycomb core forms a heat sink for conducting heat away from the solar cell array. The lattice includes a pair of patterned face sheets having a high elastic modulus bonded on opposite sides of a lattice base. The patterned face sheets provide axial stiffness and the lattice base separates them to provide bending stiffness. By splitting the solar panel into discrete carrier and lattice components, the present invention reduces the weight of existing solar panels by approximately 40% and increases power efficiency by approximately 10%.
摘要翻译：离散载体和晶格结构结合在一起形成轻量级的刚性太阳能电池板。载体包括结合在薄导热蜂窝芯的相对侧上的一对电惰性面片。面板提供用于接收太阳能电池阵列的电惰性表面，并且蜂窝芯形成用于将热量从太阳能电池阵列传导出来的散热器。格子包括一对具有高的弹性模量的图案化的面片，其结合在晶格基底的相对两侧。图案化的面板提供轴向刚度，并且格子基座将它们分开以提供弯曲刚度。通过将太阳能电池板分成离散的载体和晶格部件，本发明将现有太阳能电池板的重量减少大约40％，并将电力效率提高约10％。

3. 发明授权

US6010800A Method and apparatus for transferring heat generated by a battery 失效
标题翻译：用于传送由电池产生的热量的方法和装置
公开(公告)号：US6010800A
公开(公告)日：2000-01-04
申请号：US98849
申请日：1998-06-17
申请人： Steven J. Stadnick , Stanley J. Krause
发明人： Steven J. Stadnick , Stanley J. Krause
IPC分类号： H01M2/10 , H01M2/30 , H01M10/50
CPC分类号： H01M10/613 , H01M10/653 , H01M10/6551 , H01M10/6552 , H01M10/6553 , H01M2/10 , H01M2/30
摘要： An apparatus and method for controlling the temperature of a battery used in a spacecraft or an electric vehicle are disclosed. The apparatus includes a thermal conductor, such as a thermally-conductive heat pipe or forced-fluid cooling loop, that is in thermal contact with thermally-conductive cell terminals of the battery, and a heat sink, such as a radiator. The inventive method includes operating the battery to generate and conduct heat to the thermally-conductive battery cell terminals. The generated heat is passed via conduction from the terminals to the thermal conductor. The heat is conducted through the thermal conductor to a heat sink which may be remotely located with respect to the battery. Preferably, the thermal conductor remains electrically insulated from the battery cell terminals and the heat sink.
摘要翻译：公开了一种用于控制在航天器或电动车辆中使用的电池的温度的装置和方法。该装置包括与电池的导热单元端子热接触的热导体，例如导热热管或强制流体冷却回路，以及散热器等散热器。本发明的方法包括操作电池以对导热电池单元端子产生和传导热量。所产生的热量通过导体从端子传递到热导体。热量通过热导体传导到散热器，散热器可以相对于电池远程定位。优选地，导热体与电池单元端子和散热器保持电绝缘。

4. 发明授权

US4854975A Solar cell with integrated interconnect device and process for fabrication thereof 失效
公开(公告)号：US4854975A
公开(公告)日：1989-08-08
申请号：US881752
申请日：1986-07-03
申请人： Stanley J. Krause
发明人： Stanley J. Krause
IPC分类号： H01L31/0224 , H01L31/048 , H01L31/05 , H01L31/18
CPC分类号： H01L31/184 , B64G1/443 , H01L31/022425 , H01L31/048 , H01L31/0508 , Y02E10/544
摘要： A solar cell assembly wherein a solar cell is provided with electrical layer contacts for both the p-type semiconductor layer and the n-type semiconductor layer which are exposed on a top side of the solar cell, so that electrical contact to both layers can be made from the top side of the cell, and a glass cover overlying the solar cell includes a pair of U-shaped electrical cell contacts extending over the sides of the glass cover so that one leg of each U makes contact with one of the layer contacts and the other leg is accessible from the top of the cover glass. External electrical contact to the cell is easily and conveniently made, and cells can be electrically joined to adjacent cells in an array using a connector bar. The glass cover also supports the solar cell so that excess material on the substrate of the solar cell can be etched away to reduce the weight of the solar cell assembly.

5. 发明授权

US4849028A Solar cell with integrated interconnect device and process for fabrication thereof 失效
标题翻译：具有集成互连装置的太阳能电池及其制造方法
公开(公告)号：US4849028A
公开(公告)日：1989-07-18
申请号：US259982
申请日：1988-10-11
申请人： Stanley J. Krause
发明人： Stanley J. Krause
IPC分类号： H01L31/0224 , H01L31/048 , H01L31/05 , H01L31/18
CPC分类号： H01L31/184 , B64G1/443 , H01L31/02008 , H01L31/022425 , H01L31/048 , H01L31/0508 , Y02E10/544 , Y02P70/521
摘要： A solar cell assembly wherein a solar cell is provided with electrical layer contacts for both the p-type semiconductor layer and the n-type semiconductor layer which are exposed on a top side of the solar cell, so that electrical contact to both layers can be made from the top side of the cell, and a glass cover overlying the solar cell includes a pair of U-shaped electrical cell contacts extending over the sides of the glass cover so that one leg of each U makes contact with one of the layer contacts and the other leg is accessible from the top of the cover glass. External electrical contact to the cell is easily and conveniently made, and cells can be electrically joined to adjacent cells in an array using a connector bar. The glass cover also supports the solar cell so that excess material on the substrate of the solar cell can be etched away to reduce the weight of the solar cell assembly.
摘要翻译：一种太阳能电池组件，其中太阳能电池设置有露出在太阳能电池的顶侧的p型半导体层和n型半导体层的电层触点，使得与两层的电接触可以是由电池的顶侧制成，并且覆盖太阳能电池的玻璃盖包括一对延伸在玻璃盖的侧面上的U形电池触点，使得每个U的一个支腿与层触点之一接触另一条腿可以从盖玻璃的顶部进入。容易且方便地制造与电池的外部电接触，并且可以使用连接器条将电池以阵列电连接到相邻电池。玻璃盖还支撑太阳能电池，从而可以蚀刻掉太阳能电池基板上的多余材料，以减少太阳能电池组件的重量。

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