公开(公告)号：US06323089B1

公开(公告)日：2001-11-27

申请号：US09309242

申请日：1999-05-10

申请人： Dah-Bin Kao ,  Loc B. Hoang ,  Albert T. Wu ,  Tung-Yi Chan

发明人： Dah-Bin Kao ,  Loc B. Hoang ,  Albert T. Wu ,  Tung-Yi Chan

IPC分类号： H01L218247

CPC分类号： H01L27/11521 ,  G11C16/0425 ,  H01L27/115 ,  H01L29/42324

摘要： A semiconductor memory array and methods therefor is provided herein comprising a substrate; a plurality of memory cell field effect transistors formed on said substrate and being arranged thereon into rows and columns of transistors, each transistor includes a channel region interposed between drain and source regions, and overlaid by a control gate region; a plurality of first diffused elongated regions formed within said substrate that electrically connect in common the drain regions of transistors in respective columns; a plurality of second diffused elongated region formed within said substrate that electrically connect in common the source regions of transistors in respective columns; and a plurality of elongated conductive line formed over said substrate that electrically connect in common the control gate regions of transistors in respective rows.

摘要翻译： 本文提供了一种半导体存储器阵列及其方法，包括：衬底; 多个存储单元场效应晶体管，形成在所述基板上并被布置在晶体管的行和列中，每个晶体管包括介于漏极和源极区之间并由控制栅极区重叠的沟道区; 形成在所述基板内的多个第一扩散细长区域，其共同地将各个晶体管的漏极区域电连接; 形成在所述衬底内的多个第二扩散细长区域，其共同地将各个晶体管的源极区域电连接; 以及形成在所述衬底上的多个细长导电线，其共同地电连接相应行中的晶体管的控制栅极区域。

公开(公告)号：US6102339A

公开(公告)日：2000-08-15

申请号：US62594

申请日：1998-04-17

申请人： Albert T. Wu ,  Linchih O. Liu

发明人： Albert T. Wu ,  Linchih O. Liu

IPC分类号： B64G1/44 ,  B64G1/50 ,  B64G1/58

CPC分类号： B64G1/503 ,  B64G1/44 ,  B64G1/58

摘要： A sun-synchronous sun ray blocking device for use in a spacecraft having a directionally controlled main body, such as a low inclination angle earth (as well as other planets) orbit spacecraft, that is, a three axis stabilized spacecraft having north, south, east, west, earth and anti-earth panels defining a spacecraft main body. The north and south panels, on which the spacecraft equipment with high heat dissipation is usually mounted, have their planar normal axes relatively parallel to the spinning axis of the earth. Normal to each of the north and south panel, a solar panel loaded with solar cells is extended and is directly rotating about the same axis. The solar panels are controlled in such a way that the solar cells side of the panels always faces the sun. Each solar panel's blocking device is situated between the solar panel and sun, attached to its solar panel and rotated therewith, to block the sunlight from the north and south panels, providing a stable, benign thermal environment for those panels.

摘要翻译： 一种用于具有定向控制主体的太阳同步太阳光线阻挡装置，例如低倾角地球（以及其它行星）轨道航天器，即具有北，南， 东，西，土和反对面板，定义了航天器主体。 通常安装有高散热的航天器设备的北面和南面的平面法线与地球的旋转轴线相对平行。 正常到北面和南面的每一个，装有太阳能电池的太阳能电池板被延伸并且绕同一个轴线直接旋转。 太阳能电池板的控制方式使得面板的太阳能电池板面总是面向太阳。 每个太阳能电池板的阻挡装置位于太阳能电池板和太阳之间，连接到其太阳能电池板并与其一起旋转，以阻挡来自北面和南面的太阳光，为这些面板提供稳定的良性热环境。