1) solar cell array
太阳电池帆板
2) solar PV module
太阳电池板
1.
The thermal strain of the bonded layers in the element structure of solar PV module was tested.
试验测试了热循环过程中太阳电池板单元结构各被粘接层的热应变值,结合有限元MSC。
2.
The stress and strain distribution of elemental solar PV module structure after thermal cycles were analyzed using MSC.
Marc大型通用软件研究了热循环条件下太阳电池板单元结构热应力分布及演变规律。
3) solar panel
太阳电池板
1.
The effect of thermal property on the stress distribution in solar panel in thermal field is studied analytically.
文章利用解析法研究了材料热膨胀系数对温度场中太阳电池板最大应力的影响。
2.
Effect of elastic property on the stress of solar panel in thermal field is studied by analytical method.
解析法研究了弹性性能对温度场中太阳电池板最大应力的影响。
4) Solar array
太阳帆板
1.
This paper briefly reviews papers presented in the conference The papers cover 9 topics including on-orbit investigation, models and computer simulation,solar arrays and discharge phenomena,solar array test,interaction with charging environment,electric propulsion,interaction with plasma, internal charging,and material characterizations.
会议论文共涉及9个专题:飞行试验研究;模型和计算机仿真;太阳帆板和放电现象;太阳电池阵试验:与带电环境相互作用;电推进;等离子体相互作用;内带电;材料特性。
2.
The optimal control problem of the attitude of a spacecraft during the stretching process of its solar array is discussed in this paper.
讨论航天器太阳帆板伸展过程中航天器姿态运动的最优控制问题。
3.
The behavior of the satellites and their flexible solar arrays are imitated on the single axis gas bearing turntable (SAGBT) and flexible beam separately.
用单轴气浮台和挠性梁分别模拟卫星本体和太阳帆板。
5) solar panel substrate
太阳帆板
1.
A solar panel substrate planeness non contact system is presented, which employs optical triangulation method and bases on virtual precise benchmark.
介绍了一种采用斜光学三角形测量结构和基于虚拟精密测量基准的太阳帆板平面度无接触测量系统 。
6) Solar panel
太阳帆板
1.
Dynamics simulation of deployment for solar panels with hinge clearance
含铰间间隙太阳帆板展开动力学仿真
2.
The dynamics virtual prototype model of deployment of solar panels was built on ADAMS.
在ADAMS软件平台上建立了航天器太阳帆板展开过程动力学虚拟样机模型,研究了目前航天器太阳帆板典型的三种布局安装方式,分别为太阳帆板安装在航天器一侧同步展开;太阳帆板安装在航天器两侧同步展开;太阳帆板安装在四侧同步展开。
3.
The mathematic model for combined spacecraft’s solar panel obscuration was proposed based on geometry method, combined spacecraft self-body and solar panel as obscuring objects were taken into account.
太阳帆板的遮挡分析是航天器电源分系统方案设计的基础。
补充资料：多晶硅太阳电池
多晶硅太阳电池的性能基本与单晶硅太阳电池相同，目前国外多晶硅太阳电池大部分是10cm×10cm的方片。工业化生产的多晶硅太阳电池的典型特性参数如下：
isc=2950ma，voc=584mv，填充因子ff=0．72，转换效率η=12．4％(测试条件：am1．5，1000w／m2，25℃)。
多晶硅太阳电池的其它特性与单晶硅太阳电池类似，如温度特性、太阳电池性能随入射光强的变化等。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条