陶明慧
,
张星祥
,
张宇
,
任建岳
,
李新娥
液晶与显示
doi:10.3788/YJYXS20112601.0105
针对某航空相机的设计要求,提出了一种可行的多模式驱动时序设计方法.采用柯达公司的KAI-2093行间转移型面阵CCD传感器.结合它的结构特点和双通道数据传输的思想分析了传感器驱动时序关系,提出了3种驱动模式:binning、no-binning和TDI模式.以Ahera公司的FPGA芯片EP1C6Q240作为时序发生器并实现数据的缓存和拼接,从而实现了时序发生器与数据处理器的一体化设计.在QUARTUSII7.0开发环境下采用VHDL语言编程,通过Modelsim AE6.1b实现数据缓存器的仿真.实测结果表明,所设计的驱动时序满足KAI-2093的时序要求,binning模式下帧频可达60帧/s,120帧/s等,满足高速跟踪要求;no-binning模式下全帧输出帧频可达30帧/s;TDI模式下能保证CCD长时间工作而不影响成像质量,该没计方法提高了系统的集成度和抗干扰能力.
关键词:
航空相机
,
binning模式
,
TDI模式
,
数据缓存
,
数据拼接
,
FPGA
严东旭
,
刘天伟
,
龙重
,
白彬
,
张鹏程
,
黄河
,
郎定木
,
王晓红
,
朱建国
材料保护
采用单一的表面改性技术难以提高贫铀钛合金(Du-Ti)的耐蚀性能.采用等离子体浸没离子注入技术依次在Du-Ti合金表面注入N和Ti,再利用非平衡脉冲磁控溅射技术制备多层Ti/,TiN,研究了膜层的形貌、结构及耐蚀性能.结果表明:膜层厚约3μm,呈柱状结构,致密,但存在一些微缺陷,膜基结合紧密;膜层出现面心立方结构的TiN和密排六方的Ti,在DU-Ti合金界面形成了少量的UO2,没有铀的氮化物;膜层耐蚀性能较基体得到较大提高;微观缺陷是TiN层局部片状脱落的主要原因,外层TiN出现片状脱落后.注入层和内层Ti/TiN多层膜仍能有效保护基体.
关键词:
等离子体浸没离子注入
,
非平衡磁控溅射
,
复合膜
,
DU-Ti合金
,
电化学腐蚀
,
耐蚀性
李星星
,
杨科
,
张磊
,
刘强
工程热物理学报
本文提出了风力机翼型完整的性能参数体系和相应的评估方法,并以此评估了CAS-W1翼型与DU翼型的性能特征.对翼型性能的评估侧重于失速特性、非设计点特性和翼型气动性能的稳定性.评估结果表明,相对于DU翼型,CAS-W1翼型系列设计点性能和非设计点性能较好,但是失速特性和性能稳定性需要优化.
关键词:
风力机专用翼型
,
气动性能评价
,
失速特性
,
稳定性参数
欧阳艳东
,
黄翀
,
余云鹏
,
林舜辉
功能材料与器件学报
doi:10.3969/j.issn.1007-4252.2003.04.020
通过测量ITO玻璃及偏光片对各波段紫外光的光谱特性,分析比较一般偏光片和防紫外偏光片F1225DU的紫外透射光谱,从而说明新型偏光片的防紫外特性.F1225DU对紫外线有比较好的吸收,能挡住各种波长的紫外光,起防止紫外光破坏液晶显示器件的作用.
关键词:
偏光片
,
紫外光
,
液晶显示器
,
透射光谱
蒋兴元
,
魏季和
,
温丽娟
,
李波
上海金属
doi:10.3969/j.issn.1001-7208.2007.02.008
在几何相似比为1∶4的水模型上研究了150t RH装置内钢液的流动和混合特性及吹气管直径的影响.模型的吹气管内径分别为0.10、0.15和0.2 cm.所得结果表明,该装置的环流量计算式为:Qlp＝0.0291Qg0.323Du0.65Dd0.84(t/min),式中Qg-提升气体流量, Nl/min;Du和Dd-上升管和下降管内径,cm.在给定的Qg、Du和Dd下,吹气管直径din的变化对液体的流态没有显著影响,环流量则略有改变,在(0.40～0.80)cm的范围内,Qlp＝0.0304Qg0.322Du0.651Dd0.839din0.07.在Du和Dd均为53 cm、din为0.60 cm的情况下,该装置内钢液的最大("饱和")环流量约为135.1 t/min,相应的Qg为2500 Nl/min.钢包内钢液的混合效果随Qg的增大迅速提高.增大din使混合时间τm(s)略有缩短,对应于0.10,0.15和0.20 cm的孔径,τm与搅拌功率密度ε(W/t)的关系分别为:τm ∞ε-0.497,τm ∞ε-0.493和Tm∞ε-0.476.
关键词:
150t RH装置
,
水模型
,
流动特性
,
混合特性
,
物理模拟
,
吹气管直径
张磊
,
杨科
,
徐建中
,
张明明
,
白井艳
工程热物理学报
钝尾缘翼型气动特性受到尾涡脱落的影响,在翼型DU 91-W2-250的基础上对称加厚得到了新钝尾缘翼氆DU91-W2-250_6,利用密网格进行了非定常气动特性的数值研究.在各个攻角下钝尾缘翼型气动特性都具有周期性的特点,具体的波动特征如波动幅值及周期等则受脱落涡的大小、脱落位置及尾迹宽度的影响,而升力系数波峰、波谷则分别出现在顺时针涡及逆时针涡脱落的时刻.
关键词:
翼型
,
钝尾缘
,
非定常
Journal of Physics-Condensed Matter
This research purposes to investigate the atomic and electronic structures of the Al/TiC(001) interface with lattice misfit using the ab initio pseudopotential approach. A detailed analysis of the relaxed atomic structure reveals that the atoms over the initial unfavourable sites relax to the favourable sites along the lateral plane. The properties of the semicoherent interface can be taken as averages over the different coherent sites. In addition, the interface atoms in relatively favourable regions are dragged near to the interface, while those in unfavourable regions are pushed away from the interface. Therefore, a large war-ping near the interface is made perpendicular to the lateral plane. The calculated adhesions explain the different wetting results from the viewpoint of structural transition. The subsequent analysis of electronic properties demonstrates that adhesions dominate mainly via the strong Al-C covalent bond.
关键词:
first-principles;1st principles;adhesion;surfaces;misfit;1st-principles;wettability;al
X. Q. Yang
,
L. X. Huo
,
Y. F. Zhang and J. X. Yan (School of Material Science and Engineering
,
Tianjin University
,
Tianjin 300072
,
China)
金属学报(英文版)
The buckling formation and influence factors during welding thin - plated structures were investigated based on finite element methods, An engineering treatment method for prdicating the buckling distor- tion was proposed in here. It was used the equivalent applied thermal - load to simulate the welding residual stress,therefore the calculation of complex welding distoriton can be transformed into 3D elas- tic structural applied- load analyses, which can reduce the quantities of calculating works effectively. The validation of the method was verified by comparison of the numerical simulation and experimental results. The simulation of buckling distorition for side - walled structrues of paseenger train was per- formed and the calculation was in agreement with measuring results in general. It was shown that the main factors for producing the buckling were the intermittent fillet and ping the during welding the stiffened beams and columns to the panel.The existence of the free edge of panels would reduce the crit- ical buckling stress and enlarge the deflection obviously,but the continuous weld in closed frames didn' t degrade the buckling situation.
关键词:
welding buckling distortion
,
null
,
null
