北斗星斗柄指向考

该文通过文献考证，确认中国上古以北斗定时节的斗柄指向，有北斗七星和北斗九星两个标准，均作为初昏斗柄下指为冬至、上指为夏至的依据。北斗九星的斗柄指向，由第５、７、８、９诸星的连线、通过招摇、天锋，指向大火星，创建于４千年前的原始社会。北斗七星的斗柄指向，由第６、７两星连线的延长线，指向摄提和角、亢方向，形成于春秋、战国时期。     

锂渣高性能混凝土的性能与微观结构

锂渣是新疆特有的工业废渣,为了寻求其利用,采用锂渣来配制高性能混凝土。从力学、抗裂、收缩性能与微观结构等方面探究其增强、抗裂机理。试验结果表明:锂渣的最大掺量不宜超过45%;随着掺量的增加,收缩率增加不明显,但都较空白组要小;当掺量在20%~30%时,其力学、抗裂性能较好;锂渣掺入混凝土后,细化了混凝土的凝胶孔,提高其密实度;且在混凝土中形成了一定量的AFt,改善了其抗裂、力学性能。     

实时定量PCR检测B细胞恶性肿瘤中BCL11A基因的表达水平

目的:建立B细胞淋巴瘤/白血病BCL11A基因的定量检测方法,并分析其在B细胞恶性肿瘤中的表达水平。方法:利用实时定量RT-PCR分析B细胞淋巴瘤(18例)、B细胞性慢性淋巴细胞白血病(B-CLL,8例)、T细胞性急性淋巴细胞白血病(T-ALL,8例)和正常对照(15例)外周血单个核细胞(PBMC)中BCL11A基因的表达水平,以甘油醛-3-磷酸脱氢酶(GAPDH)基因作为内对照。结果:B-CLL组和B细胞淋巴瘤组患者PBMC中BCL11A表达水平均明显高于正常对照(P=0.000)和T-ALL组(P=0.000);T-ALL组和正常对照组BCL11A表达水平无显著差别(P=0.084);B-CLL组和B细胞淋巴瘤组BCL11A表达水平无显著差别(P=0.776)。在B细胞淋巴瘤不同的病例中,BCL11A表达水平有较大差异,其中最小值为0.04,最大值为9.70,中位值为1.00。结论:成功建立BCL11A基因的定量检测方法。     

关于不锈钢压力容器防污染及酸洗、钝化的问题

不锈钢材料在加工过程中会出现黑色、黄色的氧化皮,为了提高不锈钢压力容器的外观和耐蚀性,加工过程中的不锈钢压力容器零件等需进行防污染处理,完工后不锈钢压力容器需进行酸洗、钝化。     

从RNA走向DNA——细胞基因组的发生与形成

基因和基因组的发现为研究物种的进化提供了物质基础,物种进化的本质是细胞基冈组的进化,以此可完美地阐明达尔文的进化论,但细胞基因组本身是如何发生与形成的.目前尚未阐明,甚至有的科学家还认为生命最初是一堆有机分子偶然聚集在一起形成的.     

探讨大体积混凝土的施工技术

随着现代建筑技术的不断发展,大体积混凝土的应用越来越广泛.大体积混凝土逐渐成为构成大型设施或构筑物主体的重要组成部分.笔者结合实践经验,对建筑工程中大体积混凝土的施工技术进行探讨.     

Anthropogenic influence has increased climate extreme occurrence over China

There is overwhelming evidence that anthropogenic activity has exerted a great influence on climate extremes, especially on heat events at continental to global...     

NGDcrm:a numeric graph dependency-based conflict resolution method for knowledge graph

Knowledge graph(KG)conflict resolution is to solve knowledge conflicts problem in the con-struction of KG.Aiming at the problem of KG conflict resolution,a KG c...     

Magnetic circuit optimization and experimental study of new internally excited automatic balancing

Mass imbalance-induced vibration affects the rotating machinery very large,especially the high-speed types.Off-line balancing techniques have been widely develo...     

Robust Chattering-Free Finite Time Attitude Tracking Control with Input Saturation

This paper addresses the attitude tracking control problem of a rigid spacecraft in the presence of the modeling uncertainty, external disturbance, and saturated control input by designing two robust attitude tracking controllers. The basic controller is formulated using an integral sliding mode surface which is continuous and provides an asymptotic convergence rate for the closed-loop system. In this case, only the external disturbance with the prior information is considered. Then, to provide a finite time convergence rate and further improve the robustness of the control system under the unknown system uncertainty containing both the modeling uncertainty and external disturbance,a novel integral terminal sliding mode surface(ITSMS) is designed and associated with the continuous adaptive control method. Besides, a command filter is utilized to deal with the immeasurability problem within the proposed ITSMS and an auxiliary system to counteract the input saturation problem. Digital simulations are presented to verify the effectiveness of the proposed controllers.