JJG 1002-2005旋转黏度计计量检定规程存在的问题探讨

对JJG 1002-2005旋转黏度计计量检定规程存在的问题进行探讨,指出该规程不适合血液黏度计的检定,应重新制订血液黏度计计量检定规程或计量校准规范,以适应医学临床需要.     

化学分析方法验证和确认的应用研究

分析方法的验证/确认是实验室引进新方法时必做的工作,也是实验室技术工作的重点和难点之一。对实验室采用分析方法的验证和确认工作进行归纳总结,详述了分析方法选择性、测量范围、线性范围、检出限和定量限、精密度、准确度的验证/确认方法及结果判定方式。适用于实验室引进的标准方法(包括标准变更)和非标准方法(实验室设计/制定的方法、超出预定范围使用的标准方法、扩充和修改过的标准方法)的验证和确认。     

智能石墨消解–ICP–MS法测定空气PM2.5中的Pb和Cd

建立电感耦合等离子体质谱(ICP–MS)测定空气PM2.5中的Pb和Cd元素的分析方法。采用连续β射线–DHS PM2.5大气颗粒物浓度监测仪采集空气中的PM2.5,以智能石墨消解PM2.5滤膜样品,ICP–MS测定其中的Pb和Cd元素含量。在优化的仪器条件下,元素Pb和Cd标准曲线的线性相关系数均为0.999 9,检出限分别为0.018,0.52ng/m3,满足HJ 657–2013的要求。Pb和Cd的加标回收率分别为95.8%~101.4%,99.3%~104.9%,测定结果的相对标准偏差分别为4.20%和2.38%(n=6)。对滤膜标准样品进行了测定,测定结果与标准值一致。该方法测定结果准确、可靠,可用于测定空气PM2.5中的Pb和Cd。     

基于公钥基础设施的Hadoop安全机制设计

为了满足运载火箭遥测系统集成验证的测试需求,同时提升测试设备的通用性,降低测试设备的研制成本,本文采用面向信号的设计思想,设计了一种简洁高效的遥测系统自动化测试平台。该测试平台基于PXI总线开发,通过采取多路复用开关与输入输出模块相结合的设计思路,可实现多参数的巡检测试及同时测试,使测试平台具有较好的通用性和灵活性,在硬件设备不做更改的前提下可适用于多型运载火箭的测试需求,同时研制成本大幅降低;通过接收解析箭上遥测数据,测试过程无需人工干预,实现了自动化测试与自动化判读。通过试验验证,该测试平台工作稳定,能较好的满足多型运载火箭遥测系统集成验证测试需求,同时该平台的设计方法为同类测试系统的设计提供了一种思路。     

内部审核在计量体系中的作用

介绍内部审核制度在计量测试工作中的目的和作用，提出了内部审核工作应注意的事项，如内部审核工作计划的完整性，内部审核工作的有效性，管理者工作内容的全面性，以及后续工作的完善性。     

核弹头惰层厚度的反解方法

高分辨γ探测技术是一种可靠的核弹头核查技术.通过模拟计算和实验标定的方法，研究特定核弹头模型出壳γ射线强度与吸收材料厚度的关系，提出了一种简便的反解核弹头惰层厚度的方法，并讨论了该方法的应用条件.     

The dry-packing of columns in liquid chromatography

This contribution comprises two parts, the one covering some variables in the dry-packing of columns for liquid chromatography, the other the use of an automatic dry-packer in liquid chromatography. A high-pressure stainless steel column was dry-packed using a 20-44 μm size, irrregularly shaped, silica gel support. It was found that, when support was added in discrete amounts, lateral tapping produced a column of higher efficiency (HETP = 0.69 mm) than was the case for vertical tapping (HETP = 1.37 mm). Simultaneous vertical and lateral tapping produced an intermediate result. Bulk filling of the column followed by tapping was inferior to adding support in discrete amounts. An apparatus constructed to perform the vertical and lateral tapping operations automatically confirmed the above conclusions. It was concluded that commercially available dry-packing apparatus do not offer the best action for packing an efficient column since they involve predominantly vertical tapping.     

瓦斯煤尘爆炸火焰光谱的实验研究

本文概述了瓦斯煤尘爆炸火焰光谱实验研究的重要性,我们在弱爆炸和探测器小视场角的条件下,利用自己研制的多波道仪,在一端开口的Φ200cm×2900cm大型管道里,得到了CH4、空气和煤尘的混合物在不同状态下,特征波长λ等于0.8875、1.000、1.505、2.801和4.346微米(μ)的绝对辐射强度及其有关的变化规律,对结果进行了分析讨论,并与国外实验结果进行了对比,根据测量λ=4.346μ绝对辐射强度和我们选择的黑体辐射模型,获得了爆炸火焰的温度,该项研究不仅在工业中具有重要意义,而且对燃烧和化学动力学的研究也具有参考价值。     

Reduced Functions, Gradients and Hessians from Fixed-Point Iterations for State Equations

In design optimization and parameter identification, the objective, or response function(s) are typically linked to the actually independent variables through equality constraints, which we will refer to as state equations. Our key assumption is that it is impossible to form and factor the corresponding constraint Jacobian, but one has instead some fixed-point algorithm for computing a feasible state, given any reasonable value of the independent variables. Assuming that this iteration is eventually contractive, we will show how reduced gradients (Jacobians) and Hessians (in other words, the total derivatives) of the response(s) with respect to the independent variables can be obtained via algorithmic, or automatic, differentiation (AD). In our approach the actual application of the so-called reverse, or adjoint differentiation mode is kept local to each iteration step. Consequently, the memory requirement is typically not unduly enlarged. The resulting approximating Lagrange multipliers are used to compute estimates of the reduced function values that can be shown to converge twice as fast as the underlying state space iteration. By a combination with the forward mode of AD, one can also obtain extra-accurate directional derivatives of the reduced functions as well as feasible state space directions and the corresponding reduced or projected Hessians of the Lagrangian. Our approach is verified by test calculations on an aircraft wing with two responses, namely, the lift and drag coefficient, and two variables, namely, the angle of attack and the Mach number. The state is a 2-dimensional flow field defined as solution of the discretized Euler equation under transonic conditions.