CDM in the Kyoto Negotiations:

The Clean Development Mechanism (CDM) under the Kyoto Protocol to the UN Framework Convention on Climate Change (UNFCCC) has its origins in the decade of UNFCCC negotiations. ‘Joint implementation’ and ‘activities implemented jointly pilot’ opened the door for the project-based mechanisms between developed and developing countries. The US proposal of the Joint Implementation in the Kyoto Protocol negotiations was almost identical with CDM approved in Kyoto; however, a detour around the Clean Development Fund (CDF) concept raised by Brazil in the negotiations catalyzed the mutual understanding on the win-win nature of the concept of joint implementation.CDM has been played an important role to bridge the developed and developing countries in its development process initiated as the joint implementation in the UNFCCC, and can lead to the cooperative future in the implementation stage starting from the year 2003, including the development of future commitments beyond 2013. This revised version was published online in August 2006 with corrections to the Cover Date.     

某型飞机外翼5—8肋损伤原因分析及修复探讨

目的 分析某型飞机外翼5—8肋油箱区结构不同程度损伤的原因,制定修复方案。方法采用受载分析、有限元仿真计算、静力试验数据分析等强度计算方法分析损伤产生的原因,采用扫描电子显微镜和光学显微镜对磨痕形貌进行观测等失效分析,对损伤结构件开展失效模式分析,根据损伤原因及失效模式制定科学简便的修复方案,同时对损伤长桁采取的修补措施进行强度校核。结果 通过对外翼油箱充压破坏理论分析、有限元仿真计算、静力试验数据反推,并结合飞机实际损伤情况,得出油箱破坏理论分析危险薄弱部位与真实破坏情况一致的结论。有限元仿真计算最危险结构部位与实际结构首先发生破坏部位吻合,可作为深入制定修复方案及推测实际加载压力的依据。通过静力试验数据反推、结构实际损伤及有限元仿真计算结论得出,外翼5—8肋结构出现损伤时油箱施加压力约0.5 MPa,针对损伤制定了更换外翼油箱内部第5—8肋损伤结构和贴补加强损伤长桁的修理方案,经结构强度校核,满足设计要求。结论 分析认为外翼5—8肋油箱区结构损伤原因为油箱压力超过设计值导致结构过载断裂,采用贴补加强修理损伤长桁和更换第5—8肋损伤结构的修复方案能够满足强度设计要求,可指导同类飞机类似结构损伤故障的原因分析和修理,提醒同类飞机维修人员在飞机维护时应关注外翼油箱压力超压问题。     

A Variance Estimator for Constrained Estimates of Change in Relative Categorical Frequencies

Consistent estimators of change and state becomes an issue when sample data come from a mix of permanent and temporary observation units. A joint maximum likelihood estimator of state and change creates estimates of state that depend on antecedent viz. posterior survey results and may differ from estimates of state derived from a single-date analysis of the sample data. A constrained estimator of change in relative categorical frequencies that eliminates this potential inconsistency is proposed and a model based estimator of their sampling variance is developed. The performance of the constrained estimator is quantified against six criteria and a joint maximum likelihood estimator in simulated sampling from 15 populations with three combinations of permanent and temporary samples, four to six categorical class attributes, and constant size between sampling dates. Bias of the constrained estimators was negligible but larger than for joint maximum likelihood estimators. Mean absolute deviations and variances of constrained estimators were generally at par with the joint estimators. Constrained estimators of root mean square errors and achieved coverage of nominal confidence intervals of constrained estimators were occasionally better. A generalized variance function for the constrained estimates of change is provided as a computational shortcut.     

梯齿形桥梁伸缩缝U形弯曲件的成形技术

此文介绍一种新型桥梁伸缩缝关键零件U形弯曲件的成形技术.通过对该零件的变形分析和采用合理的工艺措施,使得这一成形难度较大的弯曲件一次压制获得成功.     

机车检修污水处理回用设施实例分析

机车清洗污水经撇油、酸碱中和、气浮、过滤、活性碳吸附等工艺流程的处理后,进行全封闭循环,再用于清洗机车,合理选择污水处理工艺流程是确保处理后的污水能否经济、合理回用的关键.     

电热管焊接接头挤压裂纹的分析

针对电热管焊接接头挤压产生的裂纹 ,通过采用金相显微镜观察其金相组织并用直读光谱对原材料成分进行化学成分分析 ,排除了成分、焊接工艺规范等的影响。经过对挤压过程分析 ,发现应力集中点是产生裂纹的主要原因 ,并提出了改进的方法     

水深变化对波高与周期联合概率密度分布影响的分析

本文研究了水深的变化以波高与周期联合概率密度分布造成影响。本文将２３６组实测数据按水深因子Ｈ的大小进行了分组，分别对其进行了谱分析和统计分析，得到了各组数据的联合分布图。利用数值模拟的方法扩大水深因子的变化幅度，得到了模拟联合分布图。研究发现，水深因子的改变不会对联合分布构成大的影响，因此得现一般水的波高与周期联合概率密度分布模式适用于浅海的结论。     

城乡接合部居民楼火灾风险评价及防控对策研究

为了准确探究城乡接合部居民楼火灾事故致因机理,预防与控制城乡接合部日常生产与生活过程中引发火灾事故的有效途径,建立信息面更全、实际性更强的火灾风险评估模型是目前行之有效的手段。基于湖南省某地发生火灾事故的实际情况,根据事故树分析法,以城乡接合部居民楼火灾事故为顶事件构建事故树,计算得到事故树的最小割集、最小径集和结构重要度,研究城乡接合部居民楼火灾事故的发生模式、致因因素及影响程度,为改善城乡接合部居民楼火灾安全提供重要的理论依据,并提出相应的防控措施及对策。     

航空装备外场级平均修复时间评估研究

目的探索航空装备部队使用保障阶段维修性指标评估的实施方法。方法构建航空装备外场级平均修复时间评估指标体系,包括评估条件界定、统计准则确定、数据处理方法、评估流程、使用表格等,并结合具体机型进行评价应用。结果该机型飞机整机的累计修复时间为138.5 h,平均修复时间Mct=2.17 h,满足不大于3 h指标要求。结论评估方法系统科学,可为各类装备开展相关维修性评估工作提供方法支持和工程借鉴。     

某型机襟翼舱下壁板蒙皮腐蚀原因分析与修理措施研究

目的研究某型机襟翼舱下壁板蒙皮产生腐蚀损伤的原因,分析腐蚀危害性,制定腐蚀修补方案,提出后续腐蚀防护与控制的建议措施。方法首先现场仔细检查结构的腐蚀状况,然后分别从结构设计与选材、服役环境分析、腐蚀产物分析3个方面研究结构腐蚀产生的成因,并且针对性地制定腐蚀部位的补强修理方案。结果在襟翼舱局部高温湿热环境下形成的内部冷凝水,夹杂大气环境中的Cl~-污染侵袭,导致壁板蒙皮材料LY12铝合金产生了晶间剥落腐蚀。结论老龄飞机机体结构腐蚀成因复杂多样,准确界定腐蚀原因是制定腐蚀防护与控制措施的关键。