飞机环控系统典型故障分析

环控系统解决了飞机座舱的供气、调温和增压问题,座舱的压力制度按3个阶段进行。通过典型的飞机环控系统故障,对座舱压力调节机理进行了分析,介绍了座舱压力调节过程,分析了导致飞行员耳膜疼痛、座舱压力持续下降的原因,提出了预防故障发生的建议。     

老龄飞机结构的腐蚀问题与对策

列举了某型老龄飞机腐蚀故障案例,阐明了老龄飞机结构腐蚀的共性问题及特点,从使用寿命期指标体系、结构抗腐蚀品质、服役环境、使用维护与腐蚀修理等方面较系统地分析了老龄飞机结构腐蚀的主要原因和影响因素。重点阐述了老龄飞机结构腐蚀防护对策与措施,主要包括结构腐蚀检查评估、涂层体系改进与结构密封防水改进、外场使用维护中腐蚀预防与控制措施。     

北京2015年大气细颗粒物的空间分布特征及变化规律

近年来,随着雾霾事件的频发,人们逐渐提高了对雾霾的关注度,PM_2.5作为其首要污染物对大气能见度及人体健康造成了严重影响.因此,本文利用2015年北京12个环境监测站点的PM_2.5、PM₁₀、NO₂、SO₂、CO和O₃的浓度数据和气象数据,综合研究了北京2015年大气细颗粒物的空间变化特征及分布规律.同时,利用空间差异率（COD）统计方法评估了不同地区细颗粒物浓度的差异程度,并结合2015年2次特殊事件（春节和阅兵）,对大气污染特征及其与排放源控制的关系进行了深入对比分析.结果发现,重污染天气集中发生在秋冬季,且污染程度高、持续时间长.城区PM_2.5浓度比郊区高约12 μg·m^-3.东城区与对照区差异最大,COD值为0.24;东城区与西城区差异最小,COD值为0.05.春、夏、秋季颗粒物PM_2.5、PM₁₀浓度日变化较为平稳,在中午有所升高,冬季颗粒物质量浓度明显呈现出夜间高于日间的污染模式.近3年PM_2.5与PM₁₀保持显著的相关性,但PM_2.5/PM₁₀比值呈降低趋势.阅兵期间采取的空气质量管控措施和气象要素共同作用导致PM_2.5浓度下降约72%,市中心的首要污染物为NO₂,郊区首要污染物为O₃和PM₁₀.春节期间烟花燃放对PM_2.5的瞬时贡献量很大,对比春节假期和非假期2个阶段的大气污染特征发现,人口和机动车减少及餐馆暂停营业并没有使北京局地空气质量得到明显改善.该研究结果提示在进行PM_2.5控制的同时也要对O₃浓度有所关注,同时也进一步支撑了北京空气质量改善需要京津冀协同控制这一重要结论.     

上海浦东国际机场飞机尾气排放对机场附近空气质量的影响

统计2012年10月和11月浦东机场飞机机型和航班架次，根据各类飞机起降的污染物排放设计工作参数，估算出2012年浦东机场飞机起降时排放的NO2、SO2、CO和HC的估算值。利用浦东新区13个空气监测子站二氧化氮和二氧化硫数据绘制等值线图。结果显示，机场所在的江镇点位和祝桥点位二氧化氮浓度变化受飞机影响很大，而飞机排放的二氧化硫对两个点位的影响可以忽略不计。建议采用改进飞机滑行路线、探讨征收飞机碳排放税等措施减少飞机尾气排放对空气质量的影响。     

Humanitarian action and military intervention: temptations and possibilities

Although the war in Liberia in July 2003 claimed hundreds of lives, the international community was reluctant to intervene. In this article, the author debates the question: does international military intervention equal protection of populations? The role of humanitarian organisations in military intervention is considered. Aid organisations cannot call for deployment of a protection force without renouncing their autonomy or appealing to references outside their own practices. Such organisations provide victims with vital assistance and contribute to ensuring that their fate becomes a stake in political debate by exposing the violence that engulfs them, without substituting their own voices for those of the victims. The political content of humanitarian action is also outlined and military intervention in the context of genocide is discussed. The author concludes that the latter is one of the rare situations in which humanitarian actors can consider calling for an armed intervention without renouncing their own logic.     

某飞机维修公司个人听力防护用品使用情况调查分析

为了解听力防护用品使用过程中的问题,提高我国噪声暴露工人听力防护用品的使用率和有效率,选择噪声危害较大的某飞机维修公司的员工,进行听力防护用品使用情况的问卷调查。结果显示:该公司为员工提供耳塞和耳罩两种听力防护用品;员工的听力保护意识、使用情况较好,使用率达95%,但对听力防护用品相关知识的了解不够全面;能够在工作中一直坚持使用的工人较少,仅占11%,影响工人工作时间使用听力防护用品时间长短的因素主要是其舒适性。调查分析提示:在未来听力防护用品的生产过程中,需要进一步加强和改善舒适性的技术;政府、企业和个人3方面共同参与,降低职业性噪声暴露对工人听力的损伤。     

现役民机客舱热舒适评价

采用修正热舒适评价值(Corrected Predicted Mean Vote,CPMV)模型,针对实测的国内及国际航线数据进行了客舱环境的热舒适评价.结果表明,当客舱内压力满足适航标准要求范围、相对湿度明显低于舒适性要求时,低压和低相对湿度均能导致热舒适评价值(Predieted Mean Vote,PMV)的正偏移,偏移量为0.3～0.4,即低气压和低湿会使乘客感觉更温暖,但这2个参数对乘客热舒适的影响有限.短途航班热舒适性不理想,部分航班出现过热或过冷现象.     

飞机撞击下核电厂安全壳载荷曲线相关问题研究

针对大型商用飞机对核电厂反应堆安全壳恶意撞击的安全评估需求,综述了国外确定飞机撞击安全壳载荷曲线的基础理论、试验测试技术和数值模拟方法.首先,从理论上对飞机撞击安全壳的载荷特性和Riera撞击模型进行分析,给出了Riera模型的基本假设、模型各项物理意义及模型的求解方法,明确了靶体碰撞表面的冲击载荷(力)由静载项和动载项组成;其次,分析总结了确定Riera模型中压损载荷参数的试验方法和真实飞机撞击载荷测量的试验技术和实施方法,指出大型商用飞机对核电厂反应堆安全壳恶意撞击属"软冲击"范畴,撞击载荷可用Riera模型计算得到;再者,在数值模拟方面,总结了采用有限元技术进行飞机撞击载荷计算和安全评估的数值模拟方法及其发展趋势;最后,在分析国内开展飞机撞击载荷研究面临问题的基础上,指出从理论上建立飞机撞击载荷-时间曲线计算模型及方法,并通过试验和数值模拟验证是国内确定大型商用飞机撞击安全壳结构载荷曲线比较可行的技术路线.     

Exergetic Sustainability Indicators as a Tool in Commercial Aircraft: A Case Study for a Turbofan Engine

This paper focuses on the exergetic sustainability indicators of a medium-range commercial aircraft engine for constant reference environment and ground running conditions. First, a detailed exergy analysis of turbofan engine have been performed based on engine test cell parameters. Starting from the sustainability considerations and the second law of the thermodynamics, the paper presents six exergy-based sustainability indicators. The indicators of the turbofan engine developed here in conjunction with exergetic analysis and sustainable development are exergy efficiency, waste exergy ratio, exergy destruction factor, recoverable exergy rate, environmental effect factor, and exergetic sustainability index. The investigated sustainable indicators have been calculated by using exergy analysis outputs for aircraft ground running condition. Results from this study show that values of exergy efficiency, waste exergy ratio, exergy destruction factor, recoverable exergy rate, environmental effect factor, and exergetic sustainability index of investigated turbofan engine are found to be 0.315, 0.685, 0.408, 0, 2.174, and 0.460, respectively. These parameters are expected to quantify how the turbofan engine and aircraft become more environmentally benign and sustainable.     

Integrated disaster relief logistics: a stepping stone towards viable civil–military networks?

The twenty‐first century has seen a significant rise in all forms of disasters and this has resulted in military and humanitarian organisations becoming more frequently engaged in the provision of support to those affected. Achieving an efficient and effective logistic preparation and response is one of the key elements in mitigating the impact of such events, but the establishment of mechanisms to deliver an appropriately integrated civil–military approach remains elusive. Not least because of the high percentage of assistance budgets spent on logistics, this area is considered to represent fertile ground for developing improved processes and understanding. In practice, the demands placed on civilian and military logisticians are broadly similar, as is the solution space. Speaking a common language and using common concepts, it is argued, therefore, that the logistic profession should be in the vanguard of the development of an improved civil–military interface.