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1421.全球商用飞机零部件制造人批准市场报告(2015-2019年)
[铁路、船舶、航空航天和其他运输设备制造业] [2015-09-06]
Aircraft PMA parts are manufactured according to the Federal Aviation Administration (FAA) design and production approval process. These parts are approved replacements for the original OEM parts. The production of aircraft PMA parts by thirdparty companies started in the US in the 1950s. In the absence of PMA manufacturers, OEMs have the monopoly over the design and manufacture of aircraft and aftermarket parts.
关键词:航空;PMA件;制造;设计和生产;批准程序;OEM部件
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1422.全球装甲车辆升级和改造市场报告(2015-2019年)
[铁路、船舶、航空航天和其他运输设备制造业,汽车制造业] [2015-09-06]
Armored vehicles include ground combat and transportation vehicles used by landbased military forces for operations such as transporting cargo and military personnel, as well as for operating in active combats. These vehicles are protected by armor and in many cases armed with weapons. Armored vehicles provide significant strength to a country’s army and are used in large numbers by military forces around the world.
关键词:装甲车;陆基地面作战;运输车辆;活性搏斗操作;装甲保护
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1423.全球无人水下航行器市场报告(2015-2019年)
[计算机、通信和其他电子设备制造业,铁路、船舶、航空航天和其他运输设备制造业] [2015-09-06]
An unmanned underwater vehicle is a small submarine used for underwater tasks. They can be divided into two categories: ROV and AUV. ROVs are usually tethered with cables, whereas AUVs operate independently and are remotely controlled. ROVs are divided into two classes: work class and eyeball. Work class ROVs are large and heavy and have the ability to lift large equipment. Eyeball ROVs are small and used in scientific exploration, inspection, observation, and rescue. AUVs are untethered and are programmed to gather oceanographic data for a set period, without any human supervision. Payloads are attached to the unmanned underwater vehicles; they help collect data and enhance the functionality of the vehicles.
关键词:无人水下航行器;小型潜艇;ROV;水下机器人;遥控潜水器;独立运作;远程控制;收集;海洋数据
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1424.飞行航空电子设备路线图
[铁路、船舶、航空航天和其他运输设备制造业,计算机、通信和其他电子设备制造业] [2015-09-03]
As part of NASA's Avionics Steering Committee's stated goal to advance the avionics discipline ahead of program and project needs, the committee initiated a multi-Center technology roadmapping activity to create a comprehensive avionics roadmap. The roadmap is intended to strategically guide avionics technology development to effectively meet future NASA missions needs. The scope of the roadmap aligns with the twelve avionics elements defined in the ASC charter, but is subdivided into the following five areas: Foundational Technology (including devices and components), Command and Data Handling, Spaceflight Instrumentation, Communication and Tracking, and Human Interfaces.
关键词:航空电子设备;指挥和控制;航天器仪表
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1425.多任务地球大气层飞行器应用中的泡沫冲击测试
[铁路、船舶、航空航天和其他运输设备制造业,电气机械和器材制造业] [2015-09-02]
Multi-Mission Earth Entry Vehicles (MMEEVs) are blunt-body vehicles designed with the purpose of transporting payloads from outer space to the surface of the Earth. To achieve high-reliability and minimum weight, MMEEVs avoid use of limited-reliability systems, such as parachutes and retro-rockets, instead using built-in impact attenuators to absorb energy remaining at impact to meet landing loads requirements. The Multi-Mission Systems Analysis for Planetary Entry (M-SAPE) parametric design tool is used to facilitate the design of MMEEVs and develop the trade space. Testing was conducted to characterize the material properties of several candidate impact foam attenuators to enhance M-SAPE analysis. In the current effort, two different Rohacell foams were tested to determine their thermal conductivity in support of MMEEV design applications. These applications include thermal insulation during atmospheric entry, impact attenuation, and post-impact thermal insulation in support of thermal soak analysis. Results indicate that for these closed-cell foams, the effect of impact is limited on thermal conductivity due to the venting of the virgin material gas and subsequent ambient air replacement. Results also indicate that the effect of foam temperature is significant compared to data suggested by manufacturer's specifications.
关键词:航空航天器;大气层;衰减器;泡沫
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1426.冻土斜坡路基温度水分分布特性分析
[铁路、船舶、航空航天和其他运输设备制造业] [2015-08-31]
为研究冻土斜坡路基温度与水分分布规律,基于不饱和土Richards方程推导出冻土水分与温度变化的耦合关系式,建立水热耦合模型。应用有限差分原理进行离散化,编制计算程序模拟冻土斜坡路基室内模型试验。通过模拟结果与试验值的对比,验证了应用模型计算程序的可靠性。对青藏铁路风火山K1139试验段斜坡路基的温度水分分布变化进行模拟分析。结果表明:相对于同一海拔高度的路基中心线上点及右坡脚点,斜坡路基的左坡脚点温度和含水量均较高。冻土斜坡路基的融化界面与水分富集层均沿斜坡发展,与斜坡坡向相同,影响斜坡路基稳定性。
关键词:冻土路基;青藏铁路;水热耦合模型;数值模拟;温度分布
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1427.车轮擦伤对高速轮轨接触行为的影响
[铁路、船舶、航空航天和其他运输设备制造业] [2015-08-31]
在高速列车运行过程中,车轮踏面常因制动或空转打滑而造成局部擦伤。车轮擦伤将产生异常的轮轨冲击力,从而加剧车辆轨道结构的疲劳破坏。为调查车轮擦伤对高速轮轨接触行为的影响,建立考虑车轮擦伤的高速轮轨动力学模型,对新、旧两种车轮擦伤扁疤的几何形状及作用机理进行数值描述和动力学建模。基于动力学仿真计算,对新、旧车轮擦伤激扰下高速车辆的动力学响应进行详细调查,着重分析车轮擦伤对轮轨法向作用力及轮对垂向振动加速度的影响,并系统调查了车速、车轮擦伤扁疤深度及长度对高速轮轨冲击的影响,提出了高速车轮擦伤维修界限的计算方法。
关键词:高速列车;轮轨动力学;车轮擦伤;动力学建模;轮轨接触行为;维修界限
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1428.30t轴重重载列车轮轨法向接触应力分析
[铁路、船舶、航空航天和其他运输设备制造业] [2015-08-31]
轮轨接触应力对轮轨磨耗和滚动接触疲劳影响较大,因此精确计算轮轨接触点与接触应力非常重要。本文基于重载铁路轮轨标准型面,利用改进的轮对轴向切片投影法,准确找到轮轨多点接触。引入弹性压缩量,找到接触斑,利用一种精确计算轮轨接触应力的方法求得轮轨法向接触应力,并考虑轮轨摇头角和侧滚角的影响。结果表明:该方法在寻找轮轨多点接触与计算轮轨接触应力时结果较为准确、直接和全面;轮轨接触斑随着轮对横移和摇头角变化,呈现非椭圆形状;一侧车轮轮缘和轨距角处接触,曲率半径较小,轮轨法向接触应力最大值可达3 400MPa,而另一侧轮轨的法向接触应力均小于2 000MPa。在轮对横移量为0~3mm时,摇头角的增加使右轮轨接触斑面积减小,相应的接触应力增大;在轮对横移量为4~9mm时,摇头角的增加使右轮轨接触斑面积增大,相应的接触应力减小;摇头角的增加对左轮轨接触状态有利,但影响不明显。
关键词:重载列车;轮轨接触;多点接触;接触应力
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1429.高速铁路建设碳减排的算法与评判
[铁路、船舶、航空航天和其他运输设备制造业] [2015-08-31]
对高速铁路碳直接减排量、完全消耗碳减排量和完全需要碳减排量以及高速铁路碳减排量的组成进行分析计算;通过计算碳减排影响力和感应系数、行业边际完全碳减排量,分析高速铁路碳减排在整个铁路行业中的作用和影响; 采用灰色均值GM(1,1)模型,对高速铁路未来5年直接碳减排进行预测,检验模型的精度,提出碳减排弹性系数,量化高速铁路碳减排对其他行业部门和总碳减排的影响程度。结果表明,高速铁路对总碳减排的推动作用小,是最符合低碳要求的交通方式。
关键词:高速铁路;碳减排;碳减排影响力;灰色均值GM(1,1)模型;碳减排弹性系数
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1430.膨胀土地段新型基床结构动力响应数值分析
[铁路、船舶、航空航天和其他运输设备制造业] [2015-08-31]
采用一种新型的防排水结构层控制膨胀土的含水率变化,对新建云-桂高速铁路广西段的膨胀土进行整治。采用FLAC3D有限差分软件分析云-桂线中强和中弱膨胀土地段新型基床(基床中设置新型防排水结构层)在列车荷载作用下的动力响应规律,利用现场试验结果对数值分析结果进行验证,对比分析两类膨胀土地段基床动力响应规律的异同。研究表明:新型基床结构动应力、动位移、振动速度和加速度随深度的增加而减小;基床动应力的现场实测值与软件计算值规律基本一致,且大小相近,说明该数值模拟分析新型基床的动力响应规律可行;中强、中弱膨胀土地段的新型防排水结构层上下表面的动应力、剪应力存在差异,但其基床结构内的动应力、动位移、速度和加速度的衰减规律一致。本文为膨胀土地区高速铁路基床的设计、施工及其动力响应研究提供参考。
关键词:中-强膨胀土;中-弱膨胀土;新型基床结构;FLAC3D;现场试验;动应力