期刊文献+
共找到141篇文章
< 1 2 8 >
每页显示 20 50 100
Influence of the gassing materials on the dielectric properties of air 被引量:2
1
作者 张含天 厉天威 +4 位作者 罗兵 吴翊 杨飞 孙昊 唐力 《Plasma Science and Technology》 SCIE EI CAS CSCD 2017年第5期68-73,共6页
Influence of the gassing materials, such as PA6, PMMA, and POM on the dielectric properties of air are investigated. In this work, the fundamental electron collision cross section data were carefully selected and vali... Influence of the gassing materials, such as PA6, PMMA, and POM on the dielectric properties of air are investigated. In this work, the fundamental electron collision cross section data were carefully selected and validated. Then the species compositions of the air–organic vapor mixtures were calculated based on the Gibbs free energy minimization. Finally, the Townsend ionization coefficient, the Townsend electron attachment coefficient and the critical reduced electric field strength were derived from the calculated electron energy distribution function by solving the Boltzmann transport equation. The calculation results indicated that H;O with large attachment cross sections has a great impact on the critical reduced electric field strength of the air–organic vapor mixtures. On the other hand, the vaporization of gassing materials can help to increase the dielectric properties of air circuit breakers to some degree. 展开更多
关键词 air circuit breaker gassing materials Boltzmann equation analysis dielectric properties EEDF critical reduced electric field strength electron collision cross section
下载PDF
Study on Non-Collision Mineralizing Mechanism of Froth Cyclone
2
作者 董平 许占贤 周晓玲 《Journal of China University of Mining and Technology》 2002年第1期20-24,共5页
On the basis of the mineralizing mechanism of froth cyclone, this paper expounds that the froth cyclone flotation process is accomplished in a limited centrifugal field. The main feature of air bubble mineralizing in ... On the basis of the mineralizing mechanism of froth cyclone, this paper expounds that the froth cyclone flotation process is accomplished in a limited centrifugal field. The main feature of air bubble mineralizing in the froth cyclone is a synthetic mineralizing process, of which the non collision mineralization of minute air bubble separated out dominates, supplemented with the collision mineralization. Moreover, this paper points out that the hydrophobic separated out and centrifugal force strengthen the selectivity of fine coal particle, accelerate the flotation speed and improve the slime recovery. 展开更多
关键词 froth cyclone mineralizing air bubble non collision centrifugal force
下载PDF
TRANSPRESSIVE DEFORMATION OF THE LONGXINGGOU NAPPE AND ITS SIGNIFICANCE,SOUTH OF TONGBAI MOUNTAINS, CENTRAL CHINA
3
作者 Wang Guocan Liu Rong and He Bing(China Univercity of Gcosciences, Wuhan, 430074) 《Geotectonica et Metallogenia》 1995年第4期53-61,共9页
The Longxinggou Nappe which is located in Guangshui county, north of Hubei province, has been first identified by our detail mapping. It is composed of lowgrade metamorphosed rocks of middle Proterozoic Shuixian group... The Longxinggou Nappe which is located in Guangshui county, north of Hubei province, has been first identified by our detail mapping. It is composed of lowgrade metamorphosed rocks of middle Proterozoic Shuixian group, late Proterozoic Yaolinghe group, Sinian Liantuo,Doushantuo and Dengying formations. It is quite different from the lower beds, middle.Proterozoic Hong’an epidote-amphibole facies metamorphose metapelite and metagranite. They are different not only in composition, metamorphic degree, but also in deformation forms. The Longxinggou nappe has characteristics both of ductile thrusting and ductile dextral strike-sliping, illustrating a transpressive deformation regime of middle crustal in the orogenic belt due to the oblique collision, between the Shuiying terrain and the Tongbai terrain during Caledonian period. 展开更多
关键词 Longxinggou NAPPE Tongbai MOUNTAinS transpressive deformation CALEDONIAN collision OROGENY
下载PDF
Numerical analysis method of ship-ice collision-induced vibration of the polar transport vessel based on the full coupling of ship-ice-water-air 被引量:1
4
作者 Yuan-He Shi De-Qing Yang Wen-Wei Wu 《Journal of Ocean Engineering and Science》 SCIE 2023年第4期323-335,共13页
As the Arctic Channel continues to be developed,collisions between polar navigation vessels and sea ice are inevitable,which will directly affect structural safety and vibration comfort.However,the numerical analysis ... As the Arctic Channel continues to be developed,collisions between polar navigation vessels and sea ice are inevitable,which will directly affect structural safety and vibration comfort.However,the numerical analysis method of ship-ice collision-induced vibration is not perfect,and the effect of fluid coupling is not typically considered.In this paper,a simplified numerical analysis method for ship-ice collision-induced vibration is proposed,in which a reliable ice load is obtained by first performing ship-ice-water-air coupled collision calculations,followed by ship-ice-water coupled vibration calculations to obtain the vibration response of the structure.In addition,this paper investigates the full coupling method and the modeling ranges and meshing sizes involved in the analysis ship-ice collision-induced vibration,and the computational efficiencies of the traditional ALE algorithm and S-ALE algorithm are compared.The results indicate that the simplified simulation analysis method and gradient meshing model improve the calculation accuracy and efficiency in ship-ice collision and vibration response analysis.Moreover,the modeling range of the water and air models cannot be less than 6 times the ship width,2 times the ship length,and 1 times the ship depth,and the S-ALE algorithm saves 47.86%time compared to the ALE algorithm.The research results in this paper can provide a reference for the numerical simulation of ship-ice collision-induced vibration. 展开更多
关键词 Ship–ice collision Ice-induced vibration Ship–ice–water–air coupling Fluid–structure interaction S-ALE algorithm Gradient meshing model
原文传递
Collision risk assessment of reduced aircraft separation minima in procedural airspace using advanced communication and navigation
5
作者 Qing CAI Hao Jie ANG Sameer ALAM 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2023年第4期315-337,共23页
With the advancement of Communication,Navigation and Surveillance(CNS)technolo-gies such as space-based Automatic Dependent Surveillance-Broadcast/Contract(ADS-B/C),large separation minima may be reduced in procedural... With the advancement of Communication,Navigation and Surveillance(CNS)technolo-gies such as space-based Automatic Dependent Surveillance-Broadcast/Contract(ADS-B/C),large separation minima may be reduced in procedural airspaces.It is of great significance to know the upper limit of the Reduced Separation Minima(RSM)for a procedural airspace and the corre-sponding consequences on collision risk with specifics of the advanced ADS-B and control interven-tion model.In this work,an interactive software is first developed for collision risk estimation.This software integrates the International Civil Aviation Organization(ICAO)collision risk models for lateral and longitudinal collision risk calculation for the Singapore procedural airspace.Results demonstrate that the lateral and longitudinal collision risk of Singapore procedural airspace with respect to current control procedures meets the ICAO Target Level of Safety(TLS)standard.Moreover,the feasibility of reducing the horizontal separations implemented in the Singapore pro-cedural airspace with respect to advanced CNS techniques is investigated.It is found that if advanced CNS technologies are applied,then the current 50-NM lateral and longitudinal separa-tion standards can be reduced to 22 NM(1 NM=1.825 km)and 20 NM,respectively,to meet the TLS standards based on current demand.A method is then devised to expand the traffic demand by p for p∈[10%,200%].It is found that the minimum lateral and longitudinal separa-tions can be reduced from 50 NM to be within the range of[23,31]NM,and 20 NM,respectively,for p∈[10%,200%],while the collision risk still meets the TLS standards. 展开更多
关键词 air transportation collision risk Procedural airspace Separation minima Space-based Automatic Dependent Surveillance-Bro adcast/Contract(ADS-B/C)
原文传递
固体火箭发动机真实热环境下EPDM绝热层烧蚀计算与试验研究 被引量:2
6
作者 刘沙石 檀叶 +2 位作者 王鹏飞 冯喜平 张雁 《固体火箭技术》 CAS CSCD 北大核心 2024年第1期99-111,共13页
基于Hertz弹性碰撞理论和Thornton弹塑性假设,导出了粒子碰撞炭层过程中的压痕硬度理论表达式,根据弯管试验数据和试件扫描电镜分析提出了临界速度模型,对于三元乙丙橡胶(EPDM)炭化后形成的多孔炭化结构,结合裂纹侵蚀理论提出了两相流... 基于Hertz弹性碰撞理论和Thornton弹塑性假设,导出了粒子碰撞炭层过程中的压痕硬度理论表达式,根据弯管试验数据和试件扫描电镜分析提出了临界速度模型,对于三元乙丙橡胶(EPDM)炭化后形成的多孔炭化结构,结合裂纹侵蚀理论提出了两相流非完全弹性碰撞多孔炭化层体烧蚀计算模型。设计了用于验证烧蚀计算模型的模拟发动机旋转过载试验,保证了模拟发动机和真实发动机的天地一致性。结果表明:在模拟发动机真实飞行过程的热环境下,计算结果与实测结果能够基本吻合。研究结果对固体火箭发动机绝热结构的设计具有工程指导意义。 展开更多
关键词 Hertz弹性碰撞理论 粒子侵蚀 三元乙丙绝热层 旋转过载试验 天地一致性
下载PDF
卧式气浮器设计及流场仿真研究
7
作者 王英 李兴振 +3 位作者 程光玮 胡徐彦 李艳坤 尹凝霞 《青岛大学学报(工程技术版)》 CAS 2024年第3期86-92,共7页
为了提高卧式气浮器的除油效率,对卧式气浮器的结构进行优化设计计算。采用CFD(Computational Fluid Dynamics)技术,研究了不同结构的流场变化特性。仿真结果表明,卧式气浮器流场仿真过程显示出阶梯分层效果,可以处理含油废水;当入水口... 为了提高卧式气浮器的除油效率,对卧式气浮器的结构进行优化设计计算。采用CFD(Computational Fluid Dynamics)技术,研究了不同结构的流场变化特性。仿真结果表明,卧式气浮器流场仿真过程显示出阶梯分层效果,可以处理含油废水;当入水口在左中间轴向,挡板高度为120 mm和出水口在右中间轴向时,卧式气浮器的除油率最高可达98.75%。 展开更多
关键词 卧式气浮器 碰撞 除油率 气浮效果
下载PDF
NEW METHOD FOR SAFETY ASSESSMENT OF PARALLEL ROUTES 被引量:1
8
作者 隋东 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2009年第1期36-43,共8页
A new safety assessment method for parallel routes is presented. From the aspects of safety guard system of air traffic control(ATC) and considering the flight conflict as causing event of air collision accidents, t... A new safety assessment method for parallel routes is presented. From the aspects of safety guard system of air traffic control(ATC) and considering the flight conflict as causing event of air collision accidents, this paper fosters a four-layer safety guard of controller command, short-term conflict alerts (STCAs), pilot visual avoidance, and traffic alert collision avoidance system(TCAS). Then, the problem of parallel routes collision risk is divided into two parts:the calculation of potential flight conflict and the analysis of failure probability of the four-layer safety guard. A calculation model for controller interference times is induced. By using cognitive reliability and error analysis method(CREAM),the calculation problem to failure probability of controller sequencing flight conflicts is solved and a fault tree model of guard failure of STCA and TCAS is established. Finally, the Beijing-Shanghai parallel routes are taken as an example to be calculated and the collision risk of the parallel routes is obtained under the condition of radar control. Results show that the parallel routes can satisfy the safety demands. 展开更多
关键词 air traffic control human factors safety assessment short-term conflict alerts traffic alert collision avoidance system
下载PDF
两座210m高烟囱定向爆破拆除空中对碰技术研究
9
作者 张焜琨 张耀良 +5 位作者 夏云鹏 张中威 李杰 钱坤 徐阳 陈美常 《工程爆破》 CSCD 北大核心 2024年第1期96-103,共8页
位于镇江市谏壁发电厂内的两座高210 m的烟囱需进行拆除,受周边环境和正常运行的两台100万机组的影响,振速不能过大。经分析论证,选择两座烟囱相对定向倒塌、空中相碰的方案是影响最小的最优方案,通过选择切口位置、精确定位倒塌方向、... 位于镇江市谏壁发电厂内的两座高210 m的烟囱需进行拆除,受周边环境和正常运行的两台100万机组的影响,振速不能过大。经分析论证,选择两座烟囱相对定向倒塌、空中相碰的方案是影响最小的最优方案,通过选择切口位置、精确定位倒塌方向、开设定向窗、多层次全方位防护等措施,结合对碰模拟分析结果以及现场测试数据等技术手段,最终两座烟囱在空中实现对碰,且周边保护目标安全无恙,此爆破方法为国内首例,对类似工程有一定的借鉴作用。 展开更多
关键词 烟囱 拆除爆破 钢筋混凝土 空中对碰 防护 数值模拟
下载PDF
基于多属性效用博弈框架的飞机自动防撞算法
10
作者 胡杨 《科技资讯》 2024年第3期15-18,共4页
随着航空运输量的高速增长,飞机发生空中冲突数量成倍增加。为了保证空域飞行的安全性,高性能的飞机防撞算法十分重要。结合多属性效用理论和Level-K博弈框架,提出了一种用于飞机自动防撞算法。该算法利用多属性效用理论综合飞机防撞过... 随着航空运输量的高速增长,飞机发生空中冲突数量成倍增加。为了保证空域飞行的安全性,高性能的飞机防撞算法十分重要。结合多属性效用理论和Level-K博弈框架,提出了一种用于飞机自动防撞算法。该算法利用多属性效用理论综合飞机防撞过程中需要考虑的多个目标,并利用Level-K博弈建模两架飞机在防撞过程中的相互博弈。实验结果表明:文中提出的自动防撞算法能方便、有效地提高飞机的防撞性能,同时算法的性能优于目前飞机装备的自动防撞系统。 展开更多
关键词 航空运输 多属性效用 博弈框架 防撞算法
下载PDF
通用航空转场飞行与运输航空横向碰撞风险研究
11
作者 张乐 杨晓琳 左杰俊 《中国民航飞行学院学报》 2024年第6期11-15,共5页
为确定《民用航空空中交通管理规则》第二百二十四条所述情形的碰撞风险,提高空域利用率,确保飞行安全,文章以Reich模型为基础,利用概率论理论建立了通航转场航线飞行与运输航空进近阶段飞行的横向碰撞模型。对比分析验证了所述横向碰... 为确定《民用航空空中交通管理规则》第二百二十四条所述情形的碰撞风险,提高空域利用率,确保飞行安全,文章以Reich模型为基础,利用概率论理论建立了通航转场航线飞行与运输航空进近阶段飞行的横向碰撞模型。对比分析验证了所述横向碰撞模型的可靠性,并对通航转场飞行与运输航空进近阶段的碰撞风险进行评估。结果表明,文中所假设的场景下,通航转场航线与运输航空进近航线同高度同向飞行时,横向间隔12km可以保持独立运行,横向间隔9.6km时需另外规定一个纵向间隔。 展开更多
关键词 空中交通管理 碰撞模型 飞行程序 安全评估
下载PDF
A survey of safety separation management and collision avoidance approaches of civil UAS operating in integration national airspace system 被引量:11
12
作者 Xiangmin GUAN Renli LYU +1 位作者 Hongxia SHI Jun CHEN 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2020年第11期2851-2863,共13页
Recent years have witnessed a booming of the industry of civil Unmanned Aircraft System(UAS).As an emerging industry,the UAS industry has been attracting great attention from governments of all countries and the aviat... Recent years have witnessed a booming of the industry of civil Unmanned Aircraft System(UAS).As an emerging industry,the UAS industry has been attracting great attention from governments of all countries and the aviation industry.UAS are highly digitalized,informationized,and intelligent;therefore,their integration into the national airspace system has become an important trend in the development of civil aviation.However,the complexity of UAS operation poses great challenges to the traditional aviation regulatory system and technical means.How to prevent collisions between UASs and between UAS and manned aircraft to achieve safe and efficient operation in the integrated operating airspace has become a common challenge for industry and academia around the world.In recent years,the international community has carried out a great amount of work and experiments in the air traffic management of UAS and some of the key technologies.This paper attempts to make a review of the UAS separation management and key technologies in collision avoidance in the integrated airspace,mainly focusing on the current situation of UAS Traffic Management(UTM),safety separation standards,detection system,collision risk prediction,collision avoidance,safety risk assessment,etc.,as well as an analysis of the bottlenecks that the current researches encountered and their development trends,so as to provide some insights and references for further research in this regard.Finally,this paper makes a further summary of some of the research highlights and challenges. 展开更多
关键词 air transportation collision avoidance SAFETY Separation control Unmanned aircraft system
原文传递
Suggesting a Very Simple Experiment Designed to Detect Tachyons
13
作者 Jerzy K. Kowalczyński 《Journal of Modern Physics》 2011年第2期92-96,共5页
Production of tachyons in, among other things, air showers would be in accordance with predictions of general relativity. Some such tachyons would travel with a precisely determined speed, almost equal to 5c/3 relativ... Production of tachyons in, among other things, air showers would be in accordance with predictions of general relativity. Some such tachyons would travel with a precisely determined speed, almost equal to 5c/3 relative to the earth, and would be registered high above the region of creation of air showers, e.g. on board of a satellite. A very simple experiment designed to detect these tachyons is outlined here. Brief justification to search for tachyons is also given. 展开更多
关键词 TACHYON HIGH-ENERGY collision air SHOWER TIME-of-FLIGHT Experiment Satellite
下载PDF
自由空域下多旋翼无人机安全间隔标定方法 被引量:2
14
作者 张洪海 李博文 +2 位作者 刘皞 钟罡 费毓晗 《系统工程与电子技术》 EI CSCD 北大核心 2023年第10期3149-3156,共8页
为确保低空空域内无人机的运行安全,考虑多旋翼无人机的特点,提出一种自由空域下多旋翼无人机安全间隔标定方法。首先,以无人机机体圆柱的最小外接球作为无人机的碰撞盒,利用无人机的位置信息、速度信息和位置误差信息,基于三维高斯分... 为确保低空空域内无人机的运行安全,考虑多旋翼无人机的特点,提出一种自由空域下多旋翼无人机安全间隔标定方法。首先,以无人机机体圆柱的最小外接球作为无人机的碰撞盒,利用无人机的位置信息、速度信息和位置误差信息,基于三维高斯分布假设,建立无人机空中碰撞概率模型;然后,根据自由空域的特点,提出基于最大碰撞概率的无人机安全间隔标定方法。以经纬M600 Pro无人机为例,将5%最大碰撞概率作为安全目标水平,使用该方法得到的最小安全间隔分别为:纵向间隔16 m,横向间隔11 m,垂直间隔6 m。据此,可为多旋翼无人机安全间隔标准的制定提供理论依据。 展开更多
关键词 航空运输 安全间隔标定 碰撞概率 多旋翼无人机 自由空域
下载PDF
空中防撞系统中提高空中安全的决议咨询算法 被引量:1
15
作者 朱安 刘庆玲 哈迪 《应用科技》 CAS 2023年第3期85-92,共8页
随着航空界向下一代航空运输系统(Next-Gen)迈进,当前的交通警报和防撞系统(TCAS II)无法完全保障航空安全,因此如何防止空中碰撞是下一代交通系统的一个重要问题。为解决此问题,本文介绍了一种新技术,用于检测和解决三维空域中2架飞机... 随着航空界向下一代航空运输系统(Next-Gen)迈进,当前的交通警报和防撞系统(TCAS II)无法完全保障航空安全,因此如何防止空中碰撞是下一代交通系统的一个重要问题。为解决此问题,本文介绍了一种新技术,用于检测和解决三维空域中2架飞机之间的空中交通冲突。该算法计算一组6个决议咨询并结合决断警报时间,以确保不侵犯保护区。该算法提出了3种安全规则解决方案,用于提高飞机面对面、飞机交叉道和飞机超车这3种场景下的安全性。本文在所提出的3个安全规则基础上进行仿真,以验证所提出算法的有效性,仿真结果表明,本文提出的方法相较于传统方法具备一定的优越性。 展开更多
关键词 下一代航空运输系统 交通警报和防撞系统 决议咨询 空中碰撞 监视 空中碰撞风险 下一代美国联邦航空管理局
下载PDF
基于可达集的无人机低空飞行冲突解脱算法 被引量:1
16
作者 杨建航 张福彪 王江 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2023年第7期1813-1827,共15页
针对无人空中交通管理(UTM)中的冲突解脱问题,提出了以可达集分析为基础的实时避撞算法。该算法可用于城市低空环境中的密集交通流空域,保证无人机(UAV)飞行过程的安全性。基于相对运动的概念,通过分析平面空域中的飞行博弈问题对避撞... 针对无人空中交通管理(UTM)中的冲突解脱问题,提出了以可达集分析为基础的实时避撞算法。该算法可用于城市低空环境中的密集交通流空域,保证无人机(UAV)飞行过程的安全性。基于相对运动的概念,通过分析平面空域中的飞行博弈问题对避撞系统进行建模,同时利用水平集方法和最优控制理论对无人机的可达集进行分析和计算,使用机载传感器获取无人机与周围物体的信息,为每架无人机提供新的避撞策略。通过3种不同空域环境的飞行案例进行仿真实验,验证了该策略不仅可以得到平滑的飞行路径,实时安全地解决冲突解脱问题,而且针对合作/非合作目标均有效。 展开更多
关键词 无人空中交通管理 冲突解脱 城市低空环境 可达集分析 避撞策略 平面空域
原文传递
BIM技术在人防地下室设计中的应用 被引量:2
17
作者 雷洋 徐星 《中国建设信息化》 2023年第6期78-82,共5页
传统人防地下室设计的平时设计、战时设计相互独立采用二维设计,常常出现各种冲突和错漏,为人防工程发挥其功能埋下隐患。本文探讨了在人防地下室设计中利用BIM技术进行平战转换、碰撞检测、净高分析、管线综合、支吊架设计、孔洞套管... 传统人防地下室设计的平时设计、战时设计相互独立采用二维设计,常常出现各种冲突和错漏,为人防工程发挥其功能埋下隐患。本文探讨了在人防地下室设计中利用BIM技术进行平战转换、碰撞检测、净高分析、管线综合、支吊架设计、孔洞套管和建立人防设备族等七个方面的应用有利于提高设计效率和设计质量,便于在战时没有专业安装人员的情况下也能快速实现转换施工。插件的适当应用可以提高设计人员对BIM技术的接受度,便于实现BIM技术的快速高效发展。 展开更多
关键词 人防设计 人防地下室 BIM 碰撞检测 平战转换
下载PDF
碰撞速度和碰撞角度对典型材料起电影响 被引量:1
18
作者 翟维鹏 胡小锋 +1 位作者 周帅 王莹莹 《兵工学报》 EI CAS CSCD 北大核心 2023年第5期1358-1364,共7页
针对飞行器沉积静电问题,以典型材料起电电压为研究对象,进一步探索在不同碰撞角度、碰撞速度条件下,典型材料与空气颗粒物碰撞后的起电变化规律。采取模拟试验和仿真分析相结合的方式,重点研究空气颗粒物碰撞角度和碰撞速度对于典型材... 针对飞行器沉积静电问题,以典型材料起电电压为研究对象,进一步探索在不同碰撞角度、碰撞速度条件下,典型材料与空气颗粒物碰撞后的起电变化规律。采取模拟试验和仿真分析相结合的方式,重点研究空气颗粒物碰撞角度和碰撞速度对于典型材料的起电影响,初步得出部分材料起电电压随碰撞角度和碰撞速度的变化规律。试验结果表明:典型材料起电电压随着碰撞角度的增加近似呈线性增大,随着碰撞速度的增加近似呈线性增大;碰撞速度会影响接触面积和接触模式,碰撞角度会影响接触面积中不同模式所占比例,二者共同影响着典型材料起电电压的变化。 展开更多
关键词 沉积静电 典型材料 空气颗粒物 碰撞角度 碰撞速度
下载PDF
轨道车辆碰撞试验台CO_(2)相变驱动过程仿真研究
19
作者 王甲强 鲁寨军 +3 位作者 刘东润 张梓轩 李田 姚术健 《中国铁道科学》 EI CAS CSCD 北大核心 2023年第6期113-124,共12页
由于现有设备条件下空气炮驱动的轨道列车碰撞试验台无法满足更高试验速度的要求,提出使用CO_(2)相变动力驱动试验车辆加速。基于质量守恒定律、能量守恒定律和CO_(2)真实气体模型,建立驱动系统做功过程数值模型;对模型求解后,通过试验... 由于现有设备条件下空气炮驱动的轨道列车碰撞试验台无法满足更高试验速度的要求,提出使用CO_(2)相变动力驱动试验车辆加速。基于质量守恒定律、能量守恒定律和CO_(2)真实气体模型,建立驱动系统做功过程数值模型;对模型求解后,通过试验验证模型计算精度;通过数值模型,对比研究空气与CO_(2)的做功性能,并分析储液缸初始压力、初始温度和驱动缸初始容积对CO_(2)做功特性的影响规律。结果表明:模型能够有效模拟CO_(2)液气相变驱动试验车做功过程;在结构条件相同且驱动工质的质量为170 kg、初始压力为20 MPa时,以CO_(2)作为驱动工质时驱动时间较空气缩短10.5%,试验车获得的末速度较空气增大21.2%;储液缸初始压力由8MPa增至20 MPa时,试验车末速度增大58.3%,加速时间减少32.2%;初始温度对驱动缸内CO_(2)相态影响较大,温度越低时,其相态越容易接近气液饱和线;驱动缸初始容积对加速时间、试验车过载和活塞所受冲击影响较大,初始容积为0.20 m3时较0.01 m3时最大过载减小23.07%,但所用时间增加20.9%。 展开更多
关键词 轨道车辆 列车碰撞试验台 CO_(2)相变 空气 气动弹射 数值模拟
下载PDF
膝部安全气囊仿真与优化 被引量:1
20
作者 栾海 田国红 程海东 《汽车零部件》 2023年第1期14-17,共4页
本文针对正面气囊和安全带等被动安全装置在正面碰撞中对乘员腿部保护效果有限问题,通过计算机仿真探究膝部安全气囊对乘员腿部的保护效果。利用仿真软件MADYMO建立含有和不含有膝部安全气囊的正面碰撞约束系统,并且对这两个约束系统进... 本文针对正面气囊和安全带等被动安全装置在正面碰撞中对乘员腿部保护效果有限问题,通过计算机仿真探究膝部安全气囊对乘员腿部的保护效果。利用仿真软件MADYMO建立含有和不含有膝部安全气囊的正面碰撞约束系统,并且对这两个约束系统进行碰撞仿真模拟;对含有膝部安全气囊的正面碰撞约束系统进行灵敏度分析、正交试验设计和极差分析,并进一步优化,同时将两个约束系统中假人的伤害指标和时程曲线进行对比。结果表明:膝部安全气囊可以减少正面碰撞时乘员腿部的损伤情况。 展开更多
关键词 正面碰撞 膝部安全气囊 正交试验
下载PDF
上一页 1 2 8 下一页 到第
使用帮助 返回顶部