期刊文献+
共找到7篇文章
< 1 >
每页显示 20 50 100
偏离规范的要求授权的所需导航性能飞行程序设计及实例分析 被引量:1
1
作者 向小军 陈红英 《交通运输系统工程与信息》 EI CSCD 北大核心 2014年第4期239-243,共5页
要求授权的所需导航性能(RNP AR:Required Navigation Performance Authorization Required)飞行程序设计灵活,用于高原山区和地形复杂机场可以降低运行标准.在实际运行中为降低运行标准设计的RNP AR飞行程序可能会偏离相关规范,本文研... 要求授权的所需导航性能(RNP AR:Required Navigation Performance Authorization Required)飞行程序设计灵活,用于高原山区和地形复杂机场可以降低运行标准.在实际运行中为降低运行标准设计的RNP AR飞行程序可能会偏离相关规范,本文研究了实际中由于地形等原因,在最后进近对正跑道的最短距离和复飞RNP值小于1的最大长度等方面偏离相关规范的情况.以国内某机场RNP AR进近程序设计为例,设计了在最后进近滚出点到入口的距离和复飞最大长度都偏离国际民航组织(ICAO:International Civil Aviation Organization)规范的RNP AR进近飞行程序,给出了进近和复飞设计参数.通过某机型的模拟机验证说明设计的偏离规范RNP AR飞行程序是可行的,能够满足运行和安全水平要求. 展开更多
关键词 交通工程 偏离规范 模拟机验证 RNP AR飞行程序 航行新技术
下载PDF
空域调整方案安全风险评估方法研究
2
作者 向征 祝琳芸 +1 位作者 张文军 钟建华 《哈尔滨商业大学学报(自然科学版)》 CAS 2018年第4期447-451,457,共6页
为了确保空域调整后空域结构的安全性,需要预判设计的空域调整方案是否在合理的安全风险以内.提出四种空域调整方案安全风险评估方法,专家评估法、计算机仿真法、雷达模拟机验证法和运行监控评估法.通过对比得出不同方法的优缺点,为合... 为了确保空域调整后空域结构的安全性,需要预判设计的空域调整方案是否在合理的安全风险以内.提出四种空域调整方案安全风险评估方法,专家评估法、计算机仿真法、雷达模拟机验证法和运行监控评估法.通过对比得出不同方法的优缺点,为合理选择评估方法提供依据.与此同时,提出上述方法可以用于雷暴天气下,航空器绕飞雷暴时的改航航路规划的安全风险评估. 展开更多
关键词 安全风险评估 专家评估法 计算机仿真法 雷达模拟机验证 运行监控评估法 绕飞雷暴
下载PDF
某机组停堆棒意外掉落事件分析及处理研究 被引量:1
3
作者 王超 杨文清 +7 位作者 黄正东 李晓飞 袁盛馨 柳继坤 刘东亮 汪宇 程雄伟 肖京 《自动化仪表》 CAS 2021年第S01期247-252,共6页
为分析某机组棒控棒位系统(RGL)停堆棒束K16意外掉落事件原因,研究了提高RGL运行稳定性和可靠性的方法。根据控制棒动作原理,通过对动棒时序进行分析,采用逐步排除的方式调查事件原因。从机组安全、共因故障、落棒功能及模拟机验证等角... 为分析某机组棒控棒位系统(RGL)停堆棒束K16意外掉落事件原因,研究了提高RGL运行稳定性和可靠性的方法。根据控制棒动作原理,通过对动棒时序进行分析,采用逐步排除的方式调查事件原因。从机组安全、共因故障、落棒功能及模拟机验证等角度进行分析。根据分析结果,提出解决方案和建议措施。建议和措施在该机组的实施,有效地保障了RGL正常运行,降低了意外落棒的风险。同时,该处理方式也为其他核电机组解决同类问题提供了参考。 展开更多
关键词 RGL 控制棒 意外落棒 动棒时序 停堆棒 机组安全 落棒功能 模拟机验证
下载PDF
Ultrasonic Sensors with Mechanical Couplers: Simulation and Validation
4
作者 Monica Femendez Cristina Rodriguez Juan M. Perez Oria Manuel Ibarra Luciano Alonso 《Journal of Mathematics and System Science》 2012年第4期264-271,共8页
The use of ultrasonic sensors has varied applications, but the sensor operation frequency limits the operating distance. An easy way to increase this distance is to couple a mechanical element (horn), but it is nece... The use of ultrasonic sensors has varied applications, but the sensor operation frequency limits the operating distance. An easy way to increase this distance is to couple a mechanical element (horn), but it is necessary to characterize this technique. In this paper the results obtained in a study of the behaviour of mechanical elements coupled to an ultrasonic sensor using finite element techniques are presented. These results have been obtained using Comsol Multiphysics modelling. Also, the effect caused by the sensor size on the radiation acoustic pressure has also been evaluated. In other way, in this paper it is presented the results obtained in the laboratory measurements. First, it is studied the influence of a straight horn attached to the ultrasonic sensor. Later, it is presented the variation in the sound pressure on the radiation axis when the sensor varies its size. In the final part of the paper, the experimental validation of the simulations is presented. 展开更多
关键词 ULTRASOUNDS SENSORS homs radiation pattem.
下载PDF
Verification on Spray Simulation of a Pintle Injector for Liquid Rocket Engine 被引量:16
5
作者 Min Son Kijeong Yu +2 位作者 Kanmaniraja Radhakrishnan Bongchul Shin Jaye Koo 《Journal of Thermal Science》 SCIE EI CAS CSCD 2016年第1期90-96,共7页
The pintle injector used for a liquid rocket engine is a newly re-attracted injection system famous for its wide throttle ability with high efficiency. The pintle injector has many variations with complex inner struct... The pintle injector used for a liquid rocket engine is a newly re-attracted injection system famous for its wide throttle ability with high efficiency. The pintle injector has many variations with complex inner structures due to its moving parts. In order to study the rotating flow near the injector tip, which was observed from the cold flow experiment using water and air, a numerical simulation was adopted and a verification of the numerical model was later conducted. For the verification process, three types of experimental data including velocity distributions of gas flows, spray angles and liquid distribution were all compared using simulated results. The numerical simulation was performed using a commercial simulation program with the Eulerian multiphase model and axisymmetric two dimensional grids. The maximum and minimum velocities of gas were within the acceptable range of agreement, however, the spray angles experienced up to 25% error when the momentum ratios were increased. The spray density distributions were quantitatively measured and had good agreement. As a result of this study, it was concluded that the simulation method was properly constructed to study specific flow characteristics of the pintle injector despite having the limitations of two dimensional and coarse grids. 展开更多
关键词 Spray characteristics Pintle injector Simulation Experiment Liquid rocket engine
原文传递
Investigation of performances and flow characteristics of two bi-directional pumps with different airfoil blades 被引量:6
6
作者 MA PengFei WANG Jun WANG HaiFeng 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2018年第10期1588-1599,共12页
Today, the most commonly used bi-directional airfoil in hydraulic machinery is the S-shaped airfoil(SA). A new bi-directional airfoil, obtained by lowering the bent airfoil camber and thickening the bone line bi-direc... Today, the most commonly used bi-directional airfoil in hydraulic machinery is the S-shaped airfoil(SA). A new bi-directional airfoil, obtained by lowering the bent airfoil camber and thickening the bone line bi-directionally, is proposed. Two bi-directional axial flow pumps, with the SA blades and the arc airfoil(AA) blades, respectively, were designed to verify the applicability of this airfoil. By comparing the hydraulic performances of the two pumps obtained from the experiments, and the cavitation performance and flow field of the two pumps obtained from numerical simulations, it was found that AA blades can improve both the hydraulic and cavitation performances under a low flow rate and near the best efficiency flow point(BEP), whether in forward or reverse operation for the bi-directional axial-flow pump. Furthermore, the hydraulic performance of the AA blade pump declines sharply in a large flow rate compared to that of the SA blade pump. The location and composition of the inhomogeneous flows inside the impellers of the two pumps are similar. However, the SA blades work on fluid, mainly at the front half of the blades, which is a distinctive feature from the AA blades and may be a universal phenomenon in all SA-type blades. 展开更多
关键词 axial-flow pump AIRFOIL numerical simulation CAVITATION
原文传递
A miniature pump with a fluid dynamic bearing 被引量:4
7
作者 LUO XianWu JI Bin +3 位作者 ZHUANG BaoTang ZHU Lei LU Li XU HongYuan 《Science China(Technological Sciences)》 SCIE EI CAS 2012年第3期795-801,共7页
This paper describes the development of a miniature pump having an impeller with an exit diameter of 24 mm supported with the motor rotor by a fluid dynamic beating. Tests verify that the miniature pump is stable and ... This paper describes the development of a miniature pump having an impeller with an exit diameter of 24 mm supported with the motor rotor by a fluid dynamic beating. Tests verify that the miniature pump is stable and quiet for rotational speeds larger than 4000 rain-1. The three-dimensional turbulent flow in the entire pump flow passage and the laminar flow in the fluid dynamic bearing were then simulated numerically. The average pump performance was well predicted by the simulations. Both the tests and the simulations show that there is no obvious Reynolds effect for the miniature pump within the tested range of rotational speeds. The numerical results also show that the beating capacity of the fluid dynamic bearing increases with the pump rotor rotational speed and the eccentricity ratio of the journal to the bushing. This pump is very compact, so it is a prom- ising device for surgical use. 展开更多
关键词 miniature pump fluid dynamic bearing hydraulic performance EXPERIMENT numerical simulation
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部