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双语推荐:等离子体发生器

空气等离子喷涂工艺在许多领域得到了应用。近年来,国立圣彼得堡综合技术大学在等离子体发生器的创建和涂覆工艺方面进行了研究,业已研制成多种涂层,既可用于新制零件的防护,也可用于磨损件的修复。国立圣彼得堡综合技术大学和雷波尼茨( INP Greifswald )等离子体及工艺研究院联合进行的理论和试验研究,可显著减少研发等离子体发生器和空气等离子涂覆工艺的试验工作量。
The air-plasma spraying technology has been found application in many fields .In recent years , research on both establishment of plasma generator and spraying process has been performed in the St .Petersburg State Polytechnic University , and many types of coatings , which may not only be used to protect freshly made parts but also to restore worn parts , have been developed .The theoretical and experimental investigations conducted by the St.Petersburg State Polytechnic University in conjunction with the Leibnits ( INP Greifswald ) Plasma and Technology Research Institute will allow amount of experimental work to be appreciably reduced in developing the plasma generator and the air-plasma spraying process .
综述了美国NIST元素汞发生器的基准溯源传递方法,通过在输出的汞标准气体中混合加入已知高纯度的201Hg0气体(201Hg2+标准溶液还原雾化),并采用同位素稀释电感耦合等离子体/质谱法(ID ICP/MS)测量加标后201Hg/202Hg同位素丰度比例,计算出待溯源元素汞发生器输出的Hg0质量浓度。该过程实现了从元素汞一级标准物质SRM 3133到201Hg2+标准溶液,再到元素汞发生器输出标准气体的溯源传递,完成了从NIST元素汞基准到仪器供应商生产基准的一级溯源传递,为建立符合我国需求的元素汞溯源传递方法和形成元素汞发生器溯源传递能力提供借鉴。
Overviewing the method of prime traceability and delivery on element mercury generator from the NIST in USA.USA NIST uses ID ICP/MS method to calculate the candidate mercury generator output concentra-tion,it adds known high pure 201 Hg0 gas to candidate element mercury generator output calibration gas,then abun-dance of the spiked isotope 201 Hg will be changed,the abundance ratio of 201 Hg/202 Hg will be measured by ICP/MS.This process completes mercury traceability which is from the prime SRM3133 to 201Hg2 +solution concen-tration,and from 201 Hg2 + solution concentration to element mercury generator.This method is for the vender prime to trace to NIST prime,it is good for us to establish the element mercury generator traceability method and capacity which is suitable for Chinese requirement.
大气压介质阻挡放电(DBD)可以在常压下产生非平衡等离子体,已经成为热点研究领域.通过脉冲或交变电源激发放电,研究电源输出特性、电源与放电发生器负载间的匹配和外界条件对放电的影响对于理解放电现象和提高放电效率具有重要意义.本文采用Lissajous图形法,分别研究了驱动电压、气流速率等因素影响同轴DBD发生器介质层等效电容及负载幅频特性的规律.结果表明,气流速率和驱动电压等外界条件影响DBD发生器的负载特性:介质层等效电容随气流速率增大而减小,随驱动电压增大而增大;幅频特性曲线均表现出RLC回路谐振现象,谐振频率随气流速率增大而增大,随驱动电压增大而减小.通过对比发现,介质层等效电容随频率的变化曲线与幅频特性曲线具有一致的特征,介质层等效电容是影响电路谐振频率动态变化的主要因素.提出了一种有关介质层等效电容的形成机制.
Dielectric barrier discharge (DBD) can produce non-equilibrium plasma at atmospheric pressure, and it has become a hot point in recent years. For the DBD excited by pulsed or alternated currents, the effects of the loading performance of power supply, the matching between supply and discharge reactor and the discharge phenomena on its discharge are interesting issues. The studies of these issues are of great importance for understanding the DBD processes and improving the power supply efficiency. In this paper, the Lissajous figures of a DBD reactor with coaxial electrode configuration are measured. The loading performance of the DBD reactor and the dependences of excitation voltage and air flow rate on the dielectric layer equivalent capacitance are studied in atmospheric air. According to the experimental data and circuit modeling analysis, it is proved that the dielectric layer capacitance decreases with the increase of air flow rate, but increases with the increase of excitation vo

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传统的增升装置设计受到各种约束条件的限制,难以充分发挥增升效果,甚至无法达到飞机对增升效果的需求,而流动控制技术可以弥补这些缺陷。通过搜集大量文献,阐述了襟翼涡流发生器、主翼后缘偏折技术、ZHU’s襟翼、自激励运动襟翼、零质量射流、等离子体技术、MEMS技术以及动力增升等各类主动控制技术的工作原理,增升效果分析以及具体应用情况等。结果表明,这些流动控制新技术对于进一步提高民用飞机的增升效果具有巨大的潜力。
Conventional high-lift devices design is limited by many factors, so lift enhancing can not be obtained sufficiently, and then, it can not meet request on lift enhancing of aircraft. However, flow control can make up the shortage. In this paper, many kind of flow control is introduced from work principle, lift enhancing efficiency and the application by consulting much information. The flow control includes vortex generators on flap, spoiler deflec-ted, ZHU''s flap, self-activated movable flap, zero mass actuation, plasma actuators, MEMS technique, dynami-cal lift enhancing, and so on. The analysis results indicate that these flow control technique has great potential for improving lift enhancing efficiency of civil aircraft.

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