143 resultados para internal target

em Chinese Academy of Sciences Institutional Repositories Grid Portal


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介绍了兰州重离子加速器冷却储存环(HIRFL-CSR)的实验环(CSRe)团簇内靶装置控制系统的设计。该内靶系统由多种设备构成,包括喷嘴测温与加热控制子系统、真空与阀门监测/控制子系统、分子泵监测与控制子系统、数据处理与流程软件子系统等部分。该系统在内靶实验中工作状态良好,满足了内靶实验的需求。在该控制系统的支持下,2010年1月第一轮辐射电子俘获物理实验顺利完成。

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介绍了国家重大科学工程项目——兰州重离子加速器冷却存储环(HIRFL-CSR)的实验环(CSRe)团簇内靶温度闭环控制器的设计。该控制器给气体喷嘴处测温电阻提供长时间稳定度为0.1%的1mA恒定电流,通过12位ADC得到喷嘴温度,并通过混合信号处理器MSP430F149来实现制冷/加热闭环操作。在多种不同实验气体的情况下,该控制器的温度控制精度小于0.5K。目前,该控制器在现场工作良好。

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Pellet target is one of the main candidate targets in CSRm (cooler storage ring’s main ring) for hadron physics studies. Pellet speed is an important physical parameter for the target. Larger pellet speed could shorten the interacting time interval between the pellet and the cyclotron beam, and thus results in a small temperature variation for the pellet. This could make the pellet facility work in a stable condition. A fluid dynamic simulation was carried out for the pellet speed, and it was found that the maximum speed for the target pellet may be restricted to about 100 m/s even if all working parameters were set to their optimal values.

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Pellet target is one of the main candidate targets in CSRm (cooler storage ring’s main ring) for hadron physics studies. Pellet speed is an important physical parameter for the target. Larger pellet speed could shorten the interacting time interval between the pellet and the cyclotron beam, and thus results in a small temperature variation for the pellet. This could make the pellet facility work in a stable con-dition. A fluid dynamic simulation was carried out for the pellet speed, and it was found that the maxi-mum speed for the target pellet may be restricted to about 100 m/s even if all working parameters were set to their optimal values.

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A new gas delivery system is designed and installed for HIRFL-CSR cluster target. The original blocked nozzle is replaced by a new one with the throat diameter of 0.12mm. New test of hydrogen and argon gases are performed. The stable jets can be obtained for these two operation gases. The attenuation of the jet caused by the collision with residual gas is studied. The maximum achievable H-2 target density is 1.75x10(13) atoms/cm(3) with a target thickness of 6.3x10(12) atoms/cm(2) for HIRFL-CSR cluster target. The running stability of the cluster source is tested both for hydrogen and argon. The operation parameters for obtaining hydrogen jet are optimized. The results of long time running for H-2 and Ar cluster jets look promising. The jet intensity has no essential change during the test for H-2 and Ar.

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An internal target experiment at HIRFL-CSRm is planned for hadron physics, which focuses on hadron spectroscopy, polarized strangeness production and medium effect. A conceptual design of Hadron Physics Lanzhou Spectrometer (HPLUS) is discussed. Related computing framework involves event generation, simulation, reconstruction and final analysis. The R&D works on internal target facilities and sub-detectors are presented briefly.

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CSR, a new accelerator project under the construction. to upgrade the existing heavy ion cyclotron system in Lanzhou, is a double cooling-storage-ring system. It consists of a main ring and an experimental ring. The heavy ion beams from the cyclotron system will be accumulated and accelerated first in the main ring, then extracted to produce radioactive ion beams or high-Z beams, and finally to be send to the second ring for internal-target experiments.

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兰州CSRm内靶终端是进行强子物理实验的平台,可开展奇异介子产生和衰变的研究、重子谱的研究、多夸克态的研究及介子介质效应和手征对称破缺与恢复等多方面的研究。这些物理目标都需要内靶实验终端提供足够多的事件率,并能进行准确的径迹构建。在众多候选的内靶装置中,小丸靶具有其它内靶所欠缺的优点,如可以获得与外靶实验相比拟的实验亮度,可以配置4π立体角的探测器单元等。因此,小丸靶被确定为CSRm内靶实验终端中的主要内靶之一。小丸内靶(Pellet Internal Target)就是将氦以外的某种气体通过低温冷却而形成的固体微球。小丸内靶靶束与储存环离子束在反应室正交并发生相互作用,其反应事例被反应室周围环绕的探测器单元探测到并被记录下来。这篇论文对小丸内靶装置的结构进行了简要的介绍,并对小丸在反应室内的热力学行为进行了模拟。计算表明,靶丸速度是影响靶丸在反应区正常运行的重要因素之一。靶丸速度越大,靶丸在反应室内爆炸的可能性越小。通过对小丸的速度进行的流体动力学分析,发现即使对所有实验条件进行优化,小丸内靶的速度至多能达到100 m/s左右

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束流储存寿命对于储存环的建造和内靶实验都是一个很重要的参数。由于重离子冷却储存环工程的优化,HIRFL-CSR主环将能提供2.SGev的质子束流,这为强子物理研究提供了一个很好的平台。设计并建立一套针对强子物理的内靶系统己经列入到计划当中,与内靶相关的束流储存寿命研究也随之展开。本论文首先分析了在内靶实验中束流储存寿命的影响因素,即真空管道中的残余气体分子、冷却电子束和内靶,以及束内散射和集体效应等,并用理论解析和数值计算的方法,对各种因素的影响程度进行估算。研究表明,内靶散射影响下的束流储存寿命比其他因素导致的短2~3个数量级,内靶是影响束流寿命的决定性因素。其次,对CSRm将来实验中主要用到的Pelle七内靶和碳薄膜靶做了简要介绍,并计算了它们的有效靶厚大约为lx10、切ms/cmZ和5火1017atoms/CmZ。再者,用理论推导方法,对内靶的多次库仑散射和束流能量损失扰动对束流的影响进行了研究,推导了束流的横向和纵向发射度增长与束流每次打靶产生的小库仑散射角均方值气s和相对动量分散气了:之间的关系,并通过数值计算的方法给出了CSRm内靶实验条件的发射度增长曲线。最后,建立了内靶散射的MOnte-Carlo模拟程序,在模拟数据的基础上,总结研究束流的发射度增长规律,以及束流存储寿命与内靶厚度和束流能量的关系。计算表明,当存在Pellet靶(1、1016atoms/cm2)和c膜(5*1017 atoms/cmZ)时,2800Mev质子束的束流储存寿命分别为397秒和0.7秒,将来的内靶实验亮度大约为2 x 1033cm-2·s-1。

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HIRFL-CSRe的内靶有两种工作模式:团簇靶模式和原子束极化靶模式,团簇靶用于为实验环内的物理实验提供厚度为1011-1013 atoms/cmZ的氮、J隋性气体和甲烷等小分子的气体薄靶。本工作主要是进行兰州重离子冷却储存环实验环团簇内靶的建设,完成了团簇内靶的安装和准直、真空测试、温度测试、流量刻度、抽速刻度以及运行稳定性测试等工作,并去得了一些结果。总体来看,除轻气体外,团簇内靶的整体指标(靶厚和真空)达到了设计要求,对轻气体尚需进行改进。尚需优化的两个方面:1)解决喷嘴堵塞问题。除了液氮之外,采用其它靶气体源都出现了喷嘴堵塞现象,这个问题直接影响到团簇靶的正常运行;2)对于较轻的气体,如Ne和H:,获得的靶厚较小或者没有,而且各级的真空较差。经过分析,认为喷嘴堵塞的原因有两个方面,一是靶气体本身含有杂质,二是外界杂质。由于喷嘴级的分子泵对于轻气体没有足够的抽速和压缩比,不能将残余轻气体及时抽走,从而导致真空较差,当还没有获得有效靶厚时,团簇源第一级真空腔体的气压已经超过分子泵的工作气压了,因而对H:未获得有效靶厚。对于以上两个问题,我们采取了两项措施:1)设计加工了气体纯化装置,采用制冷与过滤相结合的方法对充入系统的气体进行预先纯化,该装置己完成加工,即将进行实验;2)优化抽气系统,增大团簇源第一级对轻气体的抽速和压缩比。

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In order to monitor multiple protein reaction processes simultaneously, a biosensor based on imaging ellipsometry operated in the total internal reflection mode is proposed. It could be realised as an automatic analysis for protein interaction processes with real-time label-free method. Its principle and methodology as well as a demonstration for its applications are presented.

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Based on the internal variable theory, a viscoelastic constitutive model of a highly deformable continuous medium is proposed. A set of second rank tensorial internal state variables corresponding to Biot's strain is introduced, and a nonlinear evolution

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In this paper, TASCflow3D is used to solve inner and outer 3D viscous incompressible turbulent flow (R-e = 5.6 X 10(6)) around axisymmetric body with duct. The governing equation is a RANS equation with standard k-epsilon turbulence model. The discrete method used is a finite volume method based on the finite element approach. In this method, the description of geometry is very flexible and at the same time important conservative properties are retained. The multi-block and algebraic multi-grid techniques are used for the convergence acceleration. Agreement between experimental results and calculation is good. It indicates that this novel approach can be used to simulate complex flow such as the interaction between rotor and stator or propulsion systems containing tip clearance and cavitation.