10,413 research outputs found

    SRF Cavity Fabrication and Materials

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    The technological and metallurgical requirements of material for highgradient superconducting cavities are described. High-purity niobium, as the preferred metal for the fabrication of superconducting accelerating cavities, should meet exact specifications. The content of interstitial impurities such as oxygen, nitrogen, and carbon must be below 10{\mu}g/g. The hydrogen content should be kept below 2{\mu}g/g to prevent degradation of the Q-value under certain cool-down conditions. The material should be free of flaws (foreign material inclusions or cracks and laminations) that can initiate a thermal breakdown. Defects may be detected by quality control methods such as eddy current scanning and identified by a number of special methods. Conventional and alternative cavity fabrication methods are reviewed. Conventionally, niobium cavities are fabricated from sheet niobium by the formation of half-cells by deep drawing, followed by trim machining and Electron-Beam Welding (EBW). The welding of half-cells is a delicate procedure, requiring intermediate cleaning steps and a careful choice of weld parameters to achieve full penetration of the joints. The equator welds are particularly critical. A challenge for a welded construction is the tight mechanical and electrical tolerances. These can be maintained by a combination of mechanical and radio-frequency measurements on halfcells and by careful tracking of weld shrinkage. The established procedure is suitable for large series production. The main aspects of quality assurance management are mentioned. Another cavity fabrication approach is slicing discs from the ingot and producing cavities by deep drawing and EBW. Accelerating gradients at the level of 35-45 MV.m-1 can be achieved by applying Electropolishing (EP) treatment....Comment: 37 pages, contribution to the CAS-CERN Accelerator School: Superconductivity for Accelerators, Erice, Italy, 24 April - 4 May 2013, edited by R. Baile

    Ancient and historical systems

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    Coefficient of thermal expansion of nanostructured tungsten based coatings assessed by thermally induced substrate curvature method

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    The in plane coefficient of thermal expansion (CTE) and the residual stress of nanostructured W based coatings are extensively investigated. The CTE and the residual stresses are derived by means of an optimized ad-hoc developed experimental setup based on the detection of the substrate curvature by a laser system. The nanostructured coatings are deposited by Pulsed Laser Deposition. Thanks to its versatility, nanocrystalline W metallic coatings, ultra-nano-crystalline pure W and W-Tantalum coatings and amorphous-like W coatings are obtained. The correlation between the nanostructure, the residual stress and the CTE of the coatings are thus elucidated. We find that all the samples show a compressive state of stress that decreases as the structure goes from columnar nanocrystalline to amorphous-like. The CTE of all the coatings is higher than the one of the corresponding bulk W form. In particular, as the grain size shrinks, the CTE increases from 5.1 106^{-6} K1^{-1} for nanocrystalline W to 6.6 106^{-6} K1^{-1} in the ultra-nano-crystalline region. When dealing with amorphous W, the further increase of the CTE is attributed to a higher porosity degree of the samples. The CTE trend is also investigated as function of materials stiffness. In this case, as W coatings become softer, the easier they thermally expand.Comment: The research leading to these results has also received funding from the European Research Council Consolidator Grant ENSURE (ERC-2014-CoG No. 647554

    Ultrasound metrology and phantom materials for validation of photoacoustic thermometry

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    High intensity focused ultrasound is an emerging non-invasive cancer therapy during which a focused ultrasound beam is used to destroy cancer cells within a confined volume of tissue. In order to increase its successful implementation in practice, an imaging modality capable of accurately mapping the induced temperature rise in tissue is necessary. Photoacoustic thermometry, a rapidly emerging technique for non-invasive temperature monitoring, exploits the temperature dependence of the Grüneisen parameter of tissues, which leads to changes in the recorded photoacoustic signal amplitude with temperature. However, the implementation of photoacoustic thermometry approaches is hindered by a lack of rigorous validation. This includes both the equipment and methodology used. This work investigates the effect of temperature on ultrasound transducers used in photoacoustic thermometry imaging as well as characterisation of potential phantom materials for its validation. The variation in transducer sensitivity with temperature is investigated using two approaches. The first one utilises a reference transducer whose output power is known as a function of temperature to characterise the sensitivity of the hydrophone. As the knowledge of variability of transducer output with temperature is not readily available, two standard metrology techniques using radiation force balances and laser vibrometry are extended beyond room temperature to characterise the effect of temperature on the output of PZT tranducers. For the second approach to transducer sensitivity calibration, a novel method is developed utilising water as a laser-generated ultrasound source and validated using the self-reciprocity calibration method. The calibrated hydrophone is then used to characterise the relevant temperature-dependent properties of several phantom materials in a custom-built setup. The measurement results are used to determine the most suitable phantom for photoacoustic thermometry. Finally, the phantom is heated and imaged in a proof-of-concept photoacoustic thermometry setup using a linear array. These contributions are of vital importance for allowing the translation of photoacoustic thermometry into clinical practice

    Fusion energy for space missions in the 21st century: Executive summary

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    Future space missions were hypothesized and analyzed, and the energy source of their accomplishment investigated. The missions included manned Mars, scientific outposts to and robotic sample return missions from the outer planets and asteroids, as well as fly-by and rendezvous missions with the Oort Cloud and the nearest star, Alpha Centauri. Space system parametric requirements and operational features were established. The energy means for accomplishing missions where delta v requirements range from 90 km/sec to 30,000 km/sec (High Energy Space Mission) were investigated. The need to develop a power space of this magnitude is a key issue to address if the U.S. civil space program is to continue to advance as mandated by the National Space Policy. Potential energy options which could provide the propulsion and electrical power system and operational requirements were reviewed and evaluated. Fusion energy was considered to be the preferred option and was analyzed in depth. Candidate fusion fuels were evaluated based upon the energy output and neutron flux. Additionally, fusion energy can offer significant safety, environmental, economic, and operational advantages. Reactors exhibiting a highly efficient use of magnetic fields for space use while at the same time offering efficient coupling to an exhaust propellant or to a direct energy convertor for efficient electrical production were examined. Near term approaches were identified. A strategy that will produce fusion powered vehicles as part of the space transportation infrastructure was developed. Space program resources must be directed toward this issue as a matter of the top policy priority
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