DOE's Oakland Office to Close by End of 2004, Operations Will Shift To

Total Page:16

File Type:pdf, Size:1020Kb

DOE's Oakland Office to Close by End of 2004, Operations Will Shift To -0 Lam 0 fit U- fc Secretary Abraham Sends a Warm The Green Gets a Needed UPqIrade Thank you for an Enjoyable Visit ByShawna -a- Williams SLAC employees on their way Djrect pI,.e.Sr t r in. to and from the Cafeteria OFF:JCIAL IES^-° le-70 \~~~~~ ,^ may notice construction StanfAor ll ~a e,.. 2 Ad work on The Green over the as'^ -- "" next few months. gt4.u;..? Cli 275WdH rna 9402 The goal is to repair leaks in (Ulu2 L-as the irrigation cn system, "which ro cause a bog-type 0>I 1 1 1 effect," said 8 53 1,* I l tl t 1 | St 1 t ** * t ;" ...... U~~~lliili~~~~l""'"""'" ~~~.............. B * &-Z Liam Robinson, 0JJ facilities support -CJ- for manager Stan Namura (left) and Vicente Garnica look on as Angel ^O=Ke 'ILA-1M 9-%titthntc^Eb~wrAIMu lnt ur cr-Nr-x Site Engineering Martinez digs an irrigationtrench on The Green. All are WASHINGTON, D.C. 20585 and Maintenance employees of SLAC's landscaping contractor. (SEM). replace the one that died and was cut January 7, 2003 "The area may not be usable for the down. The irrigation repairs would next three months, but it will improve make a new tree's survival more the usability for the next 10 or 20 likely, since cork oak thrives in drier years," Robinson said, adding that Dr. Jonathan Dorfan soil. pedestrians should exercise caution Director on The Green in the next few months. For more information on this project, Stanford Linear Accelerator Center contact: Liam Robinson (SEM), Ext. 2575 Sand Hill Road Planners are also exploring the 2980, [email protected] 0 Menlo Park, California 94025 possibility of planting a cork oak to Dear Jonathan: DOE's Oakland Office to Close by Just a short note to thank you for making my visit to End of 2004, Operations Will Shift the Stanford Linear Accelerator Center (SLAC) successful. I appreciated your kind introduction to the to New Service Center packed all-hands meeting that you and your staff put together. Also, your tour through the SLAC was By Neil Calder extremely interesting and informative. The DOE recently announced that they will close the Oakland National I am impressed with the operation of SLAC and its Nuclear Security Administration contribution to fundamental science and to advances (NNSA) Service Center as part of a in technology that have come from that fundamental reorganization. We sat down with science research. John Muhlestein, head of DOE's Stanford Site Office, for more details Again, I appreciate the hard work of you and your on this upcoming change. staff. I look forward to a return visit. What has changed in the Sincerely, Department of Energy's organization n-V in the Bay Area? 0 0' "On December 17, 2002, DOE's 5I >c NNSA, which oversees the Bay ro 1) Area's Lawrence Livermore National Spencer Abraham n Laboratory and Sandia National 0 Laboratories, implemented a new House Science Committee Staff organizational structure, with John Muhlestein, head of DOE's Office Visits SLAC Albuquerque becoming the main of Science Stanford Site Office. Service Center." usual until transition plans have been "This new structure will streamline established and implementation of operations and oversight while links with the new Service Center has clarifying roles and responsibilities. begun. I will make sure that everyone A direct consequence of this at SLAC is kept fully informed of reorganization is that the DOE's developments."@ Oakland Service Center, which provides our Office of Science Stanford Site Office with a wide range of services, will close by the end of 2004." a/) How will these changes affect 0) 0 0: SLAC? co cd ro "SLAC staff should be reassured that there will be no sudden changes. We -0 0 4-(- still expect to get support from the 0 -C CL Oakland Service Center during the two years of transition. Members of the House Science Committee Staff, Gabe Rozsa, Tina Kaarsberg, Charlie Cook and Chris King, toured SSRL as part of their January 13 visit to SLAC. As an We do not yet know which center example of the kind of biological puzzles that can be examined with SSRL's technical will take over responsibility for capabilities, Linda Brinen (SSRL), far right, shows the visitors the molecular structure SLAC support, but it is business as of the anthrax lethal factor. New Gate House to be Built at MFD & Klystron Departments SLAC Main Gate Specialize in Hydrogen Brazing ff 0 0 By Kelley Ranlsey i) 0 A particularly unique technology Ol used in the Mechanical Fabrication 0 I (MFD) and Klystron and Microwave (KLY) departments is ultra-clean, C E:3 high temperature hydrogen furnace -c brazing. Hydrogen brazing is an essential .) C assembly technique for joining u components and assemblies for Ir V) critical ultra high vacuum (UHV) systems such as klystrons and This design sketch shows the nrew Gate House for the SLAC Main Gate. accelerator structures. By Shawna Williams Construction should begin on the In hydrogen brazing, a metallurgical new building in late February, Say goodbye to the old guard shack bond is achieved using a filler-metal around the time the current work at SLAC's Main Gate. It will be torn having a lower melting point than on extending utilities to the new down and replaced in the next few the materials being joined. One of the guest house will be completed. The months. primary benefits of brazing is that building should take two to three the mating surfaces form a complete "The guard house that's there now months to complete. A temporary metallurgical joint. When heated in Derrik Soares (MFD) lifts the furnace has a huge leak problem," explained shack will be set up further down the pure hydrogen atmosphere, the heating elemtent off a red hot retort. Rick Yeager, Manager of Labratory the hill from the current one, and filler-metal melts, wets the surfaces Safeguards/Security. "It's old, it's traffic lanes at the main entrance will to be joined, and is drawn between carbon steel, molybdenum, Glidcop, outdated, there are holes in the probably be narrower. the mating surfaces by capillary Kovar and metallized alumina. The wall-it doesn't look nice." Yeager said hours at the Alpine action. The result is a high quality, filler metal is usually an alloy of The spacious new Main Gate House, Gate might be extended during the permanent metallurgical seal. copper and gold, but other alloys containing silver, nickel, indium, in addition to being more comfortable construction. Check the Web and With other joining techniques such palladium, and other metals are and attractive, will allow for the posted signs for further information as welding or mechanical seals, often used. The brazing process installation of a modern fire alarm on Alpine Gate hours. a unbounded mating surfaces can trap takes place in a specially designed system that relays more information contaminants, are difficult to out- furnace that employs controlled to firefighters. gas and can cause problems with heating cycles in the range between UHV systems. In addition, the high 750 and 1100 degrees Celsius. The temperature pure hydrogen brazing New Signs Promote Safety brazing atmosphere is contained in a atmosphere has powerful cleaning cylindrical retort that can measure 36 effects. Oxides of metals such as 0 inches across and 10 feet in length. Ol copper, nickel, iron and chromium cn ro0w are readily reduced and eliminated, At the present time, this technology is 0pa) resulting in a bright clean surface. being used to assemble components 0: Many other contaminants are required for SSRL and the SPEAR3 0 volatilized and removed during the Upgrade, the Accelerator Department Q..0. n-' brazing process. Modified processes and NLC. We also do special brazing can be employed, such as the use work for other national labs and Alert commuters might have noticed a new yellow warning sign that of wet hydrogen. This method universities. appeared just beyond the Main Gate on January 22. This was one of eight is currently being used for final signs posted at SLAC entrances recently, part of the Lab's For more information on the ongoing effort to processing of high-gradient Next keep safety a priority in all our activities. Mechanical Fabrication Department, Linear Collider (NLC) test structures see: http://www.slac.stanford.edu/ The ES&H Coordinating Council (which encompasses all divisions) decided to reduce surface carbon. grp/mfd/ to post the signs to let visitors and contractors know that they should Many different materials can be be vigilant and inquire as to SLAC For more information on the Klystron safety issues with which they may joined by hydrogen furnace brazing. be unfamiliar. Employees and others in the SLAC community and Microwave Department, see: who have Most brazing at SLAC involves completed the appropriate ES&H training should already be aware of hazards http://wwvw.slac.stanford.edu/grp/ joining copper and/or stainless steel, here. kly/index.html 0 however other materials commonly For more information, contact: Rachel Claus (BSD), Ext. 4343, brazed at SLAC include nickel, iron, [email protected] 0 TYPES OF DETECTORS AND HOW of detectors. Ionizing detectors To avoid nuisance alarms place Smoke Detector THEY WORK respond slightly faster to flaming fires detectors: while photoelectric detectors respond Basics Ionization smoke detectors: *Away from furnace or air faster to smoldering fires. Ideally, a conditioner vents Find Out More About One of The ionization chamber smoke home should be protected by at least · Away from bathrooms to avoid the Most Important Devices detector has a small radiation source one of each.
Recommended publications
  • The Thermal Expansion of Some Common Linac Materials*
    Proceedings of LINAC2002, Gyeongju, Korea THE THERMAL EXPANSION OF SOME COMMON LINAC MATERIALS* R. Valdiviez, D. Schrage, H. Haagenstad, J. Szalczinger Los Alamos National Laboratory, Los Alamos, NM Abstract type of situation can occur during brazing operations of We have endeavored to acquire more precise data on linac structures. thermal expansion by employing a laser interferometry A thermal expansion measuring method with a precision based measuring process [1] rather than the vitreous silica high enough to avoid the high-temperature inaccuracy dilatometer methods that have been used traditionally. relative to the materials’ elevated temperature strength is a Given that all test parameters are controlled appropriately laser interferometry based method. ASTM E289 laser interferometry offers an accuracy that can be much describes an interferometry based method for measuring better than silica dilatometer based methods. The higher the thermal expansion of materials. In a laser precision method will give a more accurate measure of the interferometry based method the dilatometer is replaced response of some common linac materials undergoing by placing the sample in a fixture where the laser can thermal growth. interact with one end of the sample. Length changes can be measured to an accuracy that is primarily determined 1 INTRODUCTION by the half-wavelength of the laser being used. For the expansion measured in this testing effort the The thermal expansion of metal materials has a strong approximate precision per testing method is listed in effect in any linac design. Data covering the thermal Table 1. expansion of materials that are commonly used in linac fabrication is either sparse or contradictory.
    [Show full text]
  • Glidcop Brazing in Sirius' High Heat Load Front-End
    TUPE23 Proceedings of MEDSI2016, Barcelona, Spain GLIDCOP BRAZING IN SIRIUS’ HIGH HEAT LOAD FRONT-END COMPONENTS G. V. Claudiano, O. R. Bagnato, P. T. Fonseca, F. R. Francisco, R. L. Parise, L. M. Volpe LNLS, Campinas, Brazil Abstract their design on the state of the art. Taking Front-End Sirius is a 4th generation synchrotron light source in power absorbers as example: the refrigeration of these project. Some of Sirius’ beamlines will have a very high components is complex due to their reduced size allied to power density, more than 50 kW/mrad², to be dissipated the high thermal load that is irradiated on them [3]. To in components that have a limited space condition. Thus, solve this problem, engineered materials must be used. the refrigeration of these components is complex when The Glidcop is a good choice due to its good thermal one has in mind that the coolant flow cannot be too turbu- conductivity and preservation of mechanical properties lent in order to not induce much vibration in the compo- after heating cycles. The difficulty of this project lies on nents. the fact that dissimilar metal components (i.e. Glidcop Oxygen Free Copper (C10200) has been replaced by and stainless steel) must be joined and it is needed to the Glidcop on high heat load synchrotron applications isolate both the vacuum and the water chambers. Thus, due to its good thermal conductivity and preservation of the joint must be resistant to hold the pressure in the water mechanical properties after heating cycles. However, this chamber and must be tight to not allow the transport of material is not very workable in terms of union with other small atmosphere molecules to the vacuum chamber.
    [Show full text]
  • E-15798 Cover
    NASA/TM—2007-214663 Comparison of GRCop-84 to Other High Thermal Conductive Cu Alloys Henry C. de Groh III and David L. Ellis Glenn Research Center, Cleveland, Ohio William S. Loewenthal Ohio Aerospace Institute, Brook Park, Ohio February 2007 NASA STI Program . in Profile Since its founding, NASA has been dedicated to the • CONFERENCE PUBLICATION. Collected advancement of aeronautics and space science. The papers from scientific and technical NASA Scientific and Technical Information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or cosponsored by NASA. this important role. • SPECIAL PUBLICATION. Scientific, The NASA STI Program operates under the auspices technical, or historical information from of the Agency Chief Information Officer. It collects, NASA programs, projects, and missions, often organizes, provides for archiving, and disseminates concerned with subjects having substantial NASA’s STI. The NASA STI program provides access public interest. to the NASA Aeronautics and Space Database and its public interface, the NASA Technical Reports Server, • TECHNICAL TRANSLATION. English- thus providing one of the largest collections of language translations of foreign scientific and aeronautical and space science STI in the world. technical material pertinent to NASA’s mission. Results are published in both non-NASA channels and by NASA in the NASA STI Report Series, which Specialized services also include creating custom includes the following report types: thesauri, building customized databases, organizing and publishing research results. • TECHNICAL PUBLICATION. Reports of completed research or a major significant phase For more information about the NASA STI of research that present the results of NASA program, see the following: programs and include extensive data or theoretical analysis.
    [Show full text]
  • Creep Properties of an Extruded Copper–8% Chromium–4% Niobium Alloy
    Materials Science and Engineering A369 (2004) 101–111 Creep properties of an extruded copper–8% chromium–4% niobium alloy M.W. Decker, J.R. Groza, J.C. Gibeling∗ Department of Chemical Engineering and Materials Science, University of California, One Shields Avenue, Davis, CA 95616-5294, USA Received 23 June 2003; received in revised form 20 October 2003 Abstract Constant-stress creep experiments were conducted on extruded Cu–8 Cr–4 Nb (GRCop-84) from 0.57 to 0.79 Tm, with observed strain rates spanning over four orders of magnitude. GRCop-84 is composed of approximately 14 vol.% Cr2Nb distributed in sizes ranging from approximately 30 nm to 0.5 ␮m in a matrix of pure copper with a grain size of approximately 1–3 ␮m. This high-strength alloy exhibits creep curves with a standard pure metal-type appearance and true failure strains typically in excess of 10%. The Monkman–Grant relationship is obeyed with a slope of −1.08. Computation of activation energies between neighboring isotherms yields an average value of 287 ± 14 kJ/mol. Despite apparent power law creep behavior within an isotherm, a master plot of temperature compensated strain rate (ε˙/exp[−Q/RT]) versus temperature compensated stress (σ/G) demonstrates that most of the data are above power law breakdown, consistent with σ/G>˜ 10−3.A hyperbolic sine model facilitates interpolation on this master plot to stresses and/or temperatures where experimental data do not exist. Neither the threshold stress model nor the dislocation detachment model applies to GRCop-84 under these creep conditions.
    [Show full text]
  • Vacuum Materials
    Vacuum Science and Technology for Particle Accelerators Yulin Li Cornell University, Ithaca, NY Xianghong Liu SLAC National Accelerator Laboratory Albuquerque, New Mexico June 17-28, 2019 Table of Contents . Vacuum Fundamentals . Sources of Gases . Vacuum Instrumentation . Vacuum Pumps . Vacuum Components/Hardware . Vacuum Systems Engineering . Accelerator Vacuum Considerations, etc. Beam-vacuum interactions 2 SESSION 5: Vacuum Materials • Metals Stainless Steels Aluminum and Alloys Copper and Alloys Other metals • Non-metals Ceramics and Glasses Polymers 3 Stainless Steels – Classifications Stainless steel is a steel alloy with at least 11% chromium content by weight. It is also called corrosion-resistant steel. Austenitic stainless steel (300 series): These are generally non-magnetic steel alloys. They contain a maximum of 0.15% carbon, a minimum of 16% chromium and sufficient nickel and/or manganese to retain an austenitic structure at all temperatures from the cryogenic region to the melting point of the alloy. The low carbon (-L) grades are used when welding is involved. In UHV applications, especially accelerators, 300 stainless steels are commonly used. Other less used types of stainless steel alloys are: Martensitic stainless steels (400 series), precipitation-hardening martensitic stainless steels (most common used 17- 4PH) and ferritic stainless steels . Martensitic stainless steels are much more machinable, and are magnetic. Those are much less used for accelerators, mainly due to the magnetism. USPAS Vacuum (June
    [Show full text]
  • GLIDCOP, Subjected to Dynamic Loads: It Is a Composite Material with a Copper Matrix Strengthened with Aluminium Oxide Ceramic Particles
    ECCM15 - 15TH EUROPEAN CONFERENCE ON COMPOSITE MATERIALS, Venice, Italy, 24-28 June 2012 HIGH STRAIN-RATE MECHANICAL BEHAVIOUR OF A COPPER MATRIX COMPOSITE FOR NUCLEAR APPLICATIONS L. Peroni*, M. Scapin Politecnico di Torino, Department of Mechanical and Aerospace Engineering, Corso Duca degli Abruzzi, 24 – 10129 Turin, Italy *[email protected] Keywords: metal matrix composite, strain-rate, temperature, Johnson-Cook Abstract Aim of this work is the investigation of mechanical behaviour of an alumina dispersion strengthened copper, known by the trade name GLIDCOP, subjected to dynamic loads: it is a composite material with a copper matrix strengthened with aluminium oxide ceramic particles. Since the particle content is quite small the material keeps the OFE copper physical properties, such as thermal and electrical conductivity, but with a higher yield strength, like a mild-carbon steel. Besides, with the addition of aluminium oxide, the good mechanical properties are retained also at high temperatures and the resistance to thermal softening is increased: the second phase blocks the dislocation movement preventing the grain growth. Thanks to these properties GLIDCOP finds several applications in particle accelerator technologies, where problems of thermal management, combined with structural requirements, play a key role. Currently, it is used for the construction of structural and functional parts of the particle beam collimation systems of the Large Hadron Collider (LHC) at CERN. 1 Introduction The dispersion strengthened metal composites were studied [1] in order to achieve a combination of different material properties such as high thermal or electrical conductivity jointed with controlled thermal expansion, high strength, wear and arc erosion resistance and particular magnetic properties.
    [Show full text]
  • Friction Stir Welding of GR-Cop 84 for Combustion Chamber Liners
    Friction Stir Welding of GR-Cop 84 for Combustion Chamber Liners Carolyn K. Russell' and Robert Cartert NASA/MarshaN Space Flight Center, Huntsville, Alabama 35812 David L. Ellis: NASA/Glenn Research Center, Cleveland, Ohio 441 I I and Richard Goudys Spin Tech, Paso Robles, California 93446 GRCop-84 is a copper-chromium-niobium alloy developed by the Glenn Research Center for liquid rocket engine combustion chamber liners. GRCop-84 exhibits superior properties over conventional copper-base alloys in a liquid hydrogen-oxygen operating environment. The Next Generation Launch Technology program has funded a program to demonstrate scale-up production capabilities of GR-Cop 84 to levels suitable for main combustion chamber production for the prototype rocket engine. This paper describes a novel method of manufacturing the main combustion chamber liner. The process consists of several steps: extrude the GR-Cop 84 powder into billets, roll the billets into plates, bump form the plates into cylinder halves and friction stir weld the halves into a cylinder. The cylinder is then metal spun formed to near net liner dimensions followed by finish machining to the final configuration. This paper describes the friction stir weld process development including tooling and non-destructive inspection techniques, culminating in the successful production of a liner preform completed through spin forming. Nomenclature Copper-Chrome-Niobium friction stir weld pressure coefficient force coefficient in the x direction force coefficient in they direction chord time step Xcomponent of the resultant pressure force acting on the vehicle Y component of the resultant pressure force acting on the vehicle generic functions height time index during navigation waypoint index trailing-edge (TE) nondimensional angular deflection rate Aerospace Welding Engineer, Materials, Processes & Manufacturing, ED33.
    [Show full text]
  • North Carolina), Which Are Very Commonly Used in Synchrotron Components
    A Review of Thermo-Mechanical Considerations of High Temperature Materials for Synchrotron Applications Tuncer M. Kuzay* ' •' •«~ ? «/ :•• Experimental Facilities Division ' ^ 1993 Advanced Photon Source 0 ^ T A rgonne National Laboratory ' / 9700 South Cass Avenue Argonne, IL 60439 The third generation synchrotron facilities such as the 7-GeV Advanced Photon Source (APS) generate x-ray beams with very high heat load and heat flux levels. Certain front end and beamline components will be required to sustain total heat loads of 3.8 to 15 kW and heat flux levels exceeding 400 W/mm2 even during the first phase of this project. Grazing geometry and enhanced heat transfer techniques used in the design of such components reduce the heat flux levels below the 30 W/mm2 level, which is sustainable by the special copper materials routinely used in the component design. Although the resulting maximum surface temperatures are sustainable, the structural stresses and the fatigue issues remain viable concerns. Cyclic thermal loads have a propensity to cause spallation and thermal striping concerns. As such, the steady-state part of the problem is much easier to understand and handle than the time-dependent part. Ease of bonding as well as ultrahigh vacuum and radiation compatibility are additional constraints on material selection for these components. The two copper materials are the traditional OFHC and the newer sintered copper, Glidcop (a trademark product of the SCM Corporation of North Carolina), which are very commonly used in synchrotron components. New materials are also appearing in the form of heat sinks or heat spreaders that are bonded to the base copper in some fashion.
    [Show full text]
  • Glidcop Brazing in Sirius' High Heat Load Front-End Components
    Glidcop Brazing in Sirius’ Front-End High Heat Load Components G. V. Claudiano, R. L. Parise, L. M. Volpe, P. T. Fonseca, F. R. Francisco and O. R. Bagnato [email protected] – Brazilian Synchrotron Light Laboratory - LNLS ABSTRACT Currently under construction, Sirius is a 3 GeV, fourth generation synchrotron light source. Sirius is designed to have up to 37 beamlines with ultra-low emittance and high brightness, which will allow high-level research and development on a large range of areas as structural biology, materials science and nanoscience. Given its high quality, its components rely on fine requirements on size, safety and cooling capability, having their design on the state of the art. Taking Front-End power absorbers as example: the refrigeration of these components is complex due to their reduced size allied to the high thermal load that is irradiated on them. To solve this problem, engineered materials must be used. The Glidcop is a good choice due to its good thermal conductivity and preservation of mechanical properties after heating cycles. The difficulty of this project lies on the fact that dissimilar metal components (i.e. Glidcop and Stainless Steel) must be attached and it is needed to isolate both the vacuum and the water chambers. Thus, the joint must be resistant to hold the pressure in the water chamber and must be tight to not allow the transport of small atmosphere molecules to the vacuum chamber. As a trial to manufacture these components, given its specific features, the brazing was chosen as a joining process. THE COMPONENTS The photon shutter component (shown on isometric view at the left and on half section view on the right) is one of the power absorbers which will be built by this brazing process.
    [Show full text]
  • Glidcop [5] and Oxygen-Free Copper (OFC) Are Used to Build the Structures of These Components
    LS-204 rTh~ubmjtted manuscript has been authored I by a CO~ltractor of the U. S. Government under contract No. W-31-109-ENG-38. IAccordingly. the U. S. Government retains a ,nonexclusive, royalty-free license to publish or reproduce the published form of this contribution, or allow others to do so, for I. I). S. Government purposes. Thermo-Mechanical Optimization of Fixed Mask 2 for APS Front Ends H. L. T. Nian, T. M. Kuzay, and I. C. A. Sheng July 27, 1992 Experimental Facilities Division Advanced Photon Source Argonne National Laboratory Thermo-Mechanical Optimization of Fixed Mask 2 for APS Front Ends H. L. Thomas Nian, Tuncer M. Kuzay, and 1. C. Albert Sheng Argonne National Laboratory 9700 S. Cass Ave., Argonne, IL 60439 Abstract Fixed mask 2 (FM2) is one of the critical elements on the front end of the beamlines at the Advanced Photon Source (APS) now under construction at Argonne National Laboratory (ANL). The FM2 uses an enhanced heat transfer tube developed at ANL. Due to large thermal loads on these components, inclined geometry is used in the design to spread the footprint ofthe x-ray beam. Even then, thermal loads are very critical. To address the thermal and thermo-mechanical issues, analytical studies have been applied to a simplified model of the FM2 tube. The maximum temperature and maximum effective stress have been parametrically studied. Results for maximum temperatures and stresses are obtained and compared with the available strength/fatigue data for the materials proposed for the fixed mask design. 1 Introduction Fixed Mask 2 (FM2) is one of the critical elements on the insertion device (ID) front end [1] of the beamlines at the Advanced Photon Source (APS) now under construction at Argonne National Laboratory (ANL).
    [Show full text]
  • The Use of Dispersion-Strengthened Copper in Accelerator Designs*
    XX International Linac Conference, Monterey, California THE USE OF DISPERSION STRENGTHENED COPPER IN ACCELERATOR DESIGNS* R. Valdiviez, D. Schrage, F. Martinez, W. Clark Los Alamos National Laboratory, Los Alamos, NM Abstract The Spallation Neutron Source (SNS) project RFQ accelerator utilizes a combined OFE and Glidcop cavity Dispersion strengthened copper, known by the trade wall design [4]. The Accelerator Production of Tritium name GLIDCOP[1], has found various applications in (APT) project’s Low Energy Demonstration Accelerator accelerator designs. Glidcop has material properties (LEDA) RFQ accelerator utilizes Glidcop in the design similar to OFE copper, such as thermal and electrical of several key components [5]. The end-sealing flanges, conductivity. Unlike OFE, however, Glidcop has yield coupling plates, end walls, and vacuum-waveguide and ultimate strengths equivalent to those of connections [6] all utilize Glidcop. To date the LEDA mild-carbon steel, making it a good structural material. RFQ has operated for over two-thousand hours under This paper covers some accelerator components RF power high duty factor or CW mode with no failures fabricated with Glidcop, material properties measured due to material yield or rupture. The RFQ fabrication from room to brazing temperatures, and a also utilized Glidcop for the braze tooling needed to furnace-brazing process that has produced good, support components during brazing. consistent results with Glidcop. During the commissioning of the LEDA RFQ multipacting was found to occur in the tapered-vacuum waveguides at certain RF power levels that were very close to the operating power level. The solution used to 1 INTRODUCTION overcome this was to reduce the number of RF feeds into the RFQ by half.
    [Show full text]
  • Brazing of Mo to Glidcop Dispersion Strengthened Copper for Accelerating Structures
    materials Article Brazing of Mo to Glidcop Dispersion Strengthened Copper for Accelerating Structures Valentina Casalegno 1,*, Sergio Perero 1 , Monica Ferraris 1, Mauro Taborelli 2, Gonzalo Arnau Izquierdo 2, Stefano Sgobba 2 and Milena Salvo 1 1 Applied Science and Technology Department, Institute of Materials Physics and Engineering, Politecnico di Torino, I-10129 Torino, Italy; [email protected] (S.P.); [email protected] (M.F.); [email protected] (M.S.) 2 CERN European Organization of Nuclear Research, CH-1211 Geneva, Switzerland; [email protected] (M.T.); [email protected] (G.A.I.); [email protected] (S.S.) * Correspondence: [email protected]; Fax: +39-011-564-4699 Received: 18 July 2018; Accepted: 27 August 2018; Published: 7 September 2018 Abstract: Alumina dispersion-strengthened copper, Glidcop, is used widely in high-heat-load ultra-high-vacuum components for synchrotron light sources (absorbers), accelerator components (beam intercepting devices), and in nuclear power plants. Glidcop has similar thermal and electrical properties to oxygen free electrical (OFE) copper, but has superior mechanical properties, thus making it a feasible structural material; its yield and ultimate tensile strength are equivalent to those of mild-carbon steel. The purpose of this work has been to develop a brazing technique to join Glidcop to Mo, using a commercial Cu-based alloy. The effects of the excessive diffusion of the braze along the grain boundaries on the interfacial chemistry and joint microstructure, as well as on the mechanical performance of the brazed joints, has been investigated. In order to prevent the diffusion of the braze into the Glidcop alloy, a copper barrier layer has been deposited on Glidcop by means of RF-sputtering.
    [Show full text]