sns hyspec beamline 14b technical discussion
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SNS HYSPEC (Beamline 14B) Technical Discussion September 2012 David C. Anderson Melissa Harvey HYSPEC Timeline CD0 (Mission Need) in May 2003 Mark Hagen hired as Lead Scientist in 2003 CD1 (Preliminary Baseline Range) in April 2004


  1. SNS HYSPEC (Beamline 14B) Technical Discussion September 2012 David C. Anderson Melissa Harvey

  2. HYSPEC Timeline • CD0 (Mission Need) in May 2003 • Mark Hagen hired as Lead Scientist in 2003 • CD1 (Preliminary Baseline Range) in April 2004 • Engineering began on HYSPEC in 2004, when Bill Leonhardt was hired to be the lead engineer for the instrument • Work continued at Brookhaven National Laboratory (BNL) until June 2005, when Mark Hagen relocated to oak Ridge • CD2 (permission to proceed into detailed design) achieved in October 2005 • CD3 (procurement phase) in 2006 • Anderson replaces Leonhardt as Lead Engineer in April 2008 • CD4 (Project Complete) in August 2011 2 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  3. Beamline Components CVI BSI Detector 6-15m Shielding Shutter Vessel Insert Chopper Box B Drum Shield + Shielding Focusing Crystals 15-33m Shielding Chopper Box A + Curved Guide T0 chopper Drum Shield Chopper Box B T1a disk chopper to Sample Arm T1b disk chopper + Sample Stage T2 Fermi chopper Secondary shutter 3 He Polarization Analyzer Isolation valve 3 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  4. Shielding Drum Shield is made from High Density Concrete, Lead and B 4 C Chopper Box B Shielding 6~15m Stacked 15~33m Shielding • Shielding is qualified Shielding 6~15m Shielding is both Seismically and all High Density Concrete HDC by Neutronics Analysis 15~33m and Chopper Box B Shield is regular weight concrete except for 1 block next to the drum shield 6~15m Poured in Place (PIP) Shielding Borated Panel Shielding (Borated Polyethylene with Aluminum skins, Roll Up Door painted with B4C loaded paint) Shielding   Total dose (mrem/hr) 0.01 0.1 0.25 0.5 1 3 10 100 1000 -600 -400 -200 Y (cm) 0 200 400 600 0 200 400 600 800 1000 1200 1400 1600 1800 Z, beam direction (cm) 4 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  5. SNS Standardized Shielding Design • HYSPEC Shielding construction follows the SNS Standard Design Friction Connections for Stacked Shielding Blocks Boss (if used) Tapped Hole 1” -8 UNC for Tie-Down Rod Anchor 1” -8 UNC - counterbore 2-1/4" dia x 1" deep Steel Tie- Leveling Screw Down Plate 1" Recommended Grout Thickness 1/2" Minimum Grout Thickness Poured-in- under Boss (if Place used) Concrete Tie-Down Details for Stacked Shielding Blocks Mounted on Poured-in-Place Shielding • 7.0 STANDARDIZATION OF MECHANICAL COMPONENTS 5 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  6. SNS Standardized Shielding Design Guide Tubes for Hold-down Rods and Nuts – perpendicularity to be 1/16” Nelson studs Horizontal Tension Rod Steel Encasement sides removed for clarity Typical Steel-Encased Concrete Shielding Block (Swift-Lift Option) – Alternate Method of Construction – reinforcing bar omitted for clarity VULC0752M8U8707A012-1 Three tapped lifting Stiffener panels holes – location to be determined by CG of assembly Guide Tubes for Hold- Steel “can” (exterior surfaces down Rods and Nuts – painted or plated as required perpendicularity to be by Neutron Physics) 1/16” Typical Steel-Encased Concrete Shielding Block (Swivel Hoist Ring Option) – Preferred Method of Construction – Nelson studs omitted for clarity SING0350M8U8703A020-1 6 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  7. Upstream Optics • Procured and installed very early in the Project CORE VESSEL INSERT Shutter Insert BULK SHIELD INSERT 7 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  8. Choppers and Beam Guide • Vertical axis T0 Chopper procured from SKF Magnetic, operates at 30Hz and 60Hz • Upstream Disk Chopper operates at 60Hz (frame overlap) • Downstream Disk Chopper operates at 60Hz (order suppression) • Straight , short bladed, Fermi chopper which can run at 30, 60, 90, 120,…, 420Hz (this is the chopper that monochromates the beam) – nominal frequency is 180Hz Fermi Chopper T0 Chopper Disk Chopper Beam Guide Secondary Gate valve 8 Managed by UT-Battelle ISIS Design and Engineering Meeting shutter for the U.S. Department of Energy September 2012

  9. Drum Shield • Detail Design took ~10 months • Design began at Brookhaven National Laboratory with one engineer and one designer – Used AutoCAD and Inventor • Completed at SNS with as many as three engineers and four designers working simultaneously – Used Pro-E • Weighs ~120,000 pounds • Rotates from 14 ° to 90 ° • Contains 2 monochromators • Serves as primary beam stop for the instrument 9 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  10. Drum Shield Construction • Gray = High Density concrete • Pink = Lead • Dark Gray = B 4 C Plug Material Focusing Pb Crystals & HDC Translating Mechanism SS Guide B 4 C Field Insert Drum Shield to Sample NEUTRON FLUX Arm Shutter Sample Table Mounting Bearing 10 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  11. Manufacturing Welding Forming Lead Casting MAXUS ™ B4C / Aluminum parts 11 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  12. Drum Shield Installation and Testing Heusler Crystal Array HOPG Crystal Array 12 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  13. Drum Shield to Sample Arm • Drum Shield to Sample Arm was designed to carry the 16T compensated magnet (2.2 tons) with minimum deflection. • Linear table moves the sample from 1.4m to 1.8m from Drum Shield rotation axis linear table Drum Shield to Sample Arm Weldment Beamstop Assembly consisting of TC-16 lifting column and Beamstop Shield Assembly fabricated component Purchased part Subassembly with both fabricated and purchased components Hanger Box Assembly Beamstop Mount Weldment 13 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  14. HYSPEC Detector Vessel Overview Mast for “ship to shore” • Detail Design took one engineer Welded Rectangular cables and four designers ~7 months Aluminum Tubes Electronics racks • All non-magnetic materials mounted to top of (mostly aluminum) vessel • Weighs ~9,000 lbs • Hovers ~25 m m on 20 airpads Air cylinders • Holds 20 “8 packs” of 1.2m long for flapping ears Linear Position Sensitive Detectors (LPSD’s) Mounting for 3He Polarization Analyzer or Supermirror Polarization Analyzer Mounting plates for 3 He Filling Station Insides lined with 0.06”t Cadmium Shielding FEA Optimized 14 Managed by UT-Battelle ISIS Design and Engineering Meeting Connector for the U.S. Department of Energy September 2012

  15. Detector Vessel Overview • Filled with low pressure Argon • Large rear window required to keep detectors in air Drum Shield • Ship to shore lines carry data, to Sample power, air etc. Arm • can carry a fine radial collimator Ship to – for unpolarized or 3 He Shore Lines polarization analysis (will also work with 16T magnet) • Front is also able to carry the Helmholtz coils for 3 He analyzer system Detectors Fine Radial Collimator 15 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  16. Detector Vessel Front End Removable hatch for course collimator access 1/8 ” O-Ring Course Collimator Titanium Fasteners 0.5mm thick Aluminum Window Flapping Ears Front section ¼” O -Ring (Hidden) removable 16 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  17. Detector Vessel Lifting Features 20 Airpads Argon Inlet/Outlet Bolted on gussets connect Ports rear of skin to base 17 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  18. Rear Window Rear Window is 62.25” tall x ~200” long x 0.063” (1.6mm) thick Captured between two frames, sealed with an O- Ring Rear frame has vertical ribs to limit 18 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012 outward deflection and stress

  19. Window Analysis • Window thicknesses and construction were determined through iterative FEA • Large rear window required ribs to limit deflection and keep stress low – Ribs strategically placed to avoid shadowing detectors 19 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

  20. Design Through Analysis • Design of vessel was optimized through iterative FEA • Highest stresses, most difficult design was connection to rotation stage • Controlling deflection at rear of vessel was also challenging 20 Managed by UT-Battelle ISIS Design and Engineering Meeting for the U.S. Department of Energy September 2012

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