High Power Hg Target Conceptual Design Review Hg Target Design P.T. Spampinato V.B. Graves T.A....
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![Page 1: High Power Hg Target Conceptual Design Review Hg Target Design P.T. Spampinato V.B. Graves T.A. Gabriel Oak Ridge National Laboratory February 7-8, 2005.](https://reader031.fdocuments.us/reader031/viewer/2022020417/56649d425503460f94a1dee9/html5/thumbnails/1.jpg)
High Power Hg Target Conceptual Design Review
Hg Target Design
P.T. SpampinatoV.B. GravesT.A. Gabriel
Oak Ridge National Laboratory
February 7-8, 2005
![Page 2: High Power Hg Target Conceptual Design Review Hg Target Design P.T. Spampinato V.B. Graves T.A. Gabriel Oak Ridge National Laboratory February 7-8, 2005.](https://reader031.fdocuments.us/reader031/viewer/2022020417/56649d425503460f94a1dee9/html5/thumbnails/2.jpg)
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Outline
Design Constraints
Original Hg delivery concept & issues
Proposed new baseline delivery system
Hg flow analysis in new baseline system
Issues & recommendations
![Page 3: High Power Hg Target Conceptual Design Review Hg Target Design P.T. Spampinato V.B. Graves T.A. Gabriel Oak Ridge National Laboratory February 7-8, 2005.](https://reader031.fdocuments.us/reader031/viewer/2022020417/56649d425503460f94a1dee9/html5/thumbnails/3.jpg)
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Design Constraints Hg Jet
1cm dia, 20m/s (1.57 liter/s, 24.9 gpm) in same direction as beam Free jet created inside 15cm magnet bore Smooth, steady-state jet duration overlaps 1-sec max field
duration
Integrate optical diagnostics
Materials compatibility with Hg
No target equipment on up-beam end of magnet
Period between beam shots approximately 30 minutes to allow magnet cooling
Component module size limitation is 1.3m x 3m (facility issues)
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Experiment Geometric Configuration
Experiment is prototypic of a N.F. facility target layout Magnet tilt (wrt beam) = 66
mrad (3.8°) Hg jet tilt (wrt magnet axis) =
100 mrad (5.7°) Hg jet center intersects beam
center at Z=0
![Page 5: High Power Hg Target Conceptual Design Review Hg Target Design P.T. Spampinato V.B. Graves T.A. Gabriel Oak Ridge National Laboratory February 7-8, 2005.](https://reader031.fdocuments.us/reader031/viewer/2022020417/56649d425503460f94a1dee9/html5/thumbnails/5.jpg)
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
System Overview
Solenoid
ProtonBeam
Hg DeliverySystem
IntermediateBeamStop
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Original Hg Delivery SystemPump Motor
CentrifugalPump
Hg Jet Containment
Sump Tank
Secondary Containment
Target Module
![Page 7: High Power Hg Target Conceptual Design Review Hg Target Design P.T. Spampinato V.B. Graves T.A. Gabriel Oak Ridge National Laboratory February 7-8, 2005.](https://reader031.fdocuments.us/reader031/viewer/2022020417/56649d425503460f94a1dee9/html5/thumbnails/7.jpg)
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Pump Issues
Pump adds heat to Hg Pump delivers nominal 51 bhp at 23% efficiency (60
bhp max) Magnetic coupling losses 5.4 hp Heat energy into mercury
LostHP = (bhp - mag)*(1 - eff) + mag = 40.5 hp (30kw) With an assumed Vol=12liter, ΔT=2.4°F/sec (1.3°C/sec)
due to pump heating only
Max available pump output pressure is 750 psi (50 bar) Estimated piping system pressure drop 800-850 psi
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Pump Energy Balance
PumpHeat
Direct to Tunnel
Heat Input to
Hg
Flow Losses
Energy to Hg
Hg Temp Rise
Input Energy
(hp)Losses
Lost Energy
(hp)
Output Energy (hp)
BTU/min BTU/min BTU/minBTU/ min
KW HP BTU/min °F/sec
Elect Motor 60 60 hp * 5% inefficiency 3 57 127 127 2 3
Mag Coupling5.4hp actual coupling loss per vendor data
5.4 51.6 229 229 4 5
Hg Pump40.5hp actual pump loss
per vendor data40.5 11.1 1719 1719 30 40 1719
Hg Flow 800psi*25gpm 12 -1 526 526 9 12 526
Totals 356 1719 526 2601 46 61 2245 3.1
Total Heat Generated
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Possible Solutions
Heat issue Increase Hg volume (ΔT decreases linearly with Hg mass) Add heat exchanger for system testing
May not be needed during CERN tests
Pump discharge pressure issue Vendor specified pump to provide max DP Investigate alternative Hg delivery systems
Nature of experiment lends itself to non-continuous flow approach, so…
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Alternative Hg Delivery System
Hydraulic Fluid Cylinder (3000 psi)
Hg Cylinder (1000 psi)
Hg Discharge
Hg Inlet
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Syringe Size Comparison
Hydraulic Pump& Reservoir
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
System Energy ComparisonPump
Heat Direct to Tunnel
Heat Input to
Hg
Flow Losses
Energy to Hg
Hg Temp Rise
Input Energy
(hp)Losses
Lost Energy
(hp)
Output Energy (hp)
BTU/min BTU/min BTU/minBTU/ min
KW HP BTU/min °F/sec
Elect Motor 60 60 hp * 5% inefficiency 3 57 127 127 2 3
Mag Coupling5.4hp actual coupling loss per vendor data
5.4 51.6 229 229 4 5
Hg Pump40.5hp actual pump loss
per vendor data40.5 11.1 1719 1719 30 40 1719
Hg Flow 800psi*25gpm 12 -1 526 526 9 12 526
Totals 356 1719 526 2601 46 61 2245 3.1
Syringe
Elect Motor 20 20 hp * 5% inefficiency 1 19 42 42 1 1
Hyd Pumpenergy performed on
piston = press*area*dist/time
11
Hyd Pump pump inefficiency 8 11 340 340 6 8
Piston Energy to Hg no losses 11
Hg Flow 800psi*25gpm 12 -1 526 526 9 12 526
Totals 382 526 908 16 21 526 0.7
Total Heat Generated
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Syringe Performance Benefits Piston-driven jet has excess capacity to overcome flow
losses
No significant heat imparted to Hg by piston Heat losses isolated to hydraulic system Flow losses identical to those in pump system No heat exchanger required
Syringe design may be smaller than shown, depending on Hg volume required 1.6 liter/s → 48 liter for 30sec, 24 liter for 15sec Concept shown in size comparison was sized for 30sec jet
Lower power requirements 20hp hydraulic pump motor vs. 60hp centrifugal pump motor
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Hg Cylinder Experience
SNS test stand used pneumatic cylinders to cycle candidate drain valves several thousand cycles with no leaks
Low-pressure application with automated controls
Float chambers
Pnuematic pressurization cylinder
Mercury cylinder
LVDT’s
Phonix valve
Descote valve
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
New Baseline Target SystemHg Cylinder
Vent Line
PositionSensor
Checkvalve
Ball Valve
Sized for 20sec jet
Drain
HgSupply
HgReturn
Position Sensor
Hydraulic Lines
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Sump Tank
22" SS pipe
Hg inventory 36 liter, 1068 lb 6 inch depth
Incorporates float-type level sensor, Hg fill & extraction ports
Thermocouple on sump exterior or in direct Hg contact
Potential use as storage tank for shipping
Sight Glass
LevelSensor
Hg FillPort
HgExtraction
Port
DeflectorPlate
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Syringe 8" Hg cylinder, 4"
hydraulic cylinders, 39" strokes Sizes chosen based
on costs
Position sensor allows actual flowrate calculations
Checkvalve prevents backflow into sump Must remain
submerged throughout experiment to prevent air intake in cylinder
Discharge pipe will require structural supports
Ball Valve –Manual or Remote Position Sensor
1" SSDischarge
Pipe
Drain Valve& Cap
SS Flex MetalHoses – 1" and 6"
Checkvalve
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Hg Supply TubingHg Supply
1" SS Rigid Tubing
Tubing RestraintsTubing Welded
To Plenum
Flange or Weld Interfaces
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Hg Plenum
Purpose is to provide reservoir to allow Hg to change direction in confined space
Open chamber with nozzle exit and beam thru-tube
Raised bottom for drainage
SingleTube Dual
Supply Lines
BeamWindow
SecondaryContainment
InterfacePoint
Plenum
BeamThru-tube
Nozzle
BottomFlush w/
Exit
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Plenum Issue
Trapped air in plenum Swept out with Hg Compressed and acts
like spring
Solutions Evacuate system
prior to operation Hg vapor issue
Provide means to quickly move air out nozzle
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Plenum Structural Design
Static FEA performed using pressure load of 850psi on interior surfaces
Minimum FOS = 6 around beam thru-tube
Flow analysis presented by M. Wendel
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Plenum/Nozzle Integration
Plenum & nozzle welded to primary containment – no nozzle replacement
Nozzle side restraints resist field-induced motion in Hg
Length set at 10X dia = 4"
Changes to inlet/exit required based on flow analysis
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Primary Containment – Right Side
Weldment 0.25" SS PlateFlared Outside Magnet
O/A Length 63"
Interface toSecondary
Containment
OpticalDiagnostics
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Primary Containment – Left Side
ReflectorAssemblies
5" x 5"Hg Exit
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Primary Containment – Side View
JetDeflector Hg Jet
Z=0 ViewportSecondaryContainment
Anti-vibrationMechanismPrimary
Containment
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Deflector
Purpose is to enhance Hg drainage into sump tank by minimizing splashing and Hg drops back into magnet bore
Material is Ti6Al4V, same material used for beam windows
Designed as flat plate with low angle of incidence Some curvature may be needed to aid in flow control Princeton tests can be used to provide design feedback
Stress calculation indicates Hg jet impact force <100lb Deflector thickness of 0.1" provides FOS=5.5
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Primary Containment Cross Section
Hg Supply
Hg Jet
PrimaryContainment
Sight GlassCover
Reflector
Sight Glass
Optics
SecondaryContainment
OD=6.18" (157mm) Magnet Bore ID = 162mm
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Viewports
Optical viewport laminated with rad-resistant gaskets
Mechanically fastened cover plate
Structural rigidity of disk needs further analysis
Gaskets
Fused SilicaDisk Cover Plate
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Primary Containment As Supplied
Viewport components fabricated as part of primary containment
Windows & optical diagnostics to be provided by others
Interface sketches will be provided in Final Design
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Secondary Containment SS sheet metal
enclosure around entire primary system
Contains Hg leaks, provides access to monitor Hg vapors
Provides access to optical diagnostics, hydraulics, and sensors
Incorporates beam windows
3 components: hydraulics box, target cover, connecting rubber sleeve
Hose Clamps& Sleeve
Heater FoilElectrical Leads
HydraulicConnectors
Optics PortLid w/Gasket
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Hg Target System
Secondary tank dimensions 102x36x45" (2.6x0.9x1.1m) without support base
Need to reduce footprint Facility limits are
3m x 1.3m
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Mechanical Design Issues Nozzle design
More analysis needed Nozzle/deflector designs need validation Air entrapment in plenum Removable nozzle
Viewports Structural rigidity of viewport optics May require testing
System sizing Footprint for 20sec syringe too large
Minor width reduction possible Need to decrease required stroke
For 8" cylinder, 1 sec jet duration requires 1.9" stroke Reducing jet duration by 1 sec reduces overall cylinder
length by 3.8" Recommend reducing max jet duration to 15s
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Hg Flow Analysis
Piping analysis performed using AFT Fathom 5.0
Results shown separately
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Recommendations
Change baseline Hg delivery system to syringe approach
Size syringe & sump tank with capacity for 15-second jet
Perform additional nozzle simulations and analyses
Perform Hg flow tests to provide needed design feedback
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OAK RIDGE NATIONAL LABORATORYU. S. DEPARTMENT OF ENERGY
Conceptual Design Review 7-8 Feb 05
Syringe Layout