Helium two-phase flow in a thermosiphon open loop

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Helium two-phase flow in a thermosiphon open loop

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Presented at the COMSOL Conference 2009 Milan COMSOL Conference 2009 Milan October 14-16 2009 Helium two-phase flow in a thermosiphon open loop Florian Visentin, Bertrand Baudouy CEA Saclay Accelerator, Cryogeny and Magnetism Division 91191 Gif-sur-Yvette Cedex, France bertrand.baudouy@cea.fr 1

Outline Missions of SACM (Accelerator, Cryogenics and Magnetism Division) Context : The Large Hadron collider at CERN, Geneva Cooling large superconducting magnet Thermosiphon open loops for cooling superconducting magnets Experimental facility and ranges of the study COMSOL Multiphysics Modeling Results with COMSOL Multiphysics Comparison with experimental results 2

Missions of SACM SACM is developing and realizing particle accelerators cryogenic systems superconducting magnets for in-house and international scientific programs in the fields of astrophysics, nuclear physics, and particle physics SACM is mainly involved in large scale projects International Linear Collider (ILC) Light source XFEL IPHI project (high-intensity proton accelerator) Spiral 2 project (rare isotope beams) Neurospin Iseult, MRI solenoid R 3 B Glad spectrometer Large Hadron Collider (LHC) accelerator and detector construction at CERN with the quadrupoles magnets, the Atlas toroid and the CMS solenoid 3

Large Hadron Collider Large Hadron Collider Largest physics instrument in the world 27 km of circumference Proton-proton collider (14 Tev) LHC will describe with increasing detail the fundamental particles that make up the Universe and the interactions between them What is mass? What is 96% of the universe made of? Where is the anti-matter now? What was matter like within the first seconds of the Universe s life? Magnets at Over 8000 magnets for the ring Few gigantic magnets for detection 100 m underground! 4

Large Hadron Collider Detectors at LHC 5

Why magnetic field for particle detection? For a charged particle (q) moving in a magnetic field (B) over a distance L momentum p=mv=q B ( =bending radius) Precision on the measurement of p BL 2 /p Increasing the magnetic field and the dimension of detection (the magnet itself) improves the precision on particle detection Magnets must be superconducting Reduction in energy consumption to energize the magnet Higher current density with superconducting cables making the magnetic design feasible in reasonable space Transparency for the detection Still, these magnets are gigantic and needs to be cooled with liquid helium! 6

Example : The Compact Muon Solenoid 7

Cooling large superconducting magnet Compact Muon Solenoid magnet 7 m diameter and 12.5 m long 4 T at the center Liquid helium temperature cooling (4.2 K) Unique magnet of large scale Reduction of the quantity of cryogen Lower the cost of operation Protection in case of quench Lv 2 10 4 J/Kg Phase change ρ l /ρ v 7 External cooling Two-phase thermosiphon cooling method 8

Thermosiphon open loops (1/2) Open reservoir/phase separator No re-cooling of the warm liquid or re-condensation of the vapor Phase separator cryostat Power to be extracted Decrease in liquid density and/or vaporization Branch weight unbalance Flow induced Q Coil cryostat Suppression of any pressurization system Liquid level needs to be controlled to avoid dryout Minimum heat flux to start the flow Flow oscillations at low heat flux 9

Single phase flow Two-phase flow Single phase flow Thermosiphon open loops (2/2) In the downward branch, the flow is single phase Adiabatic branch and the liquid is sub-cooled Pressure and the temperature increase from to The upward branch is heated partially and above it is adiabatic (the riser) Flow is first in single phase from to Fluid reaches the saturation temperature at point Fluid temperature also increases up to the saturation line Point is the onset of nucleate boiling Then the flow above is two-phase Saturation line Fluid temperature decreases following theliquid saturation line Vapor Saturation line Liquid Vapor 10

Experimental facility and ranges To vapor cooled shield Test section Phase separator Pressure tap LHe 0.9 m 10 mm inner diameter ~1 m heated length Tsensor ± 2 mk Thermal anchor 0.76 m Ranges P: 1.004 ± 0.006 10 5 Pa Venturi flow-meter 0.53 m q: 0-25 kw/m 2 m: 0-12 g/s Downward tube x: 0 25% Heater 0.3 m Temperature sensors Pressure tap 0.07 m 11

COMSOL Multiphysics Modeling (1/2) Homogeneous model implemented in Comsol Multiphysics Mass d dz i du dz 0 with or with i l i m 1 x 1 m v l x Momentum dp du dp iu ig cos dz dz dz f, j 0 dp f d u l dz D l 2 f,d d d 2 dp f u u lo m dz D l 2 f,u u u 2 f 0. 079 Re 0. 25 j lo l 1 x 1 1 x 1 v v l 1/ 4 Energy q d u 4 iu hi gz cos D dz 2 j 2 with h CT or h C T L p p v 12

COMSOL Multiphysics Modeling (2/2) 1 D model with downward, horizontal and upward branches PDE general form module was used Segregated mode with three groups First group : conservation of mass and momentum with u and p as variables Pressure fixed at the loop entrance and Neumann condition for other boundaries For velocity, only Neumann conditions are used Second group : Energy conservation equation for T Temperature fixed at the loop entrance and Neumann conditions for other boundaries Third group : Energy conservation equation for the vapor quality, x Quality is set to zero until the saturation temperature is reached 13

Temperature (K) x Single phase flow Two-phase flow Single phase flow Results with COMSOL Multiphysics P (Pa) Case for 600 W/m 2 p=101325 Pa Convergence 10-7 960 elements Liquid Saturation line Vapor 4.240 0.10 4.236 Donward + horizontal branch Upward branch 0.08 Saturation line 4.232 4.228 4.224 4.220 0 2 length (m) Liquid 0.06 0.04 0.02 0.00 Vapor 14

m t (kg/s) Comparison with experimental results At low heat flux, the flow is dominated by the gravity term At higher heat flux the friction term increases causing the slight decrease of the total mass flow rate 0.012 0.010 0.008 0.006 0.004 0.002 0.000 0 1000 2000 q (W/m 2 ) 15

x Comparison with experimental results Vapor quality reproduced with good accuracy up to 1500 W/m 2 At 1500 W/m 2 film boiling appears No thermodynamic equilibrium between the two phases Homogeneous model no longer holds 0.40 0.35 0.30 0.25 0.20 0.15 0.10 0.05 0.00 0 1000 2000 q (W/m 2 ) Model sufficiently accurate to be used for designing cooling system 16

Conclusions COMSOL easy to handle for non expert Easy implementation and modification of physics models Next is transient Pressure rise due to vaporization in liquid helium Mechanical constraints on the magnet structure Fluid management Adding multi-physics Interaction with the stability of superconductors Magnetic field interaction Going superfluid (He II) Some magnets are cooled with superfluid helium Heat transfer laws are super different Modified Fourier law Non linear boundary condition (Kapitza resistance) 17