Mercury Nozzle Status V.B. Graves Hg Jet Design Meeting Princeton University Nov 15, 2004.

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Mercury Nozzle Status V.B. Graves Hg Jet Design Meeting Princeton University Nov 15, 2004

O AK R IDGE N ATIONAL L ABORATORY U. S. D EPARTMENT OF E NERGY Hg Jet Design Meeting – 15 Nov 2004 Nozzle Constraints  Tilted solenoid has imposed new geometry constraints on the nozzle  Up-beam windows are now at bottom of primary containment  Nozzle cannot penetrate primary on end flange, currently penetrates from sides  No interaction between beam & Hg until Hg exits nozzle

O AK R IDGE N ATIONAL L ABORATORY U. S. D EPARTMENT OF E NERGY Hg Jet Design Meeting – 15 Nov 2004 Flow Issues  High flow in small diameter thin-wall lines, tight flow path  Direction changes cause several problems  Pressure drop  Vibration  Cavitation  Tube erosion

O AK R IDGE N ATIONAL L ABORATORY U. S. D EPARTMENT OF E NERGY Hg Jet Design Meeting – 15 Nov 2004 Design Issues  Desire mechanically attached nozzle for changeout during cold testing – in current concept manifold is welded in position  Need to maximize pipe diameter to decrease velocity and minimize pressure drop  Two supply lines  Structural requirements for piping restraints not yet investigated  Possibly supply Hg outside of solenoid in double- wall pipe – a last resort

O AK R IDGE N ATIONAL L ABORATORY U. S. D EPARTMENT OF E NERGY Hg Jet Design Meeting – 15 Nov 2004 Nozzle Designs Initial Concept Current Concept

O AK R IDGE N ATIONAL L ABORATORY U. S. D EPARTMENT OF E NERGY Hg Jet Design Meeting – 15 Nov 2004 Next Steps  Determine physical constraints  Beam cannot penetrate manifold  Develop manifold internals for manufacturability  Flow analysis  Structural analysis  Princeton tests

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