RFQ End Flange Dipole Tuner Finger Cooling. Basis of Study Need multi-purpose end flange –Adjustable dipole mode suppression fingers –Beam current transformer.

Slides:



Advertisements
Similar presentations
HiRadMat Window Design report v2.0 1Michael MONTEIL- 16 March 2010.
Advertisements

S. N. HOM Impedance in Vacuum … 1 of 40 Sasha Novokhatski SLAC, Stanford University Machine-Detector Interface Joint Session April 22, 2005 HOM Impedance.
The Front End Test Stand Collaboration ELECTROMAGNETIC DESIGN OF A RFQ FOR THE FRONT END TEST STAND AT RAL A. Kurup, A. Letchford The RAL front end test.
Chapters 25--Examples.
New Plate Baffle Water Flow. Quick Simulation Use triangular prism as rough estimate of a vane Uniform heat flux on each surface –600 kWm -2 on end face.
RFQ Matcher. What am I doing this time?! Concerned that modulations and matcher affect field flatness and frequency These are very small features How.
RFQ Cooling Studies.
RFQ Structural Mods Scott Lawrie. Vacuum Pump Flange Vacuum Flange Coolant Manifold Cooling Pockets Milled Into Vanes Potentially Bolted Together Tuner.
Effect of RFQ Modulations on Frequency and Field Flatness
CFD Simulations of a Novel “Squirt-Nozzle and Water Bath” Cooling System for the RFQ.
Longitudinal Expansion of RFQ Vane Ends at Section-to-Section Interface.
Global Design Effort Compact Water Cooled Dump Resistor IRENG07 Wes Craddock September 19, 2007.
Modifications Required on Model Before Meshing & Solving Slice up to define mesh in different areas –Transversely separate vane-tip region (about 16x16mm.
Analysis of Simple Cases in Heat Transfer P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Gaining Experience !!!
First Wall Thermal Hydraulics Analysis El-Sayed Mogahed Fusion Technology Institute The University of Wisconsin With input from S. Malang, M. Sawan, I.
Fluid Flow and Continuity Imagine that a fluid flows with a speed v 1 through a cylindrical pip of cross-sectional area A 1. If the pipe narrows to a cross-
TMM of the CLIC Two-Beam Module T0 in the LAB – Proceedings to structural FEA Riku Raatikainen
CO2 cooling pressure drop measurements R. Bates, R. French, G. Viehhauser, S. McMahon.
INTRODUCTION to the DESIGN and FABRICATION of IRON- DOMINATED ACCELERATOR MAGNETS Cherrill Spencer, Magnet Engineer HOMEWORK PROBLEM for Lecture # 2 of.
Engineering Department ENEN 16/08/2013 LR - BBC Pre-Study 1 STATUS of BBC DESIGN and ENGINEERING : PRELIMINARY RESULTS G. MAITREJEAN, L. GENTINI.
CIEMAT CONTRIBUTION TO TBL PETS (January 2009) David Carrillo on behalf of the Accelerators Team.
Fouling Factor: After a period of operation the heat transfer surfaces for a heat exchanger become coated with various deposits present in flow systems,
RFQ Thermal Analysis Scott Lawrie. Vacuum Pump Flange Vacuum Flange Coolant Manifold Cooling Pockets Milled Into Vanes Potentially Bolted Together Tuner.
1 cm diameter tungsten target Goran Skoro University of Sheffield.
Bias Magnet for the Booster’s 2-nd Harmonic Cavity An attempt to evaluate the scope of work based of the existing RF design of the cavity 9/10/2015I. T.
Stress and cool-down analysis of the cryomodule Yun He MLC external review October 03, 2012.
1 CHAPTER 6 HEAT TRANSFER IN CHANNEL FLOW 6.1 Introduction (1) Laminar vs. turbulent flow transition Reynolds number is where  D tube diameter  u mean.
F.E.T.S. RFQ Mechanical Design by Peter Savage 7 th January 2010.
Stress and Cool-down Analysis Yun HE MLC Internal Review 9/5/2012Yun HE, MLC Internal Review1.
CRYOGENICS FOR MLC Cryogenic Piping in the Module Eric Smith External Review of MLC October 03, October 2012Cryogenics for MLC1.
30 th June 20111Enrico Da Riva, V. Rao Parametric study using Empirical Results June 30 th 2011 Bdg 298 Enrico Da Riva,Vinod Singh Rao CFD GTK.
Consideration of Baffle cooling scheme
CLIC Prototype Test Module 0 Super Accelerating Structure Thermal Simulation Introduction Theoretical background on water and air cooling FEA Model Conclusions.
Convection: Internal Flow ( )
Full Scale Thermosyphon Design Parameters and Technical Description Jose Botelho Direito EN/CV/DC 19 November, th Thermosyphon Workshop.
Replies to Spanish RFQ Questions (slides re-used from previous talks)
56 MHz SRF Cavity Thermal Analysis and Vacuum Chamber Strength C. Pai
Simple CFD Estimate of End Flange Tuner Finger Cooling.
Mitglied der Helmholtz-Gemeinschaft Jörg Wolters, Michael Butzek Focused Cross Flow LBE Target for ESS 4th HPTW, Malmö, 3 May 2011.
CRYOGENICS FOR MLC Cryogenic Principle of the Module Eric Smith External Review of MLC October 03, October 2012Cryogenics for MLC1.
AAE 450 – Spacecraft Design Sam Rodkey 1 Active Thermal Control Design Sam Rodkey March 1 st, 2005 Project Management Project Manager.
E. Da Riva1 ITS Upgrade - Air cooling Layers Geometry Change!
Cooling of GEM detector CFD _GEM 2012/03/06 E. Da RivaCFD _GEM1.
Cryogenic scheme, pipes and valves dimensions U.Wagner CERN TE-CRG.
Simulation of heat load at JHF decay pipe and beam dump KEK Yoshinari Hayato.
Aachen Status Report: CO 2 Cooling for the CMS Tracker at SLHC Lutz Feld, Waclaw Karpinski, Jennifer Merz and Michael Wlochal RWTH Aachen University, 1.
4/26/2013 Irina PetrushinaDeflecting cavity MHz for PXIE Irina Petrushina 4/26/2013.
Heat Transfer by Convection
CDR2 – Coupler Mechanical Design NICOLAS MISIARA.
CW Cryomodules for Project X Yuriy Orlov, Tom Nicol, and Tom Peterson Cryomodules for Project X, 14 June 2013Page 1.
ESS RFQ B. POTTIN and RFQ team CEA-IRFU. RFQ design Strategy 3 RF codes to validate calculations Consideration of machining and assembly possibilities.
A. Lambert: Thermal and Mechanical Analysis PXIE RFQ Design Review, Berkeley, CA April 12, 2012 Thermal and Mechanical Analysis of the PXIE RFQ Andrew.
RFQ Cooling Schemes and Instrumentation PXIE RFQ Fabrication Readiness Review LBNL – June 26, 2013 Andrew Lambert - Engineering Division Lawrence Berkeley.
STATUS OF THE NC BUNCHING RFQ (Sub-task: SC-RFQ) Antonio Palmieri INFN-LNL.
RFQ coupler S. Kazakov 07/28/2015. Requirements: Coupler requirements Expected problems: Heating (loop, ceramic window, etc.) Multipactor Solutions: Appropriate.
Engineering of the power prototype of the ESRF HOM damped cavity* V. Serrière, J. Jacob, A. Triantafyllou, A.K. Bandyopadhyay, L. Goirand, B. Ogier * This.
704 MHz cavity design based on 704MHZ_v7.stp C. Pai
Chopper Beam Dump Thermal Problem 10/27/20101PX Linac FE Technical Discussions.
Thermal Considerations in a Pipe Flow (YAC: 10-1– 10-3; 10-6) Thermal conditions  Laminar or turbulent  Entrance flow and fully developed thermal condition.
704 MHz cavity folded tuner Thermal Analysis C. Pai
Stress and cool-down analysis of the cryomodule
XFEL beamline loads and HOM coupler for CW
Thermal-Structural Finite Element Analysis of CLIC module T0#2
Thermal-Structural Finite Element Analysis of CLIC module T0#2
Physics design on Injector-1 RFQ
CFD-Team Weekly Meeting - 8th March 2012
Aachen Status Report: CO2 Cooling for the CMS Tracker at SLHC
TBM thermal modelling status
Compact and Low Consumption Magnet Design The DESY Experience
Heat As Energy Transfer
Presentation transcript:

RFQ End Flange Dipole Tuner Finger Cooling

Basis of Study Need multi-purpose end flange –Adjustable dipole mode suppression fingers –Beam current transformer toroid mount –Potentially high heat loads Not much room between LEBT and RFQ Want simple, compact cooling scheme Need estimates of cooling performance

First design from Pete 2cm 1cm 3cm 5cm 6mm 4cm 5cm

First Estimate of Heat Load FETS RFQ: 62 Wcm -2 at vane cut-back Assume less than half this on fingers? So 25 Wcm -2 is reasonable. IPHI RFQ end flange: 26 Wcm -2 on fingers (CW RFQ, though, so ours will have much less than this in reality, but 25 Wcm -2 will allow large safety margin)

Bulk copper in end flange is ~ 40 °C Finger gets pretty warm (100 °C) but that shouldn’t matter at all

As a Rough Example Simulation: 160W of heat per finger removed ok Indirect cooling means finger gets hot …but not enough to worry about Overall, this cooling strategy should be fine Assumes 25 Wcm -2 heat load (OVERESTIMATE!) Commence RF simulation to get better estimate of heat load on fingers

RF Simulation of Heat Load Internal vacuum of RFQ for solution of eigenmodes. Finger intrudes into vacuum. Parameterised to vary length and position. High resolution vacuum around finger.

End-on Views of RF Fields Around Finger Quadrupole magnetic field Dipole magnetic field 10mm diameter, 80mm long finger 15mm in x and y from beam axis 15mm 21.2mm

End-on Views of RF Fields Around Finger Quadrupole electric field Dipole electric field 10mm diameter, 80mm long finger 15mm in x and y from beam axis

Overall Body Surface Heat Flux (non-linear scale) Quadrupole heat flux Dipole heat flux 10mm diameter, 80mm long finger 15mm in x and y from beam axis

Cut-back and Finger Heat Flux (non-linear scale) Quadrupole heat flux Dipole heat flux > 50 Wcm -2 at vane cut-backs 10mm diameter, 80mm long finger 15mm in x and y from beam axis

Quadrupole heat flux Dipole heat flux Finger Surface Heat Flux 16 Wcm -2 on finger from dipole mode 3 Wcm -2 on finger from quadrupole mode 10mm diameter, 80mm long finger 15mm in x and y from beam axis 10mm 80mm

Variation of Finger Length 10mm diameter fingers of varying length 15mm in x and y from beam axis

Variation of Finger Position 10mm diameter, 80mm long fingers Vary finger distance from beam axis

Fingers allow very fine tuning of RFQ For optimal tunability, need: –Variable length (2 to 10cm) fingers –Close (< 5cm) to beam axis –Cooling close as possible to entrance hole Max. heat assumes resonating on the dipole mode which won’t be the case Overall, finger heat won’t be a problem Conclusion

Spare slides

15°C Water in at 1 ms -1 flow rate Water out with temperature raised and at 0 Bar relative pressure 25 Wcm -2 heat flux load on finger High mesh density in region between finger and pipe Copper starting temperature = 22°C

Flow Estimates Total power, P, to be removed from each finger ≈ 160 W Water mass flow rate,, per pipe = kgs -1 (assuming flow speed = 1 ms -1 = 1.7 l min -1 ) Estimated temperature rise, ΔT, of cooling water = 1.35 °C Pipe length, L, within copper = 10 cm Average water flow rate v av = 1 ms -1 Pipe diameter, D H = 6 mm Estimated pressure drop, Δp = Bar Nusselt number, N u, of water flow = Thermal conductivity of water, k = 0.6 Wm -1 K -1 Estimated heat transfer coefficient = 5500 Wm -2 K -1

Intersection of drilled pipes slightly disrupts smooth flow

Faster, disrupted flow round corner increases local HTC Average HTC ~ 6000 Wm -2 K -1 which agrees with estimate

Temperature rise of water ~ 2 °C which agrees with estimate

Pressure drop is slightly higher than estimate because the pipe doesn’t have a smooth bend at corner, but it’s still nice and low