Replies to Spanish RFQ Questions (slides re-used from previous talks)

Slides:



Advertisements
Similar presentations
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.
Advertisements

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
RFQ End Flange Dipole Tuner Finger Cooling. Basis of Study Need multi-purpose end flange –Adjustable dipole mode suppression fingers –Beam current transformer.
Introduction to Plasma-Surface Interactions Lecture 6 Divertors.
Using Copper Water Loop Heat Pipes to Efficiently Cool CPUs and GPUs Stephen Fried President Passive Thermal Technology, Inc.
Lesson 17 HEAT GENERATION
1 NCEA Physics Electricity and Magnetism. 2 Charging by friction Aims: To be able to describe common materials which are electrical conductors or insulators.
UNIT 13 : HEAT 13.1 Thermal Conductivity 13.2 Thermal Expansion.
D. Lipka, MDI, DESY Hamburg, July 2012 Simulation of fields around spring and cathode for photogun D. Lipka, MDI, DESY Hamburg.
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.
Chapter 10 Section 2 Hypothesis Tests for a Population Mean
Modifications Required on Model Before Meshing & Solving Slice up to define mesh in different areas –Transversely separate vane-tip region (about 16x16mm.
RFQ CAD Model Tolerance Studies Simon Jolly 14 th December 2011.
Injector RF Design Review November 3, 2004 John Schmerge, SLAC LCLS RF Gun Thermal Analysis John Schmerge, SLAC November 3,
A discussion paper for the Absorber Review pre-meeting on February 11 th 2003 On 3-D Fluid Flow calculations on the 22cm Absorber Window By Stephanie Yang.
Realistic Model of the Solenoid Magnetic Field Paul S Miyagawa, Steve Snow University of Manchester Objectives Closed-loop model Field calculation corrections.
Development of the FW Mobile Tiles Concept Mohamed Sawan, Edward Marriott, Carol Aplin University of Wisconsin-Madison Lance Snead Oak Ridge National Laboratory.
Effect of Vane Misalignment on RFQ Resonant Frequency.
RFQ Thermal Analysis Scott Lawrie. Vacuum Pump Flange Vacuum Flange Coolant Manifold Cooling Pockets Milled Into Vanes Potentially Bolted Together Tuner.
ELECTROMAGNETIC, THERMAL, AND STRUCTURAL ANALYSIS OF RF CAVITIES USING ANSYS 2.1 GHz 3-Cell Cavity Cliff Brutus 7/9/15 Workbench Job Name: 2.1ghz_Symmetry_
Drive beam magnets powering strategy Serge Pittet, Daniel Siemaszko CERN, Electronic Power Converter Group (TE-EPC) OUTLINE : Suggestion of.
RFQ Fabrication Plan, Schedule and QC PXIE RFQ Fabrication Readiness Review LBNL – June 26, 2013 Steve Virostek - Engineering Division Lawrence Berkeley.
CS Thermal Analysis Status Heating and Cooling of CS During Normal Operation - SN & DN Operation –Overall Heat Balance –Heating of Center Stack First Cut.
LMC 30 LPC A. Verweij, TE-MPE. 30 Sept 2009, LMC meeting 1.9 K, 0 T, 7.5 kA run Heat pulse.
F.E.T.S. RFQ Mechanical Design by Peter Savage 7 th January 2010.
LHC Phase II Collimator Compact jaw simulations New FLUKA => ANSYS mapping scheme New 136mm x 950mm jaw –60cm primary collimator –Helical cooling channel.
Chapter 4 Axial Load. Saint -Venant's Principle Saint-Venant's Principle claims that localized effects caused by any load acting on a body will dissipate.
MICE CC Test Status Ruben Carcagno 11/06/13 1. Cooldown Coil Temperature (calculated average in each of 8 coil segments) SC Transition (voltages across.
One-Dimensional Steady-State Conduction
S. Kahn 5 June 2003NuFact03 Tetra Cooling RingPage 1 Tetra Cooling Ring Steve Kahn For V. Balbekov, R. Fernow, S. Kahn, R. Raja, Z. Usubov.
IMP Visit July 10, 2013 Matt Hoff LBNL July 18, 2013.
Magnet for ARIES-CS Magnet protection Cooling of magnet structure L. Bromberg J.H. Schultz MIT Plasma Science and Fusion Center ARIES meeting UCSD January.
Chapter 6 A four-node quadrilateral element is shown in the figure. 1.Write the (x,y) coordinates in the elements in terms of (s,t) of the reference element.
Fine-Tuning the RFQ End Region. “…The Devil is in the Detail” RFQ bulk design very close to completion But before drafting need to check: Repeatability.
5 K Shield Study of STF Cryomodule Norihito Ohuchi, Norio Higashi KEK Xu QingJin IHEP 2008/3/3-61Sendai-GDE-Meeting.
Updated Thermo-Mechanical Model of the CLIC Two-Beam Module Riku Raatikainen
PASI OsC meeting 12th July 2012
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.
Nonlinear Analyses of Modular Coils and Shell structure for Coil Cool-down and EM Loads Part 1 – Results of Shell Structure and Modular Coils H.M. Fan.
CRYOGENICS FOR MLC Cryogenic Principle of the Module Eric Smith External Review of MLC October 03, October 2012Cryogenics for MLC1.
AWB NSTX TF Flag Joint Design Review April 10, 2003 Art Brooks.
E. Da Riva/M. Gomez Marzoa1 WG4 Meeting - 27th June 2012 Air Cooling by means of carbon fiber structure Enrico DA RIVA (EN-CV-PJ) Manuel GOMEZ MARZOA (EN-CV-PJ)
© 2011 Autodesk Freely licensed for use by educational institutions. Reuse and changes require a note indicating that content has been modified from the.
5 K Shield Study of STF Cryomodule (up-dated) Norihito Ohuchi KEK 2008/4/21-251FNAL-SCRF-Meeting.
TEM3P Simulation of Be Wall Cavity Tianhuan Luo. Cavity Model Pillbox cavity with Be wall R=0.36 m, f0~319 MHz, L=0.25m (not exactly 325 MHz, but not.
Heat Transfer Su Yongkang School of Mechanical Engineering # 1 HEAT TRANSFER CHAPTER 6 Introduction to convection.
Movement of Substances In and Out of Cells. Cells need and take in many substances for their metabolism and optimum functioning…Examples?? As well as.
CDR2 – Coupler Mechanical Design NICOLAS MISIARA.
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.
35 Ton LAr Impurity Distribution Measurements and CFD simulation Erik Voirin – Fermilab – Thermal and Fluids Engineering Group / Engineering.
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.
CMS TK II cooling Brainstorming P. Tropea (update after meeting on June 13 th with Duccio, Antti, Hans, Jerome, Paolo, Bart) 20 June 2016.
PXIE RFQ Engineering Design Steve Virostek Engineering Division Lawrence Berkeley National Laboratory April 10, 2012 Project X Collaboration
704 MHz cavity design based on 704MHZ_v7.stp C. Pai
PXIE RFQ Design Overview Derun Li for PXIE RFQ Design Team Center for Beam Physics Accelerator and Fusion Research Division Lawrence Berkeley National.
Date of download: 9/26/2017 Copyright © ASME. All rights reserved.
Aerodynamic and Heat Transfer Validation of LPT-OGVs (TURB34−LTH part) Chenglong Wang, Lei Wang, and Bengt Sundén Department of Energy.
APPLICATION OF COHESIVE ELEMENT TO BIMATERIAL INTERFACE
Physics design on Injector-1 RFQ
Hervé Allain, R. van Weelderen (CERN)
Mechanical Engineering progress for the Front End Test Stand
F.Pasdeloup, H.Prin, L. Williams
Presentation transcript:

Replies to Spanish RFQ Questions (slides re-used from previous talks)

Points Raised by Juan Luis Muñoz (questions_FETS_17nov2010.pdf) “Looking at a 2m model, RF power concentrates at ends. So cannot assume 2.5kW equally distributed in each 0.5m section” “Power increases at ends a lot when mirroring vacuum slots” “Should be using about 4.5kW at end sections and less toward centre”

Matcher Geometry Plane vanes Matcher On

Effect of Matcher on Long. Fields Matcher Off: Fields peak at ends Matcher On: Fields peak at centre E-field B-field

Four Metre RFQ Field Flatness

Cold Model Field Flatness

Summary of Reply to Juan Drastic change when adding a few extra vacuum slots doesn’t sound realistic. Maybe the mesh was compromised in vane-tip region by needing to mesh the extra slots? The EM fields do seem to distribute themselves in interesting ways along the entire 2m length! However we’ll aim to achieve good field flatness so there are no peaks at ends. 2.5kW per 0.5m section is based on 80kW average power in RFQ. We have already allowed at least 25% safety margin by using this figure.

Comments on Ana Megia’s Work (1) (RFQ _Megia.pdf and RFQ cooling ESSB _extended.pdf) Squirt nozzle mechanical design looks nice and simple. Good idea having separate cooling circuit for it and the 45° threaded insert. Heat flux is highest at vane cut- back but due to much larger area of vane sides, the total power applied to bulk vane is similar to total power to vane ends. Have you calculated to power distributions of each feature within a section?

Comments on Ana Megia’s Work (2) (RFQ _Megia.pdf and RFQ cooling ESSB _extended.pdf) There will be significant cooling applied to each slug tuner which will help remove heat. Even if you don’t model the slugs in the eigenmode solver, you should include their cooling in the thermal solver. We have slightly changed the cooling pocket layout to make it more symmetrical with respect to the vacuum port cooling manifold, which will alter things slightly. (ignore the pi-mode stabiliser rods: redundant design)

Comments on Ana Megia’s Work (3) (RFQ _Megia.pdf and RFQ cooling ESSB _extended.pdf) Unsure why your simulations imply that the RFQ cannot be cooled sufficiently with water at sensible temperatures... What are your criteria for a well cooled RFQ? Displacement of vane-tips toward each other should be <20µm. Temperature gradients in your models seem to be small (<10°C?) so thermal displacements shouldn’t be too large...