Physics design on Injector-1 RFQ

Slides:



Advertisements
Similar presentations
RFQ development for high power beams
Advertisements

RFQ Cooling Studies.
Final Design of a CW Radio-Frequency Quadrupole (RFQ) for the Project X Injector Experiment (PXIE)* Abstract: The Project X Injector Experiment (PXIE)
Laboratori Nazionali di Legnaro (Italy) DTL design status A. Pisent.
Progress of the sub-harmonic bunching system (i.e. upgrading progress of BEPCII present bunching system) Pei Shilun for the SHBS team Accelerator center,
C. Rossi – L4 Project Meeting 3 March 2011 Status and Plans of 3 MeV Test Stand.
ESS End-to-End Optics and Layout Integration Håkan Danared European Spallation Source Catania, 6 July 2011.
Normal-Conducting Photoinjector for High Power CW FEL Sergey Kurennoy, LANL, Los Alamos, NM, USA An RF photoinjector capable of producing high continuous.
MICE RF Cavity Design and Fabrication Update Steve Virostek Lawrence Berkeley National Laboratory MICE Collaboration Meeting October 27, 2004.
MICE RF Cavity Measurements Derun Li Center for Beam Physics Lawrence Berkeley National Laboratory March 26, 2010 University of California, Riverside,
Injector RF Design Review November 3, 2004 John Schmerge, SLAC LCLS RF Gun Thermal Analysis John Schmerge, SLAC November 3,
Cell-Coupled Drift Tube Linac M. Pasini, CERN AB-RF LINAC4 Machine Advisory Committee 1 st meeting CERN January 29-30, 2008.
Alain FRANCE for the ESS RFQ Team at CEA Saclay
The LHC: an Accelerated Overview Jonathan Walsh May 2, 2006.
SRF Results and Requirements Internal MLC Review Matthias Liepe1.
RFQ Thermal Analysis Scott Lawrie. Vacuum Pump Flange Vacuum Flange Coolant Manifold Cooling Pockets Milled Into Vanes Potentially Bolted Together Tuner.
LINAC4 STATUS Alessandra M. Lombardi for the LINAC4 team 1.Motivation and goals 2.Status of Linac4 2 years after official start of the project ( )
Preliminary design of SPPC RF system Jianping DAI 2015/09/11 The CEPC-SppC Study Group Meeting, Sept. 11~12, IHEP.
Photocathode 1.5 (1, 3.5) cell superconducting RF gun with electric and magnetic RF focusing Transversal normalized rms emittance (no thermal emittance)
Low Emittance RF Gun Developments for PAL-XFEL
F.E.T.S. RFQ Mechanical Design by Peter Savage 7 th January 2010.
Anders Sunesson RF Group ESS Accelerator Division
J. Alessi RF Structures EBIS Project Technical Review 1/27/05 RF Structures J. Alessi Some general thoughts on what our approach will be.
January 5, 2004S. A. Pande - CAT-KEK School on SNS MeV Injector Linac for Indian Spallation Neutron Source S. A. PANDE.
Development of the Room Temperature CH-DTL in the frame of the HIPPI-CARE Project Gianluigi Clemente,
PROTON LINAC FOR INDIAN SNS Vinod Bharadwaj, SLAC (reporting for the Indian SNS Design Team)
CLARA Gun Cavity Optimisation NVEC 05/06/2014 P. Goudket G. Burt, L. Cowie, J. McKenzie, B. Militsyn.
Ding Sun and David Wildman Fermilab Accelerator Advisory Committee
Design Optimization of MEIC Ion Linac & Pre-Booster B. Mustapha, Z. Conway, B. Erdelyi and P. Ostroumov ANL & NIU MEIC Collaboration Meeting JLab, October.
MICE RF Cavity Measurements Derun Li Center for Beam Physics Lawrence Berkeley National Laboratory July 8, 2010 Rutherford Appleton Laboratory, UK.
Comparison of Fermilab Proton Driver to Suggested Energy Amplifier Linac Bob Webber April 13, 2007.
Concept Preliminary Estimations A. Kolomiets Charge to mass ratio1/61/8 Input energy (MeV/u) Output energy (MeV/u)2.5(3.5) Beam.
BEAM DYNAMICS IN A HIGH FREQUENCY RFQ Alessandra M Lombardi S. Myers : head of office for medical applications at CERN The “750MHz” team (layout and beam.
THE LINAC4 RFQ – Experience with Design, Fabrication and Tuning C. Rossi and the RFQ Project Team GSI Review – 20 November 2013.
ESS AD RETREAT 5 th December 2011, Lund “A walk down the Linac” SPOKES Sébastien Bousson IPN Orsay.
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.
D. Li and S. Virostek for PXIE RFQ team Center for Beam Physics Lawrence Berkeley National Laboratory March 6, 2012.
PXIE RFQ Engineering Design Steve Virostek Engineering Division Lawrence Berkeley National Laboratory April 10, 2012 Project X Collaboration
RFQ coupler S. Kazakov 07/28/2015. Requirements: Coupler requirements Expected problems: Heating (loop, ceramic window, etc.) Multipactor Solutions: Appropriate.
PXIE RFQ Derun Li Lawrence Berkeley National Laboratory PXIE Program Review January 16-17, 2013.
D. Li, Project X Collaboration Meeting, Fermilab (October 25-27, 2011) Overview of Project X Frond-End R&D at LBNL Derun Li Project X Collaboration Meeting.
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.
One More RFQ Design Renewal ANL Design. Several MHz RFQ Designs ANL-1LBNL-1LBNL-2ANL-2aANL-2b Vane modulation typeSinusoidal Sinusoidal +
Bunch Shape Monitor for HINS Wai-Ming Tam Project X Collaboration Meeting September 11, 2009.
Welcome to the RFQ Meeting
Bunching system for SPES project
Linac4 Beam Characteristics
Progress in the Multi-Ion Injector Linac Design
SPES-RFQ review Introduction, general aspects
Part2: Cavities and Structures
Update of CLIC accelerating structure design
CEPC RF Power Sources System
ADS Accelerator Program in China
LHC (SSC) Byung Yunn CASA.
Pulsed Ion Linac for EIC
Advanced Research Electron Accelerator Laboratory
Part2: Cavities and Structures
MEBT1&2 design study for C-ADS
Physics Design on Injector I
LCLS Injector/Diagnostics David H. Dowell, SLAC April 24, 2002
DTL M. Comunian M. Eshraqi.
ICAP 2006, Chamonix Mont-Blanc
Injector Physics C. Limborg-Deprey, D. Dowell ,Z. Li. ,H. Loos, J
Status of the JLEIC Injector Linac Design
Parameters Changed in New MEIC Design
Multi-Ion Injector Linac Design – Progress Summary
Presentation transcript:

Physics design on Injector-1 RFQ OUYANG Huafu

Contents RFQ R&D background at IHEP C-ADS RFQ design philosophy C-ADS RFQ dynamic design C-ADS RFQ structure design C-ADS RFQ water-cooling design and thermal analysis Summary

RFQ R&D background at IHEP A High-duty factor proton RFQ accelerator for ADS study has been constructed at IHEP (973 ADS RFQ) Nice performance with a transmission rate about 93% and an output beam current of 44mA with a duty of 7%. Progress in high-duty factor operation from about 7% to 15% is achieved 44.5mA pulsed current with a transmission about 93% and beam duty factor of 7.15%. 973 ADS RFQ in the installing process

RFQ R&D background at IHEP Main parameters of 973 ADS RFQ This 4.75 long RFQ consists of two segments, which are resonantly coupled by a coupling cell. Each segment is formed by two technical modules. Input Energy 75keV Output Energy 3.5MeV Peak Current 50mA Structure Type 4-Vane RF Frequency 352.2MHz Inter-vane voltage 65kV Maximum Surface E 33MV/m (1.8Kilp) Structure Power 458[1.4*PSuperfish (327kW)] Beam Power 175kW Total Power 638kW Total Length 4.75m One technical module (1.2m long)

C-ADS RFQ design philosophy A proper beam current (15mA), injection (35keV) and output (3.2MeV) energy.(beam requirement for C-ADS LINAC 10mA) An appropriate length. < 4.8m (Similar to 973 ADS RFQ, the foreseen RFQ will consist of 2 physical resonantly coupled segments, and each segment includes 2 technical modules with a length less than 1.2m) Higher beam transmission preferable. > 98% (beam loss worsens the deformation of RFQ, vice versa, deformation lows the beam transmission ) As low as possible for RF power dissipation per unit length and per area. (to this end, a low inter-vane voltage 55kV chosen) As low as possible for the output beam emittance. (0.2.mm.mrad/0.2 .mm.mrad/0.0612MeV.Deg)

C-ADS RFQ design philosophy 6. Redundant water-cooling capability and water-cooling control protection ways. 7. Conservative RF coupler design to low the load of RF coupler and ensure the reliability of coupler. (4 RF power coupler, 80kW for each RF coupler) 8. To take full use of the successful experiences of the former 973 ADS RFQ designing, machining and operation at IHEP. (similar structure is chosen as the former due to the near working frequency of the two RFQ)

C-ADS RFQ dynamic design The standard LANL chain of RFQ Codes Curli, RFQuick, Pari and Parmteqm are used to design the RFQ. For these codes, the design RFQ are physically divided into four sections, ie., Radial Matching Section (RMS), Shaper, Gentle Buncher (GB) and Accelerator. In order to get a good beam transmission and a better bunching, both the shaping and the bunching energy are chosen to be comparatively lower values. At present, the dynamic design is finished.

Table 1: Main RFQ design parameters Value Frequency (MHz) 325 Injection energy (keV) 35 Output energy (MeV) 3.2128 Beam current (mA) 15 Beam duty factor 100% Inter-vane voltage V (kV) 55 Beam transmission 98.7% Average bore radius r0 (mm) 2.775 Vane tip curvature (mm) r / r0 1.0 Maximum surface field (MV/m) 28.88 (1.62Kilp.) Cavity power dissipation (kW) 272.94 [1.4* Psuperfish (194.96)] Total power (kW) 320.94 Avg. Copper power/Length (kW/m)* 41.68   (Psuperfish) Avg. Copper power/Area (W/cm2)* 3.25   (Psuperfish) Max. copper power/Area (W/cm2)* 3.77  ( Psuperfish) Input norm. rms emittance(x,y,z)(πmm.mrad) 0.2/0.2/0 Output norm. rms emittance(x/y/z) (πmm.mrad/MeV-deg) 0.2/0.2/0.0612 Vane length (cm) 467.75 Gap1(entrance) (cm) 1.10 Gap2(exit) (cm) Accelerator length (cm) 469.95

C-ADS RFQ dynamic design Main parameter variation with cell number

C-ADS RFQ dynamic design The beam transmission is about 98.7%

C-ADS RFQ dynamic design Particle distributions in phase space at the entrance and exit of RFQ

C-ADS RFQ dynamic design Transmission versus input beam parameters

C-ADS RFQ structure design RFQ consists of 2 physical resonantly coupled segments, and each segment includes 2 technical modules connected together with flanges. 4 four dipole rods are installed on the entrance plate, both sides of the coupling plate and the end plate. There are 64 plug tuners with a diameter of 55mm and nominated penetration of 5.2mm into the cavity. 16 vacuum port bodies will be machined separately and then brazed together with RFQ cavity. There are 8 RF coupler ports and 4 ports will be used. At present, the structure design is basically finished. The mechanical length for the for the 4 modules (1) 1176.558 mm (2) 1162.329mm (3) 1183.657mm (4) 1176.928 mm. One quadrant of the RFQ 3-dimension structure

C-ADS RFQ structure design Similar structure as the former 973 ADS RFQ at IHEP is chosen due to the near working frequency of the two RFQ, highly time-saving in optimization of the structure and the mechanical drawing afterwards. One quadrant of the RFQ transverse shape

C-ADS RFQ structure design Nominated penetration of 0.7mm into the cavity compensates the frequency drop caused by the vacuum port. Shape and size of the vacuum port

C-ADS RFQ structure design Thickness: 18mm Shape and size of the coupling plate

C-ADS RFQ structure design Position: (31.719,31.719) Diameter: 15mm Length: 169 mm Position, shape and size of the dipole stabilization rod

C-ADS RFQ structure design The shape and size of the beginning cell, the coupling cell and the end cell

C-ADS RFQ structure design The frequency interval between the operation quadrupole mode and its neighboring quadrupole modes is about –3.6MHZ and 3.5MHZ. For 973 ADS RFQ, the value is +-3MHZ.

C-ADS RFQ structure design The frequency interval between the operation quadrupole mode and its neighboring dipole modes is about –5.4MHZ and 5.55MHZ. For 973 ADS RFQ, the value is +-5MHZ.

C-ADS RFQ water-cooling design and thermal analysis Water-cooling serves two functions in an RFQ. One is to take away the power dissipated on the inside surface of the RFQ by the RF field to maintain the thermal stability and to limit the deformation of RFQ. The other is to be used to tune the RFQ basically without effecting the field distribution profile when the RFQ is out of resonance, since the beam transmission of RFQ is very sensitive to the field profile, the ordinary frequency tuning method by the movable tuners is no more adopted in a RFQ operation.

C-ADS RFQ water-cooling design and thermal analysis Water-cooling components: 4 cavity bodies (vanes and walls) 64 tuners 16 vacuum ports 4 RF power couplers 2 end plates and 8 rods on them 1 coupling plate and 8 rods on it

C-ADS RFQ water-cooling design and thermal analysis

C-ADS RFQ water-cooling design and thermal analysis Tunnel temperature choice: 20oC The thermal analysis model of ANSYS (1/8 cross section of RFQ)

C-ADS RFQ water-cooling design and thermal analysis Temperature rise at the end of module versus velocity of the cooling-water

C-ADS RFQ water-cooling design and thermal analysis The maximum deformation versus velocity of the cooling water

C-ADS RFQ water-cooling design and thermal analysis The frequency drift Δf at the end of module versus velocity of the cooling water

C-ADS RFQ water-cooling design and thermal analysis Positions of the water channels vary with the velocity of the cooling water

C-ADS RFQ water-cooling design and thermal analysis The optimization results Tunnel temperature choice: 20oC Temperature of cooling water: Velocity of cooling water: 3.5m/s Positions of water channels: Channel 1 (0.00,33.00) Channel 2 (0.00,58.00) Channel 3 (0.00,93.60) Channel 4 (43.0,103.0) The optimization of water-cooling channel positions for the velocity 3.5m/s of the cooling water and water temperature of 20 0C.

C-ADS RFQ water-cooling design and thermal analysis To tune the RFQ basically without effecting the field distribution profile when the RFQ is out of resonance. The frequency shift sensitivity to the temperature is about -5 kHz/ oC. The frequency shift versus the water-cooling temperature

Water-cooling design and thermal analysis (tuning) In a RFQ operation, to tune RFQ by adjusting the vane water temperature when RFQ is out of resonance. The frequency shift sensitivity to the vane water temperature is about -50 kHz/ oC when Twall=20 oC. The frequency shift sensitivity to the wall water temperature is about 42 kHz/ oC when Tvane= 20 oC. The frequency shift versus the vane water temperature at Twall=20 oC The frequency shift versus the wall water temperature at Tvane=20 oC

Summary A good dynamic design with high beam transmission, low power dissipation and low longitudinal emittance is got. RFQ structure design proceeds well and rapidly due to much experience from the former 973 ADS RFQ built at IHEP. Two dimension thermal analysis is used for the water-cooling design. Three dimension thermal analysis will be just used for checking the water-cooling design. Mechanical design is being taken based on the present physical design.

THANK YOU!