LCWS11 WG4 Fully featured accelerating structure engineering design

Slides:



Advertisements
Similar presentations
COOLING TUBE ACCELERATING STRUCTURE MANIFOLD COUPLER VACUUM INTERFACE FLANGE RF INTERFACE FLANGE TUNING STUD ENGINEERING DESIGN AND FABRICATION OF X-BAND.
Advertisements

CLIC two-beam module integration issues 4 th CLIC Advisory Committee (CLIC-ACE), May 26-28, 2009 CLIC two-beam module integration issues G. Riddone on.
CLIC08 workshop Structure production: CERN activities and Master Schedule G. Riddone, W. Wuensch, R. Zennaro, Contributions from C. Achard, S. Atieh, V.
MICE RF and Coupling Coil Module Outstanding Issues Steve Virostek Lawrence Berkeley National Laboratory MICE Collaboration Meeting October 26, 2004.
PETS components and waveguide connections CLIC Workshop 2007 David Carrillo.
Vacuum Vessel Production Readiness Review
Status of the LARP Phase II Secondary Collimator Prototype 30 September 2013 LHC Collimation WG Meeting Tom Markiewicz/SLAC BNL - FNAL- LBNL - SLAC US.
Integration of Cavities and Coupling Coil Modules Steve Virostek Lawrence Berkeley National Laboratory MICE Collaboration Meeting March 28 – April 1, 2004.
Richard F Boyce Injector UpdateL0-1 Accelerator 3 November L0-1 Design, Manufacturing & Testing R. F. Boyce, SLAC.
Status of the LARP Phase II Secondary Collimator Prototype 14 October 2013 LHC Collimation WG Meeting Tom Markiewicz/SLAC BNL - FNAL- LBNL - SLAC US LHC.
1 RF-Structures Mock-Up FEA Assembly Tooling V. Soldatov, F. Rossi, R. Raatikainen
Structure stacking alignment tolerances CLIC Workshop January 2015 CERN Anastasiya Solodko, on behalf of the CLIC study team.
Vacuum, Surfaces & Coatings Group Technology Department Vacuum tests for CLIC module prototypes 6 November 2013 C. Garion2 Outline: Reminder: specification.
2 nd collaboration meeting on X-band Accelerator Structure Design and Test-Program Structure fabrication Comparative analysis of disk and quadrant manufacture.
1 TD26_CC_SiC 06-September-2011 Assembly procedure of TD26_CC_SiC F. Rossi.
K. Alam, CLIC workshop, October 16-18, CLIC workshop, October 2007 Working group “ Two beam hardware and integration” Test module in the two.
CIEMAT CONTRIBUTION TO TBL PETS (January 2009) David Carrillo on behalf of the Accelerators Team.
ENGINEERING DESIGN AND FABRICATION OF PETS V. Soldatov¹, D. Gudkov¹, I. Syratchev², A. Samoshkin¹, G. Riddone², A. Olyunin¹, S. Atieh² 1 – JINR, Dubna,
Status of vacuum & interconnections of the CLIC main linac modules C. Garion TE/VSC TBMWG, 9 th November 2009.
International Workshop on Linear Colliders 2010 Design and fabrication update on PSI/Trieste X-band phase- space rotator structure Dmitry Gudkov 21-OCT-2010.
INTEGRATION OF RF STRUCTURES IN THE TWO-BEAM MODULE DESIGN G. Riddone, CERN, Geneva, Switzerland A. Samoshkin, D. Gudkov, JINR, Dubna, Russia Abstract.
RF power & FPC status Eric Montesinos, CERN BE-RF on behalf of all people involved, great thanks to all of them !
PETS EuCARD. Present status and precision assembly L. Sánchez, F. Aragón, J. Calero, J.L. Gutiérrez, E. Rodríguez, F. Toral, CIEMAT 26/10/2011.
CLASSE prototype: mechanical concepts G. De Michele, EPFL-PSI-CERN on behalf of CERN team SLAC, 16 th April, 2012.
1 Status of the CLIC two-beam module program A. Samochkine, G. Riddone Acknowledgements to the Module WG members 4 February 2014 CLIC Workshop 2014 (3-7.
ISTC Project #3888 Development, manufacture and experimental investigation of a unique pilot CCDTL accelerating section in the energy range of MeV.
ENGINEERING DESIGN AND FABRICATION OF X-BAND DAMPED DETUNED STRUCTURE V. Soldatov¹, D. Gudkov¹, A. Samoshkin¹, G. Riddone², A. Grudiev², S. Atieh², A.
1.3GHz Input Coupler for ILC
TM0 components inventory and procurement schedule In LAB testing facility A. Bartalesi.
CLIC08 workshop CLIC module layout and main requirements G. Riddone, on behalf of the CMWG Home page of the TBM WG:
1 Thermal tests planning for mock-up TM0 Thermal tests planning for CLIC prototype module type 0 May 30th,
Fabrication and measurement of RF components for CLIC study
Manufacturing process, validation and factory test
1 Assembly and installation of TM0 Lab components Assembly and installation of TM0 Lab components F. Rossi.
cern.ch 1 A. Samoshkin 28-Feb-2011 Progress on CDR module design.
cern.ch International Workshop on Linear Colliders 2010 CLIC TWO-BEAM MODULE DESIGN & INTEGRATION 21-Oct-2010 WG 8 «TECHNICAL SYSTEMS»
ENGINEERING DESIGN AND FABRICATION OF X-BAND ACCELERATING STRUCTURE TD24 WITH WFM Abstract To achieve high luminosity in CLIC, the accelerating structures.
1 Thermal tests planning for mock-up TM0 Thermal tests planning for CLIC prototype module type 0 July 17,
Main features of PETS tank J. Calero, D. Carrillo, J.L. Gutiérrez, E. Rodríguez, F. Toral CERN, 17/10/2007 (I will review the present status of the PETS.
1 Assembly and installation of TM0 in the Lab Assembly and installation of TM0 in the Lab F. Rossi September.
1 Assembly procedure for PETS and AS 11-July-2011 Assembly procedure of PETS and AS for T0 module Lab F.
5 th CLIC-ACE Structure production in laboratories and industries G. Riddone, 02/02/2010 (contribution from KEK/SLAC colleagues) 1.
Engineering design of the V-supports J.Huopana Input from: G.Riddone, A.Samoshkin, R.Nousiainen, D.Gudkov, N.Gazis.
Xx-xx-2010, tanks arrive from Snezhinsk to Novosibirsk A.Tribendis, July 19-21, 2010, Snezhinsk 1. Check cavity dimensions on a CMM 2. Assemble and measure.
TBTS Test Program & Schedule G. Riddone
cern.ch CLIC MEETING (17-Dec-2010) CLIC TWO-BEAM MODULE LAYOUT (short introduction) BE / RF 1.
TD26CC PLANS FROM CIEMAT Laura Sánchez on behalf Electrical Engineering Group of CIEMAT.
7-Sep-2011 CLIC RF Structure Development Meeting «BE/RF» TD26 WITH COMPACT COUPLER FOR CLEX (TD26 CC SiC) ENGINEERING DESIGN this structure will be used.
MICE RFCC Module Update Allan DeMello Lawrence Berkeley National Lab MICE CM25 at RAL, UK November 6, 2009.
Gravity load on SAS – comparison between real and mock-up April 13 th, 2016.
DTL prototype summary and production sequence F.Grespan LNL _06_22 CDR.
02-Dec XB Dec-2010 XB-10 Engineering design, production and follow-up of X-band RF components G. Riddone in collaboration.
ESS DTL: Prototyping M.Comunian - F. Grespan – P. Mereu Lund– 10/04/2013F.Grespan.
PXIE RFQ Engineering Design Steve Virostek Engineering Division Lawrence Berkeley National Laboratory April 10, 2012 Project X Collaboration
Franck PEAUGER – CEA SACLAY LCWS11 - Grenada 29 th September 2011 CEA SACLAY CLIC R&D Activities F. Peauger, A. Hamdi, M. Desmons, W. Farabolini, P. Girardot.
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.
SPS High Energy LSS5 Thermal contact & cooling aspects
GOLD- ELECTROPLATING COOLING FITTING ADAPTER ACCELERATING STRUCTURE CONCEPTUAL DESIGN OF X-BAND ACCELERATING STRUCTURE TD26 CC SIC Abstract Many accelerating.
Module layout and types Two-beam module review, September 2009 Module layout and types G. Riddone for the CMWG,
Status of the CLIC module R&D G. Riddone on behalf of the CLIC module WG (special contributions from A. Samoshkin, D. Gudkov, A. Solodko, N. Gazis)
Work on PETS Developed at CIEMAT. L. Sánchez ICWS September Work on PETS Developed at CIEMAT Laura Sánchez on behalf of Accelerator Technology.
Two-beam module layout
Status of CIEMAT work on PETS
ISTCInternational Science and technology Center, MoscowOfficial Coordinator BINPBudker Institute of Nuclear Physics of Siberian Branch of Russian Academy.
Wideband kickers Mechanical design and Fabrication
CLIC WORKSHOP January 2013 BODYCOTE Your main sub-contractor for thermal processes Raymond SAEZ-Patrick JACQUOT.
List of changes and improvements for the next generation CLIC module
Design of Distribution Feedbox at LHC P7
LARP Phase II Secondary Collimator RC-1
Undulator System Components Status Dean Walters
Presentation transcript:

LCWS11 WG4 Fully featured accelerating structure engineering design G. Riddone on behalf of the eng. design team (great contribution from A. Solodko) 28.09.2011

Contents Introduction Mechanical Design of Copper Discs and Compact Couplers Mechanical Design of Vacuum Manifolds Wake Field Monitor Design Interconnection Design Alignment Features Super Structure Main Assembly Steps Dedicated Tests Conclusions

1st AS 2nd AS LSAS=502.5mm (1/4LMODULE) Introduction 1. Each Accelerating Structure consists of: 26 regular cells with four damping waveguides 2 compact coupler cells with two damping waveguides and other two opposite waveguides for WR90 connections 2. 4 WFMs are integrated in the first cell of the second AS COMPACT COUPLER WR90 WFM BEAM DIRECTION 1st AS 2nd AS LSAS=502.5mm (1/4LMODULE)

Engineering Design Overview COOLING TUBE VACUUM MANIFOLD & COOLING SYSTEM COOLING FITTING WAVEGUIDE INTERCONNECTION WFM WAVEGUIDE VACUUM FLANGE BONDED DISC STACK RF FLANGE ALIGNMENT VACUUM PORT BEAM DIRECTION BEAM DIRECTION 1st AS 2nd AS 243.701 mm 502.5 mm Compact coupler design (already in TD26 CC); The body of an AS formed by high-precision copper discs joint by diffusion bonding at 1040 °C; Two AS are brazed together to form a superstructure (SAS); The SAS has 8 vacuum manifolds and 4 Wakefield Monitor (WFM) waveguides; The cooling system is integrated into the vacuum manifolds in order to provide a more compact technical solution.

Mechanical Design of Copper Discs and Compact Couplers Compact Coupler Cell Cell with Alignment Features Regular Cell

Mechanical Design of Copper Discs and Compact Couplers • Cell shape accuracy 0.005 mm • Flatness accuracy 0.001 mm • Cell shape roughness Ra 0.025 μm

Mechanical Design of Vacuum Manifolds Interface for WFM WG Interface for supporting system Type 1 Type 2 Type 6 Type 2 Type 5 Type 4 Type 1 Type 3 Interface for WG (x2) Pumping the SAS Type 6 Interface for WFM WG Interface for WG Type 3 Interface for WG (x2) Type 4 Interface for WFM WG Interface for WG Pumping the SAS Type 5

Mechanical Design of Vacuum Manifolds • Waveguide shape accuracy 0.02 mm • Waveguide surface roughness Ra 0.1 μm

Mechanical Design of Vacuum Manifolds The vacuum manifolds combine a number of functions: Damping. Silicon carbide absorbers are fixed inside each manifold for effective damping of HOMs. Vacuum pumping. Two of the eight vacuum manifolds are equipped with vacuum flanges. Cooling. Two internal cooling channels for the water flow are presented in each manifold. COOLING TUBE COOLING FITTING CHANNEL VACUUM PORT DAMPING MATERIAL CORNER SUPPORT VENTED SCREW

Wakefield Monitor Design WFM: accuracy of 5 μm; Four WFM are integrated in the first cell of the second AS. DAMPING MATERIAL WFM WAVEGUIDE TM-LIKE MODE PICK-UP TE-LIKE Custom design of feedthrough ST.STEEL ADAPTER FLANGE Required tolerances Waveguide shape tolerance ±10 μm Waveguide surface roughness Ra 0.1 μm

Interconnection Design SAS (N+1) EDGE WELDED BELLOWS QUICK CF CLAMP CHAIN XS40 VACOM SAS (N) DAMPING MATERIAL QUICK CF FLANGE Stretched length ~+30% Press formed length ~-70% Requirements Keeping low pressure 10-9mbar; Electrical continuity with low impedance; Damping material must be used to avoid wakefields; Be flexible; Be compact. * Agreed with Vacuum Group

Alignment Features ST.STEEL INSERT TUNING STUD REFERENCE CONICAL BORE Placed on the external reference surface of AS; Stainless steel inserts are brazed to the tuning holes; 8 stainless steel inserts per one AS; Conical bore on the insert top to provide a reference for the measuring arm; The recorded coordinates of all points help to determine the AS beam axis and to align the AS properly.

Super Structure Main Assembly Steps 1a. Brazing of the vacuum manifold bodies, cooling adapters and cooling caps 1c. Brazing of the waveguides 1e. Brazing of the waveguides and RF flanges 1d. Machining of the waveguides x 8 x 8 1b. Brazing of the WFM waveguides 2. Brazing of the pre-assemblies to the vacuum manifolds x 4 x 8

Super Structure Main Assembly Steps 3. Diffusion bonding of 2 disc’s stacks 4. Brazing of the vacuum manifolds and interconnection bellows to the bonded disc’s stack 5. Brazing of the two equipped stacks to form a superstructure 6. Installation of the silicon carbide damping loads

Super Structure Main Assembly Steps 7. EBW of the vacuum manifold covers, vacuum flanges, feedthroughs 8. Installation of cooling fittings and tubes Intermediate leak tests and alignment verifications

Test Program. Bonding This will be done before for TD26 CC Option 1: - 2 sets of regular discs Could be the problem regions for bonding Option 2: 2 sets of special discs Option 3: 2 sets of special discs

Test Program. Brazing * Courtesy of Serge Lebet Option 1: (hard to realize in a real structure) Ni, Cu, Au Disk Copper Nickel 4 um Copper 15 um Gold 15 um Could be a critical region for brazing Option 2: (hard to realize in a real structure) Ag 10 microns Disk copper Silver 10 um on one disk Option 3: (hard to realize in a real structure) Ag 15 microns Disk copper Silver 15 um on one disk Option 4: (already validated for couplers and cooling circuits) Au/Cu 50/50 foil, h=0.05mm Disk copper Au/Cu foil Disk copper * Courtesy of Serge Lebet

Engineering design under completion Conclusions Engineering design under completion It is foreseen to order fully equipped SASs to be tested in CLEX modules (June 2012) A “version” for the stand-alone test stand will also be needed First time we develop a fully equipped accelerating structure: main assembly steps under validation with mock-ups to be installed in dedicated modules

Workpackage