Fabrication of CLIC X-band RF structures and RF components

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[email protected] 21-Oct-2010 Holland@CERN Fabrication of CLIC X-band RF structures and RF components G. Riddone OUTLINE ° Two-beam module ° RF accelerating structures ° Power extraction and transfer structures ° RF components

Transcript of Fabrication of CLIC X-band RF structures and RF components

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10-Nov-2010 1 Holland@CERN21-Oct-2010 Holland@CERN

Fabrication of CLIC X-bandRF structures and RF components

G. Riddone

OUTLINE° Two-beam module ° RF accelerating structures° Power extraction and transfer structures° RF components

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10-Nov-2010 2 Holland@CERN

MAIN LINAC – TWO-BEAM MODULE

CLIC at 500 GeV (4248 modules)26312 Accelerating structures13156 PETS~ 70000 RF components

CLIC at 3 TeV (20924 modules)142812 Accelerating structures71406 PETS~ 400000 RF components

A. Samoshkin

(POWER EXTRACTION AND TRANSFER SYSTEM)

MAIN BEAM

DRIVE BEAM

Up to 8 accelerating structures and 4 PETS in a two-beam module

Prototype modules (20) 2016Few 100’s RF structures and components

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RF STRUCTURES AND COMPONENTS

3

TD18#3 at SLAC

TD18#2 at KEK

TD24#2 at CERN (12 GHz)

PETS (12 GHz, TBTS)

PETS (11.4 GHz, test at SLAC)High-power dry load Hybrid

Variable high power splitter

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ACCELERATING STRUCTURES

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Test structures

CLIC accelerating structures

DisksCouplersCooling circuits

DisksCouplersCooling circuits [~400 W average per structure]Vacuum manifolds (10-9 mbar)Damping materialSuperstructures (2 to 4)

ACCELERATING STRUCTURES

L ~300 mm

L = 500 mm

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ENGINEERING DESIGN ISSUES (WAVEGUIDE DAMPED AS)

Iris

12WDSDVG1.8_R05

0.005 A B

Geometrical tolerance of this zone

// 0.002 A

0.001

PREP

ARE

D B

Y A

. SO

LOD

KO

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CLIC’s needs: shape accuracy ± 2.5 µmroughness Ra 25 nm

S. ATIEH

WHY WE NEED ULTRA-PRECISION MACHINING

Accelerating structures– Milling and turning

PETS– Milling

Diamond tool is required (about 7 tools per disks)

- Dimensional stability

- Maintenance of tolerances

- Less stresses

- Chips do not adhere to surface

- Expensive → well characterised

At this level of tolerances: material stress-relief annealing is mandatory → Soft material → • Special care clamping without damage• Special requirements on 3D metrology (tactile): no indents!!

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TYPICAL PROCEDURE OF UHP DISKMACHINING

Pre-Fabrication:Pre-turning + x100 μmPre-milling + x100 μmTuning holesStress relief ~180 °C (optional)Finish turning + x10μmFinish milling + x10μmStress relief ~245 °C

UHP-Machining:Mounting of vacuum clamping adapterUHP-turning of the support (diamond tools)AlignmentUHP-turning ref. plan A AlignmentUHP-turning opposite sideWave guide UHP millingIris final turning (requested up to the nose)

S. ATIEH

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DETUNED DAMPED DISK FROM VDL (TD24)

Zeiss CMM, free state measurement

• Shape accuracy 5 µm 2.6 µm achieved

• Roughness Ra 0.025Iris region achieved Ra 0.016

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ASSEMBLY PROCEDURE

Diamond machining (sealed structures)

H2 diffusion bonding/brazing at

~ 1000 ˚C

Surface treatment -cleaning with light etch

Vacuum baking650 ˚C > 10 days

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ALIGNMENT AND BONDING Reference on the external diameter: - tolerance on external diameter: 12.5 µm- tolerance on the ref. line: 1 µmAlignment done on a V-shape vertical support in granite (accuracy of 1.5 µm)

Operation done under laminar flow

Straightness measurementT24: 3.5 µm

Individual inspection

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DIFFUSION BONDING PARAMETERS AND CYCLE

Temperature: up to 1040 ˚CPressure: 0.28 MPaHolding time: 2 h

Nominal diffusion bonding cycle (under 25 mbar H2)

New infrastructure to guarantee uniform load

Straightness measurement after diffusion bonding: variation of 1 µm before and after bonding

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MACHINING AND DIFFUSION BONDING ISSUES

MILLINGTURNING

GRAINS CROSSING THE JOINING PLANE

VACUUM

DIFFUSION BONDING (H2 better surface)

MACHINING (as much turning as possible!)

H2 (no faceting!)

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1. Diffusion bonding of highprecision disk stack

2. Brazing of the manifolds by means of Gold-electroplating (validation tests needed)

3. Brazing of cooling fitting adapters

RF INTERFACE FLANGE

COOLING FITTING ADAPTER

MANIFOLD BODY

WFM WAVEGUIDE

WAVEGUIDE

ACCELERATINGSTRUCTURE

GOLD-ELECTROPLATING

ASSEMBLY OF ACCELERATING STRUCTURES (1/2)

D. GUDKOV, A. SOLODKO

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4. Brazing of prepared acceleratingstructure stack (superstructure)

5. Installation of damping material6. Welding (EBW) of manifold covers

ASSEMBLY OF ACCELERATING STRUCTURES (2/2)

D. GUDKOV , A. SOLODKO

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PETS

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FABRICATION OF PETS AT 11.4 GHz

PETS for feasibility demonstration- successfully tested at SLAC

Coupler

Minitank with bars inside

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SHAPE ACCURACY OF PETS AT 11.4 GHz

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ASSEMBLY OF PETS AT 11.4 GHz

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PETS OCTANT FOR TEST BEAM LINE

• Shape accuracy 4.8 µm (15 µm nominal)

• Roughness Ra 120 -180 nm(100 nm nominal)

KERN Micro- und Feinwerktechnik GmbH (DE)

L = 800 mm

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RF COMPONENTSCurrent needs for CERN and several collaborators

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HIGH POWER DRY LOADS

Internal shape

Broadband: 11.4 GHz and 12 GHz (design made by CERN)

Ferritic stainless steel SS430ripple shape tolerance = 0.01 mmflatness accuracy 0.01 mmripple shape roughness Ra 0.4.

RF measurements-28.5 dB 11.424 GHz -36.3 dB 11.994 GHzDesign (HFSS): -39.5 dB 11.424 GHz

-30.7 db 11.992 GHz

Successfully tested at high power at KEK

L ~ 0.8 m

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HIGH POWER COMPACT DRY LOADS

Water cooled load

Ceramic (SiC) - 3 mm Cu coating needed

Cu OFE body brazed to the RF flanges and to SiC inner part

L ~ 0.3 m

V. SOLDATOV

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OTHER RF COMPONENTS

Hybrids Splitter RF flanges and waveguides

Directional couplers

Phase shifter

Variable Power AttenuatorDesign made by the company

Design made by CERN

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CLIC TENTATIVE SCHEDULE

Final CLIC CDR andproposal next phase

@ CERN Council

European Strategyfor Particle Physics

@ CERN Council

Project Implementation Plan (PIP) andproposal for next phase

Draft ConceptualDesign Report (CDR)

2010 2011 2012 2013 2014 2015 2016 2017 2018

Feasibility issues (Accelerator&Detector) Conceptual design & preliminary cost estimationEngineering, industrialisation & cost optimisation ?Project Preparation Project Implementation ?

JP. Delahaye

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• Future needs for RF structures and RF components are increasing:– Conceptual design phase will be followed by a technical design phase

from 2011 to 2016 (project preparation)

• Production of RF accelerating structures and PETS is very challenging: for future CLIC structures all technical systems will have to be integrated

• Micro-precision tolerances imply dedicated machining and assembly procedures: qualification of firms for fully equipped RF structures and components is mandatory

• Industrialization studies need to be conducted with companies

CONCLUSIONS