insulation materials Simon Canfer Technology Department Rutherford - - PowerPoint PPT Presentation

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insulation materials Simon Canfer Technology Department Rutherford - - PowerPoint PPT Presentation

Radiation damage issues for superconducting magnet insulation materials Simon Canfer Technology Department Rutherford Appleton Laboratory November 2010 STFC Science and Technology Facilities Council One of the UK Research Councils


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Radiation damage issues for superconducting magnet insulation materials

Simon Canfer Technology Department Rutherford Appleton Laboratory November 2010

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STFC

Science and Technology Facilities Council One of the UK Research Councils

  • Harwell Science and Innovation Campus

RAL, Diamond...

  • Daresbury Science and Innovation

Campus

  • UK Astronomy Technology Centre
  • Subscriptions to CERN, ILL,...

Image: CERN

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Superconducting magnet heritage at RAL

Detector magnets: Delphi, H1, ATLAS End Caps Accelerator dipole magnet projects: Next European Dipole (EU FP6), CERN EuCARD High Field Magnets (EU FP7)

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CERN High Field Magnet programme

To develop technology for LHC upgrade scenarios Aims to build a 13T, 100mm dipole “FRESCA 2” for the FRESCA test facility at CERN (compared to 8T in LHC NbTi dipoles) Block coil design, Nb3Sn VHFM insert, +6T in High Temp Superconductor

Baseline block cross section (a quarter shown). The field in the coil is computed for a 13 T bore field.

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CERN HFM Nb3Sn magnet design borrows concepts from the American LARP “HD2”

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Magnet “Insulation” Materials

Electrical insulation between turns and to ground But just as important,

  • “Insulation” forms a monolithic, mechanically stable structure
  • Form a coil pack for assembly into magnet structure
  • To resist and transmit Lorentz forces during operation,

high compressive strength (300MPa) and shear strength (100MPa)

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Polymer Composites

  • Advantages of thermoset composites:
  • suitable for low volume production runs, using vacuum

impregnation to form high quality composites

  • easily available
  • relatively cheap
  • Chemistry can be varied to give a very wide range of

properties including relatively high radiation resistance (cf other polymers)

  • E.g. Formulations for ATLAS End Cap Toroids and

“RAL 71A”, developed at RAL

  • What are the disadvantages?
  • Can have low radiation hardness so polymer dictates

magnet lifetime

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Known radiation dose limits for polymers

Many factors influence rad-hardness, including: Material: Epoxy resin structure, curing agent structure, cure schedule... Radiation: environment, temperature, dose, dose rate, particle type, particle energy, synergistic effects... Testing: test type, temperature, rate, environment since irradiation... But in general, in the environments tested to date, we know: tens of MGy for linear chain epoxies, up to 200MGy and beyond for aromatic structures (CERN Yellow reports, Tavlet et al)

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Dose 10MGy, neutron flux 1022N/m2 Interest in cyanate ester/epoxy blends for ITER TF coil insulation Tests to date (fission reactor irradiation) are encouraging How do they compare with best epoxies? How does existing test data relate to high energy physics applications?

ITER TF coils

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Effect of particle type

Neutrons – highly penetrating, lead to knock-on protons Protons- charged, so not highly penetrating but highly damaging Gamma- interaction with orbital electrons, forming ions and radicals Ideally we should consider more than just dose... Radiation types do have different effects on polymers:

  • Egusa 1991, reported glass/epoxy up to 2.6 times more

sensitive to neutrons than gamma

  • Abe 1987 reported 14MeV neutrons are eight times more

damaging than Co-60 gamma to polyimide (Kapton DuPont (R))

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What properties to test?

Classical mechanical properties can be useful, esp. Short beam shear as it tests the glass/polymer interface. Electrical testing is more sensitive than mechanical testing to radiation damage FTIR and thermal methods in use at RAL (e.g. DMA, DSC, TGA) useful and use minimal material. They provide information

  • n radiation-induced chemical change.

Ideally we would test materials beyond the expected lifetime dose using expected conditions but this is often impossible

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Opportunities

Many projects are undertaking irradiation programmes, opportunity for synergies Take advantage of the long term nature

  • f NF/MC to launch irradiation testing

Radical new approaches and inorganic materials?

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Conclusions

Some polymers have been shown to be useful up to hundreds of MGy dose Polymers usually dictate the lifetime of a magnet in a radiation environment There is a lack of data at high doses owing to the long irradiation times required There could be a need for inorganic materials, but bear in mind the processing advantages of current (organic) materials

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Extra slides

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Effect of epoxy chemistry

  • n radiation hardness

High functionality epoxies with aromatic hardeners are more radiation-stable compared to “standard” epoxies (Evans) In HFM we plan to test cyanate esters, trifunctional epoxy

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What are epoxy resins?

A family of materials characterised by the epoxide ring structure. Useful epoxy materials have more than one epoxy ring that reacts to produce a thermoset material of high molecular weight. The chemical structure of the epoxy resin, and curing agent, is varied to produce a wide variation of thermal and mechanical properties. Therefore it is vital to specify both the resin and curing agent when referring to “epoxies”

C C O

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Case Study: Atlas End Cap Toroid Magnets

Superconducting Magnet Coils Cold Mass 160 Tonnes @ 4.5K Thermal Radiation Shield Vacuum Vessel

Diameter 11m Length 5m Stored Energy 200MJ Operating Current 20kA Peak Magnetic Field 4.7T Overall Mass 239 Tonnes

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Case Study: Requirements

REQUIRED: A resin system with low viscosity and long working time, together with high modulus, tensile strength and work of fracture at low temperature.

EXISTING SYSTEMS: System Advantages Disadvantages _ DGEBA/MTHPA Low viscosity Low work of fracture High modulus/UTS Long working time DGEBA/POPDA Low viscosity Short working time High modulus.UTS High work of fracture

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Case Study: The Molecules

CH2 CH2 CH2 CH2 CH3 CH3 CH CH C O O O O

resin

O 3 CH O O C C

MTHPA hardener: stiff

H 2 N H CH CH O CH 2 CH 2 3 CH 3 CH N 2 n=5.6

POPDA: flexible

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Case Study: Characterising

Modulus at 293 K

1.6 1.8 2 2.2 2.4 2.6 2.8 3 3.2 10 20 30 40 50 60

Weight% PPGDGE Modulus /GPa

Viscosity vs Time: 300 g sample at 50'C

200 400 600 800 1000 5 10 15 20 25 30

Time / hrs Viscosity / cps

DGEBF / DETD DGEBF / DETD / 30% PPGDGE DGEBA / POPDA DGEBF / MTHPA

Bond Strengths at 4.2K

50 100 150 200 250 300

DGEBA / MTHPA DGEBA / POPDA DGEBF / DETD DGEBF / PPGDGE (30%) / DETD

Bond Strength / MPa

Range

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Atlas Manufacture 1

Base Plate Cleaning Conductor Wrapping Coil Winding

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Atlas Manufacture 2

Assembled Coil Vacuum Impregnation Impregnated Coil

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Atlas Manufacture 3

Coil Breakout Assembly Completed “Cold Mass”

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Atlas Manufacture 4

Barrel Magnet In Vacuum Vessel Finished Magnet

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Atlas Manufacture 5

Lowering into Cavern Moving into Position Final Resting Place

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Magnets for Accelerators

Other People’s Business

  • synchrotrons need powerful magnets to

bend the particle beam

  • State of the art today is 8 Tesla
  • The next step for the LHC will need

double the field of todays magnets: 15 Tesla or 300 000x earth’s magnetic field

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Other People’s Business

¼ Symmetry model geometry Deflection due to magnetic loads only

  • Only one superconductor material is feasible today:

niobium-tin

  • The whole magnet needs heat treating in vacuum at 700°C
  • How do we insulate between the magnet windings?

Forces of 100 tonnes per metre of magnet length

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The first heat treated coil

A testbed for a record- holding European superconductor

Other People’s Business