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Metallographic analysis of 11 T dipole coils for High Luminosity-Large Hadron Collider (HL-LHC)

TLDR
In this paper, the authors present evidence of cracking of the brittle Nb3Sn filaments in a prototype dipole that resulted in degraded magnet performance, which can be attributed to an issue with the collaring process that is required in the assembly of dipole accelerator magnets.
Abstract
For next-generation accelerator magnets for fields beyond those achievable using Nb–Ti, Nb3Sn is the most viable superconductor. The high luminosity upgrade for the Large Hadron Collider (HL-LHC) marks an important milestone as it will be the first project where Nb3Sn magnets will be installed in an accelerator. Nb3Sn is a brittle intermetallic, so magnet coils are typically wound from composite strands containing ductile precursors before heat treating the wire components to form Nb3Sn. However, some mechanical assembly is still required after the coils have been heat-treated. In this paper, we present direct evidence of cracking of the brittle Nb3Sn filaments in a prototype dipole that resulted in degraded magnet performance. The cracking of the Nb3Sn, in this case, can be attributed to an issue with the collaring process that is required in the assembly of dipole accelerator magnets. Metallographic procedures were developed to visualize cracks present in the cables, along with quantitative image analysis for location-based crack analysis. We show that the stresses experienced in the damaged coil are above the critical damage stress of Nb3Sn conductor, as evidenced by a measured Cu stabilizer hardness of 85 HV0.1, which is higher than the Cu stabilizer hardness in a reference Nb3Sn cable ten-stack that was subjected to a 210 MPa transverse compression. We also show that once the collaring procedure issue was rectified in a subsequent dipole, the Nb3Sn filaments were found to be undamaged, and the Cu stabilizer hardness values were reduced to the expected levels. This paper provides a post-mortem verification pathway to analyze the damage, provides strand level mechanical properties, which could be beneficial for improving model prediction capabilities. This method could be applied beyond Nb3Sn magnets to composite designs involving high work hardening materials.

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Superconductor Science and Technology
PAPER • OPEN ACCESS
Metallographic analysis of 11 T dipole coils for High Luminosity-Large
Hadron Collider (HL-LHC)
To cite this article: Shreyas Balachandran et al 2021 Supercond. Sci. Technol. 34 025001
View the article online for updates and enhancements.
This content was downloaded from IP address 194.12.169.3 on 22/02/2021 at 10:28

Superconductor Science and Technology
Supercond. Sci. Technol. 34 (2021) 025001 (9pp) https://doi.org/10.1088/1361-6668/abc56a
Metallographic analysis of 11 T dipole
coils for High Luminosity-Large Hadron
Collider (HL-LHC)
Shreyas Balachandran
1
, Jonathan Cooper
1,2
, Orion B Van Oss
3
, Peter J Lee
1
,
Luca Bottura
4
, Arnaud Devred
4
, Frederic Savary
4
, Christian Scheuerlein
4
and Felix Wolf
4
1
Applied Superconductivity Centre, NHMFL, FSU, Tallahassee, FL 32310, United States of America
2
Department of Mechanical Engineering, College of Engineering, FAMU-FSU, Tallahassee, FL 32310,
United States of America
3
Department of Physics, Columbia University, New York, NY 100027, United States of America
4
European Organization for Nuclear Research (CERN), CH-1211 Geneva, Switzerland
E-mail: shreyasb@asc.magnet.fsu.edu and christian.scheuerlein@cern.ch
Received 4 September 2020, revised 9 October 2020
Accepted for publication 28 October 2020
Published 8 January 2021
Abstract
For next-generation accelerator magnets for elds beyond those achievable using Nb–Ti, Nb
3
Sn
is the most viable superconductor. The high luminosity upgrade for the Large Hadron Collider
(HL-LHC) marks an important milestone as it will be the rst project where Nb
3
Sn magnets
will be installed in an accelerator. Nb
3
Sn is a brittle intermetallic, so magnet coils are typically
wound from composite strands containing ductile precursors before heat treating the wire
components to form Nb
3
Sn. However, some mechanical assembly is still required after the coils
have been heat-treated. In this paper, we present direct evidence of cracking of the brittle Nb
3
Sn
laments in a prototype dipole that resulted in degraded magnet performance. The cracking of
the Nb
3
Sn, in this case, can be attributed to an issue with the collaring process that is required in
the assembly of dipole accelerator magnets. Metallographic procedures were developed to
visualize cracks present in the cables, along with quantitative image analysis for location-based
crack analysis. We show that the stresses experienced in the damaged coil are above the critical
damage stress of Nb
3
Sn conductor, as evidenced by a measured Cu stabilizer hardness of 85
HV
0.1
, which is higher than the Cu stabilizer hardness in a reference Nb
3
Sn cable ten-stack that
was subjected to a 210 MPa transverse compression. We also show that once the collaring
procedure issue was rectied in a subsequent dipole, the Nb
3
Sn laments were found to be
undamaged, and the Cu stabilizer hardness values were reduced to the expected levels. This
paper provides a post-mortem verication pathway to analyze the damage, provides strand level
mechanical properties, which could be benecial for improving model prediction capabilities.
This method could be applied beyond Nb
3
Sn magnets to composite designs involving high work
hardening materials.
Keywords: Nb
3
Sn, HL-LHC, dipole magnets, damage analysis
(Some gures may appear in colour only in the online journal)
1. Introduction
Nb
3
Sn is the most viable conductor for high eld acceler-
ator magnets in the range of 10–16 T for High Energy Phys-
ics research [1]. Beyond the Large Hadron Collider (LHC)
the next generation Future Circular Collider (FCC), a 100
TeV hadron-hadron collider, is expected to use both Nb
3
Sn
dipoles and quadrupoles operating at 16 T, 4.2 K [2]. Chal-
lenges involved in the construction of 16 T Nb
3
Sn magnets
include the development of production quality conductors that
1361-6668/21/025001+9$33.00 1
© 2021 The Authors. Published by IOP
Publishing Ltd Printed in the UK
This is an open access article distributed under the terms of the Creative Commons Attribution 4.0 License.
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Supercond. Sci. Technol. 34 (2021) 025001 S Balachandran et al
can carry a demanding current density, J
c
, of 1500 A mm
2
(16 T, 4.2 K) and magnet designs incorporating stress manage-
ment to control the high stresses experienced by Nb
3
Sn con-
ductors during magnet construction and under the inuence of
Lorentz forces during operation. Recently achieved increases
in the upper limits of J
c
in Nb
3
Sn strand indicate that suf-
ciently high J
c
to meet FCC requirements is now possible
[3, 4]. Furthermore, an experimental prototype Nb
3
Sn dipole
magnet has recently generated the signicant milestone eld
of 14 T. Further design testing is now underway for a 15 T tar-
get eld, where conductor degradation in high-stress regions
is a major concern [5].
A crucial step in the development of high eld Nb
3
Sn
magnets is the major upgrade of the LHC, called High
Luminosity LHC (HL-LHC). Tens of Nb–Ti magnets will be
replaced with Nb
3
Sn dipole and quadrupole magnets using
state-of-the-art Nb
3
Sn conductor. The 11 T dipole magnets
[6] are the rst Nb
3
Sn magnets that will be installed in a
particle accelerator. They will provide the same integrated
field as the standard 8.3 T LHC dipoles over a shorter length,
which allows the installation of additional collimators in the
LHC arcs.
Stress management is a critical issue in Nb
3
Sn magnets
due to the brittle Nb
3
Sn phase. Although the conductors are
wound and then reacted to minimize mechanical stresses on
the Nb
3
Sn laments, there remain several avenues leading to
conductor damage. Improper assembly may result in over-
stressing and coil damage, thermal expansion mismatch of
the coil, and magnet constituents can cause damage during
thermal cycling, Lorentz forces generated during powering
may overstrain the Nb
3
Sn. FE simulations can provide use-
ful but approximate predictions of the stress distribution in the
magnet during the different assembly and operational condi-
tions; however, the prediction of precise stress levels remains
a challenge.
During cold testing of an 11 T dipole short model mag-
net at CERN, a critical current limitation of the coils was
detected. It was suspected that the reason for this degrada-
tion was fracturing of some of the Nb
3
Sn laments as a res-
ult of excessive mechanical stress during the collaring of the
coils. A post-mortem (destructive post magnet testing) metal-
lographic analysis technique has been developed in order to
provide more in-depth insight, at the conductor level, into the
degradation and complexity in stress states. This approach was
previously demonstrated in Nb
3
Sn cable-in-conduit magnet
sections tested for the ITER project [79].
This paper provides a roadmap for different aspects related
to damage and microstructure in Nb
3
Sn model dipole coils. A
comparison between multi-axial loaded dipole sections versus
uniaxially loaded cable ten-stack sample sections indicate
variations in the damage behavior. A technique to resolve the
effects of stresses on the lament level using Cu microhard-
ness measurements s presented in this paper. This technique
could be applied to future model magnets and also provide
granular data to provide realistic stress values for the devel-
opment of stress prediction models for complicated magnet
assemblies.
2. Experimental methods
For the current study, we have analyzed two 11 T dipole coil
cross sections, which were rough-cut using a band saw after
disassembling the magnets after cold testing and then preci-
sion cut with a diamond wire saw. The coil cross-section and
the coil collaring procedure are discussed in detail in [10].
11 T dipole cable ten-stack samples [11] were also evaluated.
Figures 1(a)–(e), provides a visualization of the dipole section
at various stages of disassembly. An 11 T dipole collared aper-
ture containing two coils is shown in gure 1(a). Figure 1(b)
shows a photograph of the short model coil #109 after magnet
cold test and disassembly. The dipole design used in the 11 T
dipole magnet is indicated in the top view of the solid model
in gure 1(c). The sectional view (Section AA) in gure 1(d)
shows the various components that make up the dipole seg-
ment, including (a) Nb
3
Sn cables, (b) austenitic stainless steel
316L loading plate which presses against the loading pole,
(c) oxide dispersed Cu (DISCUP 30
®
) wedges. The insulat-
ing layers and epoxy impregnation that is present in the dipole
cross-section are not indicated in the gure here. The 11 T
dipole Nb
3
Sn coils are segmented into six different conductor
blocks, as numbered in gure 1(d). To evaluate metallographic
details of cross-sections, different dipole coil sections were cut
as shown in gure 1(e). The orientation of the samples pol-
ished from the dipole section corresponded to the plane con-
taining the axial and transverse directions. The nomenclature
of the sections consists of the conductor block number follow-
ing the word section, and the corresponding row cut from the
section. As indicated in gure 1(e). Section 1-R1, shows the
section from coil block #1, the rst row cut from coil block #1
indicated by R1. The two-layer Nb
3
Sn segments in the cross-
sections are indicated as Row 1–9, with each row consisting
of two Nb
3
Sn conductor segments.
2.1. Details of 11 T dipole coils for this study
For this metallographic study, two coils were selected for ana-
lysis, short model coil #109, which showed severe critical cur-
rent degradation, and 11 T dipole series coil GE-C02 that did
not show current degradation.
After collaring coil #109 was assembled in 11 T twin aper-
ture dipole MBHDP102, as shown in gure 1(a). Cold tests
of MBHDP102 revealed a substantial critical current limita-
tion at the mid-plane turns of coil #109, and the n-value was
also strongly suppressed [10, 12], both indications of pos-
sible Nb
3
Sn lament breakage. The critical current limitation
probably caused the relatively low quench currents of magnet
MBHDP102.
The critical current deterioration, which was detected over
an extended length in the straight part of the coil, was pre-
sumed due to excessive mechanical stresses applied during
the collaring of the coil [10]. Section AA in gure 1(c) is
a coil cross-section in which lament damage is expected.
Coil #109 was de-collared and central section cuts were made
for metallographic examination. A central section is shown in
gure 1(d) was diamond wire saw cut and analyzed further.
2

Supercond. Sci. Technol. 34 (2021) 025001 S Balachandran et al
Figure 1. Segments of the 11 T dipole coil at various stages of disassembly, (a) cross section of collared 11 T dipole coil assembly made of
two coils, (b) 11 T dipole short model coil #109, (c) top view of a 11 T dipole coil, (d) cross-sectional view of section AA, including the cut
dipole segment of Coil #109 used in this study, (e) isometric view of the dipole section to visualize the coil segments analyzed by
metallography.
The second coil investigated here (GE-C02) was the second
series 11 T dipole coil collared in the 11 T dipole aperture
HCMBH_C001-01000001. There was a difference between
manufacturing procedures used in GE-C02 versus coil #109.
The series coil GE-C02 has an optimized insulation scheme,
and the collaring procedure was improved to reduce the mech-
anical stress on the Nb
3
Sn conductor during collaring. Finite
element simulations of the stress distribution in the coil dur-
ing the Collaring procedure indicate that the highest stresses
are experienced at the coil midplane on the Nb
3
Sn cables in
section 1-R1 [13].
The aperture, including coil GE-C02, was cold tested in
a ‘hybrid’ magnet assembly where the second aperture was
not powered. Powering tests after the rst magnet cool down
showed excellent quench performance, and in particular, no
critical current degradation at the coil mid-plane was observed.
However, after an additional thermal cycle, the coil perform-
ance was degraded, due to a critical current (I
c
) limitation at the
coil ends (making the magnet available for destructive post-
mortem analysis). The degradation at the coil ends was pre-
sumably caused by warming the magnet too fast. For metal-
lographic examination, the coil samples were extracted in the
central- straight part of GE-C02 (similar to the coil section in
#109). In the central section of GE-C02, no lament damage
is expected [10].
2.2. Description of 11 T dipole cable ten-stack samples
The ten-stack samples are made of ten 11 T dipole cables
(nominal width and mid-thickness are 14.7 mm and 1.25 mm,
3

Supercond. Sci. Technol. 34 (2021) 025001 S Balachandran et al
Figure 2. Ten-stack Nb
3
Sn coils in three different states: (a)
#28-compression loaded to 210 MPa (change to 210 MPa in the
gure) along the direction transverse to the Nb
3
Sn wire
cross-section, (b) #33-compression loaded to 210 MPa along the
axis of the superconductor wire, and c) is an unloaded ten-stack.
respectively [14]), which are stacked alternatingly in order to
compensate for the keystone angle of 0.79
. The Rutherford
cables are made of 40 Restacked-Rod Process type Nb
3
Sn
strands with 0.7 mm nominal diameter, which were pro-
duced by Oxford Instruments Superconducting Technology
(now Bruker-OST). The Rutherford cables have a 25 µm thick
stainless steel core, and they are surrounded by a 0.15 mm
thick cable insulation made of mica tape and S2/E-glass fiber.
The Nb
3
Sn formation heat treatment was performed with a
ramp rate of 50
C h
1
and was comprised of three iso-
thermal plateaus of 210
C-48 h, 400
C-48 h and 665
C-
75 h. The ten-stack samples are designed to be comparable
to dipole cable sections; the wire volume in the ten-stack
samples that were analyzed is 72%. The Cu in this sample
is assumed to be fully annealed after the prior heat treatment
to a peak temperature of 665
C. More information about the
ten-stack sample production and mechanical loading has been
published in [15].
Ten-stack samples No 28 and No 33 (gure 2) were uni-
axially loaded to compressive peak stress of 210 MPa. Ten-
stack #28 was loaded in the transverse direction (corresponds
to gure 1(e)), and No. 33 was loaded in the axial direc-
tion. Unloaded sample #57 was used as a reference in this
study.
Composite theory predicts iso-strain in the composite con-
stituents under axial loading [16]. This has been conrmed
experimentally for the Nb
3
Sn laments and Cu matrix in dif-
ferent Nb
3
Sn wires by high energy synchrotron x-ray dif-
fraction [16], and in ten-stack samples by neutron diffraction
[8]. At 210 MPa (sample 28), the macroscopic axial ten-stack
stresses in the Nb
3
Sn and Cu are about 450 MPa and 100 MPa,
respectively [17].
Transverse loading theory predicts iso-stress [18] in the
composite constituent materials [19]. Neutron diffraction
measurements conrm that under transverse macroscopic ten-
stack stress of 210 MPa (sample 33), the stress in the Nb
3
Sn
laments and in the Cu matrix is very similar and correspond
to the externally applied stress of 210 MPa [11].
2.3. Metallography
For metallographic evaluation, the samples were mounted in
a clear epoxy-hardener mixture, which was cured at room
temperature (RT). Subsequent sectioning was performed using
a wafering saw with the sample glued to a base plate to
avoid the danger of damage that might be caused by clamping
the sample directly. The samples were mechanically polished
using SiC pads with a decreasing grit size of 320, 400, 600,
800, and 1200. The load on the sample during the grinding
process was 12 N, and the cross-sectional area of the mount
was ~500 mm
2
. After the grinding process, the samples were
polished using diamond slurries of successively decreasing
particle size (5 µm, 3 µm, 1 µm). The nal polishing step
used a 50 nm colloidal silica solution with a pH ~ 11 in a
Vibromet
®
vibratory polisher. This polishing procedure is a
standard metallographic sample preparation technique; how-
ever, the low loads are essential here to maintain the integ-
rity of the sample. The samples were lightly etched in a 1:1:
HF:H
2
O solution for 10 min to make the cracks more visible
by light microscopy. In order to remove staining from the etch,
the samples were returned to the vibratory polisher for 30–
45 min, after which the samples were cleaned and dried for
further imaging.
Imaging of the cracks was performed using an Olympus
BX41M reected light microscope combined with an Olym-
pus UC50 digital camera and Olympus Stream capture soft-
ware. Backscattered Electron (BSE) images were obtained
using a Zeiss ESB- FESEM. Analysis of shape and crack dens-
ity was performed using FIJI-ImageJ [20, 21], combined with
custom routines for superconductor analysis [8].
Vickers microhardness tests were performed on the pol-
ished cross-sections of the dipole and ten-stack samples using
a LECO 300 AT hardness tester. The load dependence on the
hardness was veried over the complete range of 10 g–1 kg on
the unloaded ten-stack samples. For hardness comparisons, a
100 g load with a dwell time of 15 s was used in this study.
The hardness measurements are designated HV
0.1
XX, where
HV signies Hardness Vickers (scale), and the subscript 0.1,
means the applied load in kg, and XX is the hardness number
derived from the diagonal indent measurements.
Metallography and hardness measurements in this paper
focus on section 1-R1 in dipole coils #109, and GE-C02, where
the stresses on the Nb
3
Sn cables are predicted to be maximum
from available simulation results [13]. A complete descrip-
tion of the metallographic process development and compar-
isons between different coil sections are underway and will be
presented elsewhere.
3. Results
3.1. Nb
3
Sn crack distribution in coil #109
Section 1-R1 of Coil #109 was mounted, polished, etched, and
imaged. Cracks were observed in this section with varying
densities based on location. Crack morphologies vary in the
lament, as shown in gure 3. The commonly found cracks are
4

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Frequently Asked Questions (1)
Q1. What contributions have the authors mentioned in the paper "Metallographic analysis of 11 t dipole coils for high luminosity-large hadron collider (hl-lhc)" ?

The high luminosity upgrade for the Large Hadron Collider ( HL-LHC ) marks an important milestone as it will be the first project where Nb3Sn magnets will be installed in an accelerator. In this paper, the authors present direct evidence of cracking of the brittle Nb3Sn filaments in a prototype dipole that resulted in degraded magnet performance. The authors show that the stresses experienced in the damaged coil are above the critical damage stress of Nb3Sn conductor, as evidenced by a measured Cu stabilizer hardness of 85 HV0. The authors also show that once the collaring procedure issue was rectified in a subsequent dipole, the Nb3Sn filaments were found to be undamaged, and the Cu stabilizer hardness values were reduced to the expected levels. This paper provides a post-mortem verification pathway to analyze the damage, provides strand level mechanical properties, which could be beneficial for improving model prediction capabilities. This method could be applied beyond Nb3Sn magnets to composite designs involving high work hardening materials.