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Plank #7 and beyond
2
What was new for plank#7?
• Carbon-fibre jig• Oversize (by 10mm) facesheets during stave core build
– Facesheets now at the very limit of curved co-cure jig → will move to halfpipe (like LBNL)
– No contamination of jig surface (as expected)– Facesheets are milled to size after stave core build – worked ok, but
want to investigate more gentle methods• First full-size core with 45gsm prepreg made in UK
– Both facesheets developed crinkles during co-cure (CF & tape together) • Is this because jig too small?• Or because of UK tape?
• Glue applied to pipe instead of foam blocks– This brought the amount of glue used for this step from >20g to <4g– No glue between upper and lower foam blocks
• Thermally probably ok (as long as there is no other fault, but what’s the impact on shear rigidity?)
• Glue mixer
Pictures
3
Side A (bottom)
Side B (top)
Pipe glue applicator
4
Weights
• Total weight of stave core: 308.64g (plank#6: 444.37g)• Weight reduction per facesheet: ~50g
– 100gsm → 45gsm expect ~25g– Rest due to different tape build-up (Altaflex vs UK)?
• Glue has been reduced from 75g to 26g
Face sheet 1 (estimated)
Face sheet 2
Lower foam blocks (estimated)
Close outs
Upper foam blocks (incl bend)
cooling pipe (with plugs)
C-channels
honeycomb sections
Glue estimated
0
50
100
150
200
250
300
Face
shee
ts
Foam
C-cha
nnel
s & cl
ose-
outs
Coolin
g pip
e
Honey
com
bGlu
e
we
igh
t [g
]
Stave #6
Stave #7
5
FlatnessPlank #7 Side A
0
20
40
60
80
100
120
140
160
0 200 400 600 800 1000 1200
Plank #7 - side B
0
20
40
60
80
100
120
140
160
180
0 200 400 600 800 1000 1200
-0.2
-0.15
-0.1
-0.05
0
0.05
0.1
0.15
0.2
0 200 400 600 800 1000 1200
position [mm]
dis
pla
cem
ent
[mm
]
side A
side B
-0.1
-0.05
0
0.05
0.1
0.15
0.2
0.25
0.3
0 50 100 150 200
transverse position [mm]
dis
pla
cem
ent
sid
e A
[m
m]
-0.3
-0.25
-0.2
-0.15
-0.1
-0.05
0
0.05
0.1
dis
pla
cem
ent
sid
e B
[m
m]
Side A
Side B
After removal of z-dependence
Stiffness• Plank with similar build-up (45gsm K13C2U/EX1515) is US
stave– Compared to that plank#7 has 20% higher bending stiffness (without
taking sandwich thickness into account)– Shear rigidity was not measurable for US stave, for plank#7 lower
than other planks we built, but not clear how biased by bending stiffness
6
16.13
29.41
24.66
12.85
64.03
33.10
10.79
102.63 102.83 101.4892.38 101.39
51.83
133.42
61.59
0
20
40
60
80
100
120
140
160
0
20
40
60
80
100
120b
end
ing
sti
ffn
ess
[Nm
2 ]
shea
r ri
gid
ity
[kN
]
beam shear rigidity
beam bending stiffness
Plank Material CommentWeight
plank [g]Weightglue [g]
1 80gsm K13D2U/RS-3 Multiple delaminations 420.0 53.5 (12.7%)
2 80gsm K13D2U/RS-3 Thermo-mechanical 444.1 91.6 (20.6%)
3 80gsm K13D2U/RS-3 No tapes 317.2
4 80gsm K13D2U/RS-3 Foam core 449.6
5 80gsm K13D2U/RS-3 Corrugated core 444.7
US 45gsm K13C2U/EX1515 Tube close-outs 390.5 32.4 (8.3%)
6 100gsm K13C2U/EX1515 444.4 75.4 (17.0%)
7 45gsm K13C2U/EX1515 308.6 26.4 (8.6%)
What should we do next?
• Thin stave: to get a feeling for integrity and stiffness of such a stave– 2mm cooling pipe (material uncritical)
– Need special close-outs
– Special inserts for C-channel jig (but main part can be used without modification)
• And/or stave with multiple broken cooling pipe: To address concerns about internal weld joints– Cooling pipe diameter and material TBD (I naively assume the most
critical would be larger diameter and Ti)
– The rest of the stave would be as usual, but we could do another corrugated core (low mass)
– This should then go into the QMUL thermal chamber
• And/or…?
• And what should we do with plank#7 (and plank#6)?7