FrançoisXavier Nuiry Wolfgang Klempt Fernando Duarte Ramos Miguel Angel Villarejo 1 Stave studies 2 Reception of 3 new staves from Composite Design Stave 1 layup T800 skin 3 plies 0 90 0 0095mm thick ID: 797501
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Slide1
Stave studies
11/18/2013François-Xavier NuiryWolfgang KlemptFernando Duarte RamosMiguel Angel Villarejo
1
Slide2Stave studies2
Reception of 3 new staves from Composite Design:
Stave 1 layup:
-T800 skin, 3 plies [0°, 90°, 0°] (~0.095mm thick)
-
Rohacell
core 51kg/m
3
(Machined)
-T800 skin, 3 plies [0°, 90°, 0°] (~0.095mm thick)Thickness: ~1.77mm Length: ~280.2mm Width: ~25.85mm Mass: 3.173gStave 2 layup: -T800 skin, 3 plies [0°, 90°, 0°] (~0.095mm thick) -Nida Nomex C2 3.2 29, density 29kg/m3 -T800 skin, 3 plies [0°, 90°, 0°] (~0.095mm thick)Thickness: ~1.68mm Length: ~280.2mm Width: ~ 25.9mm Mass: 3.448gStave 3 (same as stave 2):Thickness: ~ 1.71mm Length: ~280.2mm Width: ~26mm Mass: 3.505g
Slide3AddendumStave studies3
Composite design staves
Material properties
Glue: DP490 (3M)
150g/m
2
2.18g / stave!
Should be 3.5-0.32-1.31=
1.87g
Rohacell
core 51kg/m3Masse in one stave~ 0.56gE=70 MPaNida Nomex C2 3.2 29, density 29kg/m3Masse in one stave: ~ 0.32gMP,EX,2,0.0001mp,ey,2,0.0001mp,ez,2,48.26mp,gxy,2,0.00001mp,gyz,2,11mp,gxz,2,15mp,prxy,2,0.5mp,pryz,2,0mp,prxz,2,0 mp,dens,2,0.029E-6T800 skin, 3 plies [0°, 90°, 0°] (~0.095mm thick)Mass for 2 skins ~ (30g/m
2) 1.31gmp,ex,1,161000
mp,ey,1,8600mp,ez,1,8600mp,gxy,1,4870mp,gyz,1,4870mp,gxz,1,4870
mp,prxy,1,0.286
mp,pryz,1,0.3
mp,prxz,1,0.286
!mp,alpx,1,-7.65E-007
!mp,alpy,1,15E-006
!mp,alpz,1,15E-006
mp,dens,1,1.570E-6
Source: ESACOMP
Coming from ESACOMP
Coming from
Composite design
Coming from
rohacell
datasheet
Loading case for transverse shear modulus calculation:
Gxy
Gyz
Glue: DP490 (3M)
150g/m
2
2.18g / stave!
Should be 3.173-0.56-1.31=
1.3g
AddendumStave studies4
Composite design staves
Mass
Stave 1
Stave 2
Stave 3
Skin
T800
1.31g
T800
1.31g
T8001.31gCoreRohacell0.56gNida0.32gNida0.32gGlue1.3g1.87g1.87gTotal mass3.17g3.5g3.5g
Slide55
Composite Design Staves: Full sandwichCalculation of the bending stiffness E*I
Two options:
2- E*I calculated from the beam bow formula
1- E*I calculated from the beam theory
Can be approximated:
t
d
h
t
t
b
L
W
F
6
Composite Design Staves: Full sandwichANSYS Calculation of the flexural stiffness
Composite design staves
1
2
3
Geometry
Full sandwich
Full sandwich
Full sandwich
Full sandwich
Full sandwich
Full sandwich
Full sandwich
Full sandwich
Skin Mat
T800 (TPT)
T800 (TPT)
T800 (TPT)
T800 (TPT)
T800 (TPT)
T800 (TPT)
T800 (TPT)
T800 (TPT)
Core Mat
Rohacell
Rohacell
Rohacell
Rohacell
Nida nomex
Nida nomex
Nida nomex
Nida nomex
Span (mm)
180
260
180
260
180
260
180
260
Displacement (mm)
0.6
0.6
0.6
0.6
0.6
0.6
0.6
0.6
Core E modulus Mpa
70
70
20
20
48.26
48.26
48.26
48.26
Core G modulus Mpa
26.92
26.92
7.69
7.69
15.00
15.00
15.00
15.00
Reaction force in the center (N)
1.619
0.5666
1.2904
0.50132
1.3545
0.48997
1.407
0.509
Flexural stiffness (N/mm)
2.70
0.94
2.15
0.84
2.26
0.82
2.35
0.85
Bending stiffness (EI)
N.mm^2 (Bow formula)
3.66E+05
3.65E+05
3.68E+05
3.65E+05
3.22E+05
3.24E+05
3.36E+05
3.38E+05
Bending
stiffness (EI)
N.mm^2 (beam theory)
3.52E+05
3.52E+05
3.52E+05
3.52E+05
3.16E+05
3.16E+05
3.30E+05
3.30E+05
MEASURMENTS
Flexural stiffness N/mm
2.12
0.781
2.12
0.781
2.17
0.776
2.24
0.79
Bending stiffness (EI) N.mm^2
3.61E+05
3.37E+05
3.13E+05
3.09E+05
3.24E+05
3.15E+05
Slide77
StavesComparison of the measured flexural stiffness
Stave
Skin
Core
Span (mm)
Flexural stiffness (N/mm)
Masse, g (280mm long stave)
Bending stiffness
N.mm
2
Natural frequency estimate (Hz)(280mm long stave clamped on both sides)PH/DT cross bracing prototypeStave 8M55JRohacell180 mm1.78 N/mm1.48 g2.39 * 105138 HzPH/DT sandwich prototypeM55JRohacell180 mm6.95 N/mm3.74 g16.3 * 105314 HzCD Stave 1T800
Rohacell180 mm
2.12 N/mm3.173 g
3.61 * 10
5
152 Hz
CD Stave 2
T800
Nida
Nomex
180 mm
2.17 N/mm
3.448 g
3.13 * 10
5
140 Hz
CD Stave 3
T800
Nida
Nomex
180 mm
2.24 N/mm
3.505 g
3.24 * 10
5
142 Hz
Slide8Short – Mid term strategyDiscussions with Composit Design
8
Staves manufacturing process:
Nida
Staves
Glue application on skins (150g/m2)
Impregnation of the
nida
on the skin
Re-application of glue (150g/m2) on skinsRealisation of the sandwichCure at room temperature under 0.2BarAlternatives:-Impregnation of nida on a table and impregnation of the skin and then gluing (better control of the glue quantity)-Glue sheets 150g/m2 (~ 110 micron) thick with micro holes (cure at 120C)-CD could also tests other glue films (e.g: Staystick…)-Direct polymerisation of the prepreg on the nida (not so good for Alum nida, but OK for Nomex). Here a specific glue is necessary.What is not possible:Just an impregnation of the nida and direct gluing on skins. It would not stick according to them.For space applications, skins are always polymerised before realising the sandwich.
Rohacell StaveGlue application
on skins (150g/m2)Realisation of the sandwich
Cure at room temperature under 0.2Bar