Composites in the growing field of carbon nanotubes and other carbon nano-forms

Содержание

Слайд 2

Initial studies in carbon nanotubes and nanoclay modified composites Cytec Engineering

Initial studies in carbon nanotubes and nanoclay modified composites

Cytec Engineering Materials.

CYCOM 977-20, 177˚C curing epoxy resin with 126-138˚C dry and 104˚C wet service capability, used in Dreamliner Boeing 787.

Achieved mechanical properties did not differ from the original system which was seen as the advantageous aspect compared to graphene particles which reduce the property of epoxy modified systems by a significant percentage with each added layer, levelling at 30% loss in mechanical properties, However, the increased electrical conductivity of CFRP modified with 1% CNT was tenfold.

Vahid Nekouie, The University of Sheffield

Слайд 3

Composites At Sheffield. Inkjet printing of PMMA in CFRP laminates as

Composites
At
Sheffield.

Inkjet printing of PMMA in CFRP laminates as the

alternative to toughening improvement

© 2015 The University Of Sheffield

Funded by AFOSR 2011-2014, and US Army & AFOSR in 2015

Слайд 4

Shear Modulus & ILSS Fibre-reinforced plastic composites — Determination of apparent

Shear Modulus & ILSS

Fibre-reinforced plastic composites — Determination of apparent interlaminar

shear strength by short-beam method. (BS EN ISO 14130:1998)

Yi Zhang and Richard Grainger, The University of Sheffield

Слайд 5

www.sheffieldcomposites.co.uk Composites At Sheffield ILSS ILSS: Maximum interlaminar shear stress (τM)

www.sheffieldcomposites.co.uk

Composites
At
Sheffield

ILSS

ILSS: Maximum interlaminar shear stress (τM)
No damage introduced, investigation

of undamaged parameters and postcuring effect of potential un-crosslinked group

Note: error bar represents standard deviation, n = 5

Heating cycle: 177℃ for 2 hours, (harshest conditions)
Purpose: to investigate any potential reduction of the ILSS, due to the presence of printed surface. ILLS values of all groups are enhanced after heat treatment, which indicated the existence of post curing.

© 2015 The University Of Sheffield

Yi Zhang and Richard Grainger, The University of Sheffield

Слайд 6

www.sheffieldcomposites.co.uk Composites At Sheffield. Stiffness © 2015 The University Of Sheffield

www.sheffieldcomposites.co.uk

Composites
At
Sheffield.

Stiffness

© 2015 The University Of Sheffield

Heating cycle: 177℃ for

2 hours, (harshest conditions)
Purpose: to investigate effect of printed additions on the material’s stiffness.
The effect achieved successfully. The printed surface noticeably increased the stiffness of the material both before and after heat treatment compared to virgin group.

Note: error bar represents standard deviation, n = 5

Yi Zhang and Richard Grainger, The University of Sheffield

Слайд 7

www.sheffieldcomposites.co.uk Composites At Sheffield. X-ray tomography © 2013 The University Of Sheffield

www.sheffieldcomposites.co.uk

Composites
At
Sheffield.

X-ray tomography

© 2013 The University Of Sheffield

Слайд 8

Composites At Sheffield. Printed surface ratio & volume fraction Volume fraction:

Composites
At
Sheffield.

Printed surface ratio & volume fraction

Volume fraction: ~ 0.025vol.%
Weight

increased: ~ 0.020wt.%
(Negligible, within the manufacturing error margin)

Printed surface ratio between the plies:
30 ~ 40%

© 2015 The University Of Sheffield

Слайд 9

Composites At Sheffield. Printed PMMA droplets on epoxy coated glass substrate

Composites
At
Sheffield.

Printed PMMA droplets on epoxy coated glass substrate

© 2015

The University Of Sheffield

Optical images of epoxy coated glass substrates with printed PMMA droplets:
5, 10 and 20% PMMA deposits before and after the heating cycle.

Yi Zhang and Jonathan Stringer, The University of Sheffield

Слайд 10

Composites At Sheffield. PMMA film between CFRP plies before and after

Composites
At
Sheffield.

PMMA film between CFRP plies before and after heating

©

2015 The University Of Sheffield

PMMA film is comparable to inkjet printed area that is double the percentage of concentration of the film pattern. 10% film pattern is comparable to 20% PMMA droplets due to the volume fraction of PMMA in those two systems.

Yi Zhang and Jonathan Stringer, The University of Sheffield

Слайд 11

© 2015 The University Of Sheffield Composites At Sheffield. Evidence of

© 2015 The University Of Sheffield

Composites
At
Sheffield.

Evidence of selective printing

on GIc of CRFP laminates

GIc values of printed areas are comparatively higher than unprinted areas, which means inkjet printing can be applied to delicate material design work, and manufacture property graded multifunctional materials.

A

B

Crack propagation way

Yi Zhang, Patrick Smith and Jonathan Stringer, The University of Sheffield

Слайд 12

Composites At Sheffield. PMMA contribution to CFRP properties © 2015 The

Composites
At
Sheffield.

PMMA contribution to CFRP properties

© 2015 The University Of

Sheffield

PMMA droplets act as plastic zones that can absorb energy by plastic deformation. Due to the viscoelastic nature of PMMA, those well dispersed microphases by inkjet printing provide an energy-absorption path by thermoplastic deformation, which can decelerate crack growth as the crack tips are shielded by those plastic zones.
Crack propagation is arrested by the combination of crack-diverting discretely deposited droplets and the higher fracture toughness of PMMA. The second option can be further evidenced by the lower standard deviation in the system with hexagonally printed 20% PMMA system.

Слайд 13

Composites At Sheffield. Influence of the machining parameters in CFRP laminates

Composites
At
Sheffield.

Influence of the machining parameters in CFRP laminates I


© 2015 The University Of Sheffield

Indented areas on (a) the non-aged specimen and the specimens aged at (b) 200 C and (c) 350 C, in MTM44-1 CF0300. MTM44-1 resin is a toughened phenol–formaldehyde (PF)-based aerospace grade resin, CF0300 is a 2/2-twill carbon fabric, (HS) carbon fibre reinforcement.

Julian Marino-Perez, The University of Sheffield

Слайд 14

Composites At Sheffield. Influence of the machining parameters in CFRP laminates

Composites
At
Sheffield.

Influence of the machining parameters in CFRP laminates II


© 2015 The University Of Sheffield

Julian Marino-Perez, The University of Sheffield

Maximum temperatures developed in the drilling of selected CFRP systems:
(a) MTM44-1 CF0300, (b) MTM44-1 CF2216 and (c) MTM28B CF0300 at different distances away from the hole edge, measured using thermocouples and thermal imaging (IR camera).

Слайд 15

Composites At Sheffield. Damage to CFRP laminates due to machining ©

Composites
At
Sheffield.

Damage to CFRP laminates due to machining

© 2015 The

University Of Sheffield

Julian Marino-Perez, The University of Sheffield

Left to right: SEM images at the hole exit corresponding to 49.8 m/min, 99.6 m/min, 149.4 m/min and 199.2 m/min cutting speeds. Above: fibres at 90° (perpendicular to the machining direction), below: fibres at 0° and 90°.