Composites- Mechanics and Processing Considerations Flashcards

1
Q

Tensile moduli directions

A

1 is parallel to uniaxial fibres. 2 is perpendicular to fibres but in plane of lamina. 3 is vertically out of lamina (don’t normally consider)

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2
Q

Rule of mixtures for tensile modulus in 1 and 2 directions

A

E1=ffEf+(1-ff)Em
E2=EfEm/((1-ff)Em+ffEm)
Where f subscript f is fibre volume fraction
Ef is the fibre modulus
Em is matrix modulus
E2 equation isn’t accurate so often use Halpin-Tsai equation

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3
Q

When do fibre and matrix work in series of parallel?

A

In the 1 direction (along fibre length) they work in parallel.
In the 2 direction (perpendicular in plane) they work in series and the matrix is the weakest (most compliant) link

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4
Q

Why are unidirectional composites anisotropic?

A

It is stiffer axially as the fibres and matrix work in parallel and more compliant in transverse as they work in series. Small contribution is whether the fibres themselves are anisotropic (but glass isn’t)

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5
Q

Major poisson’s ratio formula

A

ν12=ffνf+(1-ff)νm
f and m mean fibre and matrix
This is for force applied in axial direction (length of fibres)

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6
Q

How are major and minor poisson’s ratio linked?

A

ν12/E1=ν21/E2

21 means stress in transverse direction

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7
Q

In which direction do composites contract more in?

A

More in the transverse direction when loaded axially because this direction is matrix (more compliant) dominated. Axial direction is stiffer as is fibre dominated. Therefore ν12 is greater

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8
Q

In-plane shear modulus formula

A

G12=GfGm/((1-ff)Gf+ffGm)

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9
Q

What is needed for successful manufacture of parts from fibre reinforced composites?

A

Fibres and matrix must be maintained at the correct shape, temperature, pressure. The conditions must be maintained throughout the process and the full part

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10
Q

Processing considerations for the reinforcement

A

Type (fibres, particulates). Continuous or discontinuous. Random or oriented. Sizing, coupling agent, surface treatment. Fibre volume fraction. Safety (nanomaterials in lungs).

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11
Q

Processing considerations for the matrix

A

Thermoset or thermoplastic. Temperature tolerance (shrinkage). Environmental tolerance (moisture). Compatibility with reinforcement. Additives, fillers. Void fraction (vacuum/gas won’t support load). Reaction chemistry- cure schedule (T, P, t), degree of cure, post-curing. Viscosity gelatinous time (pot life). Safety

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12
Q

Processing considerations for the component

A

Size, thickness, cross-section, curvature. Surface finish. Dimensional tolerance. Holes, fixings, strong points, inserts

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13
Q

Processing considerations for the cost

A

Equipment. Moulds. Materials. Labour. Energy

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14
Q

Processing considerations for the process type

A

Automation, rate. Machining, trimming, static electricity. Heat transfer- curing T (can overheat/overture and burn part), exothermic reaction (excess heat output). Mould fabrication. Reinforcement draping (getting fibres to follow shape of mould, e.g around corners)

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