4: Preforming Flashcards

1
Q

What is preforming?

A

The processes used to convert intermediate products into suitable shapes for moulding (3D form from 2D intermediates)

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2
Q

What are some material joining techniques?

A

-Inter-ply stitching
-Adhesive binders (powder or solvent)
-Welding (thermoplastics)

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3
Q

What is the importance of preforming?

A

-Either manual or automated
-Directly influences: Cycle time (max parts/annum), cost and quality
-Typically involves head and/or pressure
-Affects impregnation with resin: Fibre volume fraction, Local fibre orientations, Layup sequence and Defects (wrinkles)
-Allows parts integrations (seamless joining of multiple parts)

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4
Q

What is the influence of preform compaction on resin flow?

A

-Over compaction of the preform affects resin flow, and therefore the fibre volume fraction which can be plotted as a function of compaction pressure
-Resin “race-tracking” (voids) occurs at fibre bends due to high pressure, leading to dry spots

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5
Q

What materials are used in Hand layup 3D preforming?

A

-Dry fabrics - woven or NCF
-Prepregs

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6
Q

How suitable is Hand layup 3D preforming for production volumes?

A

~1000 parts per annum
-Good for prototyping or small production runs

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7
Q

Why is high volume production expensive for Hand layup 3D preforming?

A

-Requires skilled labour
-Multiple tools used in parallel
-Long production and layup time
(used in aerospace, motorsport or marine)

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8
Q

Why does Hand layup 3D preforming have poor repeatability?

A

-Dependent on the experience of the operator
-Fabric shear during shaping on the tool
-High scrap rate (material wastage ~40%)

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9
Q

Why do some plies need to be ‘darted’ when designing for manufacture?

A

-Darting (small cuts to reduce wrinkles) conforms the plies to the curved tool
-However, stress concentrations are created (account for these in calculations)
-For “black metal” designs (unsuitable for automation)

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10
Q

List some advantages and disadvantages of using humans during the layup process

A

Advantages:
-Highly dexterous (layup movements)
-Good at visually spotting errors
-Adaptive (can perform multiple roles)

Disadvantages:
-Expensive, skilled labour
-Variability (due to user error)
-Can take short cuts
-Motivation required for repetitive tedious tasks

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11
Q

List some advantages and disadvantages of using robots during the layup process

A

Advantages:
-Strong
-Repeatable and more consistent
-High precision
-Fast
-Inexpensive
-Continuous work
-Able to work in dangerous/harsh environments

Disadvantages:
-Limited feedback
-Cannot take corrective action if there’s an error
-Not as fast as expected
-Limited movement envelope (hard to achieve straight line due to 6Dof)
-Dedicated to one role
-Requires skilled programmers

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12
Q

What are properties of Automated Tape Laying (ATL) 3D preforming?

A

-High cost
-High quality
-Prepreg tapes (continuous unidirectional 8”-12” wide) robotically placed on tool surface
-Simple 3D or 2D shaped parts achievable
-Automatic debulking of thermoset prepregs
-In-situ consolidation of thermoplastic prepregs
-Allows: tailored orientation, more intelligent use of materials, reinforcement of other substrates
-Wastage is dependent on size/shape of component & fibre orientations

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13
Q

What are challenges of Automated Tape Laying (ATL) 3D preforming?

A

-Void content increases with line feeding speed
-Expensive feedstock materials (due to required precision)
-Expensive machines (~£2mil+)
-Limited to simple geometries (due to size of placement head)
-Limited curvature (hard to shear wide tapes due to buckling)
-Limited accel/decel rates of machines
-Long machine setup times
-Lack of CAE design tools
-Layup quality depends on: humidity and age of prepreg

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14
Q

What are properties of Automated Fibre Placement (AFP) 3D preforming?

A

-Places individual tows, increasing precision
-Lays up to 32 tows at once
-AFP achieves greater precision than ATL
-More suitable for shorter courses
-Achieves moderate double curvature at slow speeds
-Lower material wastage than ATL
-Tow is more likely to fail in tension than tape

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15
Q

What are limitations of robotic grippers (needle gripper and vacuum gripper) for automated preforming?

A

Needle gripper; can damage plies

Vacuum gripper; limited by how much it can pick up)

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16
Q

What is/are the forming mechanism(s) for metal forming?

A

-Plastic deformation (material thinning)

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17
Q

What is/are the forming mechanism(s) for composite fabric forming?

A

Fibres are inextensible

-In-plane shear (trellising) is the primary mechanism
-Shear resistance (due to: fibre crimp constraining yarn rotation, friction between yarns (, tension of stitch for NCFs))

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18
Q

What are the challenges for 2D to 3D preforming?

A

-Wrinkling (reduces mechanical properties due to stress concentrations)
-Thickness uniformity (particularly around male corners)
-Fibre breakage (tool will close if pressure is too high)

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19
Q

What is the mechanism and measure for macroscale wrinkling (ply folds) in a fabric?

A

Mechanism:
-Transverse yarn compaction (shear locking)

Measure:
-Shear angle (locking angle)

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20
Q

What is the mechanism and measure for mesoscale wrinkling (bundle loops) in a fabric?

A

Mechanism:
-Longitudinal yarn compression (yarn buckling)

Measure:
-Fibre compressive stress (critical buckling stress)

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21
Q

What is the mechanism and measure for gaps/voids (laddering) in a fabric?

A

Mechanism:
-Intra-ply yarn spacing (intra-ply over-slippage)

Measure:
-Fibre tensile strain (fibre spacing)

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22
Q

What is the mechanism and measure for Stitch damage in a NCF?

A

Mechanism:
-Longitudinal stitch extension (stitch rupture)

Measure:
-Stitch stress (stitch strength)

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23
Q

What are the 3 main components in the 2D to 3D press forming process?

A

-Punch (male die)
-Die (female die)
-blank holder (applies tension to the fabric)

24
Q

What are the 4 stages in 2D to 3D press forming process?

A

-Tool opened, release agent is applied, blank is transferred to the mould
-Blank holder clamps the fabric stack around the edge of the cavity
-Male punch is driven by a hydraulic press (preform heated to activate binder)
-Tool is opened & preform is ejected

25
Q

What are the press forming variables on the forming tool?

A

-Blank holder arrangement
-Blank holder pressure
-Minimum radii
-Surface finish (COF)
-Temperature
-Closure rate (prepreg only)

26
Q

What are the press forming variables on the fabric blank?

A

-Material format (orientation, areal density, fibre constraints)
-Binder or resin content
-Ply shape
-Ply layup sequence relative to the forming tool
-Darts or slits

27
Q

Give an outline of single diaphragm forming (SDF)

A

-Typically used in aerospace to form long structures (spars <20m)
-Only suitable for single curvature components (folding)
-Single sided tool, with silicone membrane forming bag
-Heat applied by infra-red lamps

28
Q

What are the process steps for double diaphragm forming (DDF)?

A

DDF suitable for complex, double curved components

-Fabric plies sandwiched between diaphragms

-Vacuum drawn between 2 diaphragms to clamp the fabric

-Diaphragm heated (or raised to heating units) to activate the binder

-Quickly lowered onto contact tool (die)

-2nd vacuum (independent of the first) applied between lower diaphragm & die

-Preform cools below Tm of binder

-Vacuum removed, top diaphragm released first to prevent distortion

29
Q

What are the double diaphragm forming variables on the diaphragm?

A

-Material type
-Stress/strain profile & temp/time relationship
-Diaphragm thickness
-COF between diaphragm & fabric
-Vacuum level

30
Q

What are the double diaphragm forming variables on the diaphragm?

A

-Minimum radii
-Surface finish (COF)
-Temperature

31
Q

What are the double diaphragm forming variables on the risers &/or intensifiers?

A

-Shape
-X-Y position relative to the tool
-Height relative to the tool
-Material (stiffness)

32
Q

What are the double diaphragm forming variables on the fabric blank?

A

-Material format (orientation, areal density, fibre constraints)
-Ply shape
-Ply position/orientation (relative to forming tool)
-Binder/resin content
-Darts or slits

33
Q

Provide an overview of matched tool forming

A

-High CAPEX
-Non-isostatic pressure (problems for near vertical faces)
-High material wastage (additional blank material required for gripping
-Blank holder controls material draw-in and tension
-Preforms can be formed using multiple operations
-Blank holder used to locate/hold preform prior to forming

34
Q

Provide an overview of Single Diaphragm Forming (SDF)

A

-Low CAPEX
-Isostatic pressure
-Net-shape
-Limited control over material draw-in or fabric wrinkling
-Preforms can be formed using multiple operations
-Intensifiers can be placed inside (or incorporated within) the diaphragm
-Minimal spring-back (depends on release agent/film)
-Difficult to locate preforms prior to forming

35
Q

Provide an overview of Double Diaphragm Forming (DDF)

A

-Low CAPEX
-Isostatic pressure
-Net-shape
-Pressure between diaphragms can be regulated to control tension
-Lower membrane prevents multiple forming operations

-Difficult to incorporate intensifiers:
Lower membrane (wrong side of preform)
Upper membrane (may impede fabric slippage/draw-in)

-Problems removing preform (spring back of lower diaphragm)
-Lower diaphragm used to transport preforms

36
Q

Give an overview of the braiding Direct Textile Preforming method

A

-Interlacing of fibres about a mandrel (internal tube)
-May-poling action used to create prismatic shape (tubes with geometrical changes)
-Must be strong enough for braiding forces & resin injection
-Commonly biaxial (10 to 85 degrees) or triaxial

Fibre angles controlled by:
-Rotational speed of fibre carriers
-Axial speed of mandrel
-Number of fibre carriers
-Mandrel diameter

37
Q

Give an overview of the braiding complex geometries possibilities

A

-Concave/convex sections
-Square/circular sections
-Care required to avoid fibre bridging (control speed)
-Ply drops (change in number of layers) produced by reversing braid direction
-Displacers used to create holes, keeps fibres continuous, decreasing stress concentrations (1.8x higher strength)
-Superior fatigue performance compared to filament winding (due to interlacing)
-

38
Q

What are some advantages of braiding?

A

-Low wastage (<10%)
-High degree of automation
-High deposition rates
-Cycle time is independent on mandrel complexity
-Most efficient when braiding straight sections
-Suitable for structural applications (bending, torsion, crash)

39
Q

What are some disadvantages of braiding?

A

-Batch process (limited mass of fibre on bobbins)
-Long setup times & downtime initiating & terminating a part

40
Q

What are the 3 styles (Z binder yarn pattern) of 3D weaving?

A

-3D angle interlock
-3D orthogonal
-3D layer-to-layer

41
Q

What is a 3D weaved fabric?

A

Similar to 2D weaving, with the inclusion of high stiffness/strength fibres in the through-thickness (Z) direction (0.5-10%)

42
Q

What are properties of a 3D weaved fabric?

A

-High delamination fracture toughness
-High impact damage tolerance
-Higher through-thickness electrical & thermal conductivity

43
Q

How do z-fibres affect the in-plane performance of the laminate?

A

Depends on % content
-up to 25% reduction in stiffness
-up to 50% reduction in strength

44
Q

What are some limitations of 3D weaving production?

A

-Long machine setup time (due to number of creels)
-Limited preform width dur to available yarn ends
-Available preform width gets narrower as preform becomes thicker

45
Q

How can more complex geometries be produced using 3D weaving?

A

-Strategic removal of z-binder yarns in some regions, then hollow out

46
Q

What are some 3D weaving applications?

A

-Stiffeners for aerospace panels (T and pi cross-sections)
-Nodes for civil applications
-Turbine blades
-Fan casings

47
Q

Explain Embroidered fabric placement

A

-Reinforcement fibres are embroidered onto a substrate (fabric or polymer film)
-Net-shape with no waste
-Fibres can be steered through tight radii
-Used to reduce stress concentrations around holes/notches
-Stitches improve through thickness permeability
-Limited fibre deposition rates, parallel embroidery head can be used on a single part
-Standard tows can be used (minimising cost)

48
Q

Give an overview of random fibre products

A

-Low performance applications (usually marine)
-Low fibre volume fractions due to high bulk factor
-Difficult to form from sheet (risk of tearing as unable to shear uniformly in-plane)

49
Q

Give an overview of Directed Carbon Fibre Preforming (DCFP)

A

-Chopped fibres & resin randomly sprayed onto part (perforated screen)
-Easy to automate (high precision not required)
-For semi-structural components
-Preforms moulded using liquid resin methods

50
Q

What are the advantages of Directed Carbon Fibre Preforming (DCFP)?

A

-Rapid cycle time (5-10 mins)
-Low cost of raw materials
-Low use of intermediates
-Low wastage (2-5%)
-Complex geometry
-Parts integration
-Large parts (2-3m)
-Locally variable thickness

51
Q

What are the manufacture process steps of Directed Carbon Fibre Preforming (DCFP)?

A

-Fibre and binder deposited onto perforated screen/tool
-Heating and compression of preform (activates powdered binder)
-Cooling (freezes preform)
-Demoulding (extracts preform part)

52
Q

Explain the Directed Carbon Fibre Preforming (DCFP) chopper gun

A

-Fibre fed in by rollers into a pressure roller and chopper (number of blades determines the fibre lengths)
-Randomly oriented fibres
-Tuneable fibre deposition rate
-Scalable process
-Max volume fraction ~55%

53
Q

What are the challenges of Directed Carbon Fibre Preforming (DCFP)?

A

-Heterogeneous (different properties in different regions) as it’s not a laminate
-Many variables (orientation, tow size, fibre length, local Vf changes)
-Local stiffness & strength variations due to architecture
-Fibre homogeneity affected by fibre length and tow size
-Material stiffness & strength dependent on thickness (scale effects)

54
Q

What effect does thickness have on modulus for Directed Carbon Fibre Preforming (DCFP)?

A

Exponential curve, rapidly increasing modulus with thickness then plateauing

55
Q

What effect does volume fraction have on modulus for Directed Carbon Fibre Preforming (DCFP)?

A

Positive linear relationship

56
Q

What effect does volume fraction have on UTS for Directed Carbon Fibre Preforming (DCFP)?

A

Positive parabolic curve

57
Q

Discuss the permeability of Directed Carbon Fibre Preforming (DCFP)

A

-Local permeability is affected by heterogeneous fibre architecture
-Global permeability ~10x lower than for quasi-isotropic laminate of the same Vf
-Higher injection pressures required (risk of washing)
-Irregular resin flow (risk of dry spots in final moulding)
-Variability makes tool design & process simulation difficult