Palm Cards Flashcards

1
Q

Define a Laminate

A

Laminate is a product
made by bonding
together two or more thin
layers (plies or laminae)
of materials. Most
common composites
employed in aircraft
industry are polymer
matrix laminates.

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2
Q

Driving factors for composite selection

A

Weight, strength, resistance to environmental effects, performance under temperature extremes, resistance to damage and fatigue. Assembly costs

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3
Q

Role of both the fibers and the matrix in a complete composite.

A

Fibers: Oriented for principal stress/es in order to carry the major load/s

Matrix: Transmits load to/from fiber. Shapes and protects.

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4
Q

At what orientation relative to fiber direction is the composite strongest?

A

Along fiber direction

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5
Q

Polymer Matrix Composites (PMCs) vs Metals

A
  1. Properties are not uniform in all directions
  2. Strength and stiffness can be tailored to meet loads
  3. Possess a greater variety of mechanical properties
  4. Have poor through the thickness (short transverse) strength
  5. Are usually laid up in two dimensional form, while metals
    may be used in billets, bars, forgings, castings, etc.
  6. Have greater sensitivity to environmental heat and moisture
  7. Possess greater resistance to fatigue damage
  8. Damage propagates through delamination rather than
    through-the-thickness cracks
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6
Q

PMC Advantages Over Metals

A
  • Light weight
  • Resistance to corrosion
  • High resistance to fatigue damage

Reduced machining

Tapered sections and compound contours easily
accomplished

Strength and stiffness can be tailored

Reduced number of assemblies and reduced fastener count
when co-cured or co-consolidation is used

Absorb radar microwaves (stealth capability)

Near zero thermal expansion reduces thermal problems in
outer space applications

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7
Q

PMC Disadvantages Over Metals

A

Composite Materials are expensive

Less historical data and established design allowables

Corrosion problems can result from improper coupling with
metals, especially when graphite is used (sealing is
essential)

Degradation of structural properties under temperature
extremes and wet conditions

Poor energy absorption and impact damage resistance

May require lightning protection

Expensive and complicated inspection methods

Reliable detection of substandard bonds is difficult

Internal nature of defects makes damage assessment
difficult

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8
Q

Reasons for Lower-than-Expected Usage of Composites

A

High Cost of raw materials and manufacture

High Cost of Certification

Low Resistance to Impact

Damage and transverse cracking

Limited applicability at high temperatures

Advancement in aluminium alloys
(improved toughness,
fatigue resistance and corrosion resistance)

Development of new light weight alloys (Al-Li)

Low cost aerospace grade castings, mechanical alloying and
super-plastic forming, diffusion bonding

Advanced joining techniques for metals (laser and friction
welding, automated riveting

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9
Q

Different Types of Polymers

A
  • Polymer Matrix Composites
  • Metal Matrix Composites
  • Ceramic Matrix Composites
  • Carbon Carbon Composites

Hybrid Metal/PMC Composites

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10
Q

Types of Matrix Reinforcements

A
  • Continuous Fibers made from light elements (C, B, Si, etc)
  • Whiskers: Ultra strong, stiff, short fibers made up of single crystals
  • Particulates: Mainly ceramic, to improve toughness of brittle matrices
  • Nanotubes
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11
Q

Types of strengths provided by a matrix

A

Transverse, Shear, Compressive

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12
Q

Service temperatures of the different composite types

A

PMC: Less than 300 deg

MMC: Less than 650 deg

CMC: Less than 1400 deg

C/C: Greater than 1400 deg

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13
Q

Overview of PMC Benefits

A

Light weight, high performance
fibers in organic polymer matrices

Usually processed at low temperatures and pressures.

reasonably low cost.
Easier to machine, mould and fabricate

Limited high temperature applications

Susceptible to environmental degradation

Includes thermosets and thermoplastics.

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14
Q

MMCs compared to PMCs

A

Higher temperature resistance.

High melting point

High ductility and toughness

Higher dimensional stability (low CTEs)

Mostly heavier than PMCs

Costly, complex and limited fabrication techniques

Problems with thermal coefficient mismatch and poor
interfacial bonding between reinforcements and matrices

Susceptible to corrosion

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15
Q

Types of MMCs

A

Aluminium Metal

Magnesium and Copper

Titanium Alloys Intermetallics

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16
Q

Types of MMC Reinforcements

A

Continuous Fibers

Whiskers

Particulates

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17
Q

Manufacturing Methods for MMCs

A

Rapid liquid metal processes such as squeeze casting

Powder metallurgy processes based on heating

compacted metal powders to just below their melting
points to consolidate them (Hot Isostatic Press)

Some conventional metal working techniques for
particulate MMCs

Super plastic forming

Diffusion bonding (for Ti matrix systems)

Additive manufacturing.

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18
Q

Types of ceramic composites, and their operating temperatures

A
  1. Glass ceramics (up to 500deg)
  2. Oxides (?)
  3. Nitrides (up to 1400 deg)
  4. Carbides (Over 1400 deg)
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19
Q

Overview of ceramic composites

A

Ceramic matrices reinforced with continuous fibres,
whiskers or particulates

High temperature applications in gas turbine engines and
high temperature airframe/space structures

Ceramics are brittle and subject to microcracking at high temperatures

Hence reinforcing fibres with high strength and stiffness
that have chemical stability and resistance to oxidation at
high temperatures as well as matching CTEs are required

Hence it is common to use similar materials for both
reinforcement and matrix such as SiC/SiC and alumina
fibres in alumina matrix.

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20
Q

Features of C/C Composites

A

C/C has the best structural properties (specific
strength, specific stiffness, creep resistance, at the highest
operating temperatures (over 20,000 C) of all materials

Further it has no significant chemical or thermal expansion
compatibility problems

Its greatest disadvantage is susceptibility to oxidation at
high temperatures

Hence C/C is the main candidate for use in rocket nosecones, nozzles, and leading edges on hypersonic wings.

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21
Q

Advantages of Hybrid Metal/PMC Composites

A

Combines the advantages of metals (such as high
resistance to low velocity impact damage) with the advantages of
PMCs (such as high fatigue life).

They typically consist of thin sheets of metal (usually Aluminium)
bonded together with a fibre reinforced adhesive.

Much higher fatigue lives than
monolithic alloys and greater impact resistance than PMCs

They have lower densities than aluminium, higher post yield
strength and higher damping capacity

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22
Q

Disadvantages of Hybrid Metal/PMC Composites

A

Higher sensitivity to blunt notches,

lower elastic modulus than monolithic aluminium

Possibility of earlier
crack initiation, and

high cost.

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23
Q

Types of Fiber Metal Laminates

A

ARALL, GLARE

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24
Q

Explain how fiber form of a material relates to the probability of a defect being present

A

Elements of low atomic number have strong directional inter-atomic bonds.

The strong bonding inhibits plastic flow, so they are very
sensitive to sub-microscopic flaws.

These materials can achieve very high strengths when made
into fibers due to the probability of a flaw being present
being proportional to the volume of the materials for a given length.

However, for the same reason, they also become very sensitive to flaws, exhibiting a much higher variability in
strength compared to bulk materials.

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25
Explain why fibers have high strength
The probability of a flaw being present is proportional to the volume of the materials for a given length (and fibres have very low cross sectional area). Flaws can be minimized by proper manufacturing and coating procedures Drawing and spinning impose high strains along the fibre axis produces a more favourable orientation of crystal structure High cooling rate or rapid molecular deposition produces ultrafine grained structures with much higher properties.
26
Explain the process used to manufacture glass fibers
Glass is first melted at temps between 12500 and 14000 C Flows into an electrically heated alloy bushing which contains a large number of holes at its base The glass drops emerging from the holes are drawn into fibres at speeds of up to 50 m/s They are cooled by a water spray and coated with a “size” by a rolling applicator Finally the fibres are combined into a strand (of 52, 102 or 204 fibres) and wound on to a take-up spool
27
How do the properties of glass fiber differ from those of the bulk material?
The cooling rate experienced by the fibres is very high (greater than 10,0000 C per sec) Hence the fibre structure is different from that of bulk glass, resulting in a higher tensile strength but lower elastic modulus and chemical resistance
28
Outline how flaws affect glass fibres
Glass fibres, being essentially monolithic, linearly elastic brittle materials, are very sensitive to flaws in the form of sub-microscopic inclusions and cracks Commercial fibres are particularly prone to abrasion against other fibres, resulting in a reduction in strength of up to 20% compared to pristine fibres Humid environments reduce the strength of glass fibres under sustained loading due to adsorption of moisture on to the surface causing “static fatigue” Individual fibre strength is reduced by about 50% in a PMC, but the bundling of the fibres overcomes this effect.
29
Define the two types of glass fiber
1. E-Glass: Calcium Alumino-Borosilicate used for electrical applications due to its higher electrical resistivity. 2. S Glass: Magnesium Alumino-Silicate, used for structural applications due to its higher strength and low cost
30
What is 'Size', and why is it used?
Consists of a lubricant, binders such as starch and polyvinyl alcohol (to hold filaments together) and primers to improve adhesion between fibres and matrices. Reduces damage caused by friction upon fibres.
31
Carbon Fiber: - Why is it used - What Types - What is it made from
1. High specific strength and stiffness 2. High Modulus, High Strength, Intermediate Modulus 3. Organic precursor materials (PAN and Pitch) by a process of carbonization.
32
What is PAN
PolyAcryloNitrile is an acrylic textile fibre
33
How is PAN manufactured:
By wet or dry spinning of the polymer or co-polymer, and then stretching. Stretching of fibres during spin reduces the diameter, aligns more molecular chains along the length, increasing stiffness
34
How is carbon fiber manufactured from PAN?
Stage 1 – Stabilisation: PAN is first stabilised in air at about 2500C by oxidation to form a thermally stable ladder polymer, with a high glass transition temperature (Tg). Stage 2 – Carbonisation: Removal of N, O and H in an inert nitrogen atmosphere at 1200-16000C. Fibres develop full strength at 1500-16000C. Basal planes align along the fibre axis, but remain as extended 2D ribbons. Stage 3 – Graphitisation: Final heat treatment at 1500-25000C in an inert atmosphere (Argon), wherein basal layers grow and coalesce along the fibre direction, to provide higher E (up to 380 GPa) at the cost of lower strain capability (0.7%) and strength.
35
What is Pitch? What are its advantages and drawbacks?
Precursor made of organic compounds Cheap but poor mechanical properties Low compression, shear and tensile properties. High electrical and thermal conductivity. No tension required to develop molecular orientation (unlike PAN).
36
How is Pitch manufactured into carbon fiber
Stage 1 – Isotropic to Mesophase Pitch: Isotropic pitch is subjected to prolonged heating in an inert atmosphere at 400- 4500C to form a liquid crystal phase (mesophase) which is meltspun into fibre form Stage 2 – Cross linking: To reduce relaxation, the pitch fibres are cross linked by heating for a short time at 3000C in atmosphere containing O2. Stage 3 – Pre Carbonisation Stage 4 – Carbonisation Stage 5 – Graphitisation
37
Benefits and drawbacks of Boron fibers. How are they made
Very hard Difficult to machine Chemical vapor deposition
38
Properties of Aramid fibers
Superior Specific Properties: Higher specific properties compared to glass fibers. Tensile Properties: Good tensile properties up to 400°C. Compressive Strength: Poor compressive strength limits applications. Energy Absorption: High energy absorption during fracture. High strain-to-failure. Applications: Used in ballistic protection and engine containment rings Anisotropic Properties: Strong covalent bonds within chains and weak hydrogen bonds between chains result in anisotropic properties. Non-linear Compression: Highly non-linear under compression due to kink band formation from in-phase compressive buckling of fibrils. Thermal Stability: Strength reduces by about 20% at 180°C, with rapid decline thereafter. Hygroscopic Nature: Absorbs moisture (around 4% at 60% relative humidity for Kevlar 49), but tensile strength remains largely unaffected. Creep Characteristics: Significant short-term creep, negligible long-term creep. UV Degradation: Susceptible to UV degradation, but protected in PMCs by resin matrix.
39
Properties of polyethylene fibres
Tough Operate best under 100 deg temps Poor creep behavior Low compressive strengths due to kink band formation Specific strengths comparable to aramids.
40
List the types of dry fiber forms
1. Mats 2. Woven Fabrics 3. Warns 4. Tows 5. Rovings 6. Braided Fabrics 7. Non-Crimp Fabrics 8. Tapes 9. 3D textile preforms
41
Function of the matrix
Provides shape Holds the fibres together Transfers load in and out of fibres Separates the fibres to prevent failure from adjacent fibres Protects fibres from environmental damage Determines “matrix dominated” properties: - Longitudinal compressive strength - Transverse tensile strength - Intra and interlaminar shear strength
42
Service temps for different matrix types
1. Low temp thermosets (epoxies, polyesters, vinyl esters, phenolic resins) = 100 - 150 deg 2. Medium temp thermosets (Bismaleimides) = Up to 230 deg 3. High temp thermosets (Polyimides) = Up to 300 deg
43
Properties of an epoxy resin
1. Excellent chemical and mechanical properties at low temps 2. Low viscosity during curing, enabling easier forming 3. Low shrinkage 4. Good fiber adhesion 5. Tg increases with increasing cure temperature
44
Limitations of epoxy resins
Low toughness, and sensitive to impact damage Limited temp range Absorbs moisture Sensitive to UV exposure High cost compared to polyesters Less convenient curing compared to polyesters
45
List the additives used in epoxy resins, and describe their effects
1. Diluents Added to reduce viscosity before cure 2. Flexibilizers Added to reduce elastic modulus and increase elongation to failure 3. Toughening agents Increase fracture toughness and reduce crack propagation rates 4. Inert fillers, such as hollow glass microspheres: Added to alter density, resin flow and effective modulus
46
List and describe the mechanisms through which an epoxy resin can be toughened.
Formation of a solid solution with a more ductile polymer Precipitation of elastomeric second phase Development of interpenetrating polymer networks The inclusion of elastomeric second phase can be achieved by adding an elastomer (rubber) to form a copolymer with the base resin which then precipitates out upon curing to form a dispersed second phase Adding a very fine powder to form a dispersion
47
List the advantages of polyester resins
Initial low viscosity that permits good wetting of the fibres Low cost (inexpensive and readily available raw materials, easy long term storage) Cure conditions can be modified easily without too much expertise Easy manufacture of modifications for a variety of specific applications Excellent environmental durability
48
List the disadvantages of polyester resins
High exotherm and high shrinkage on cure (this leads to residual stresses and poor interfacial bonding with fibres) Lower values for mechanical properties than epoxies Systems with adequate shear strength tend to be brittle (low toughness) Toughening mechanisms are relatively ineffective Poor chemical resistance
49
List the general properties of vinyl-ester resins
Intermediate class of materials between epoxies and polyesters The major ester ingredient is produced by reaction of a standard epoxy and methacrylic acid The resins are cured by free radical reaction process like polyesters Tougher and more chemically resistant than polyesters due to less cross linking Large range with different mechanical properties, including rubber toughened resins
50
Outline the advantages and disadvantages of vinyl-ester resins
Advantages: Combines chemical resistance of epoxies with easy processing of polyesters Lower cross linking, hence better mechanical properties than polyesters Improved interfacial bond strength with fibres Disadvantages: High cost compared to polyesters Higher shrinkage levels than epoxies
51
Outline a general description of phenolic resins
Condensation polymerisation of phenol with formaldehyde under alkaline or strong acid conditions is used to produce a pre-polymer called “resol”. This is polymerised under heating or with acidic or basic catalysts to form densely cross-linked structure forming the matrix Water and volatile byproducts are formed in the reaction, hence high pressures are required for curing High void content
52
State the advantages and disadvantages of phenolic resins
Advantages Excellent resistance to high temperatures, especially under oxidizing conditions Phenolics have good ablation properties, forming char readily, yielding a superficial layer of carbon, which burns away protecting the underlying composite Good as fire retardant materials Disadvantages High pressures needed for polymerisation, hence difficult to fabricate Significantly lower mechanical properties due to high void content
53
What are the two types of Polyimide Resins? What is special about them?
1. Condensation polyimides - Thermoplastics used as matrices or toughening mechanisms in high temperature epoxy formulations 2. Addition polyimides thermoSETs. In general they release large quantities of volatiles unless high temperatures and pressures are employed, hence fabrication is complex and expensive 3. Very high Tg
54
Advantages and disadvantages of Polyimide Resins?
Advantage: Stability at high temperatures (up to 3000C) Resistance to most chemicals Can be formulated to give better mechanical properties Disadvantages High Cost Difficulty in processing
55
List the requirements of the component manufacturing process
To orient the fibres in the appropriate directions and proportions to obtaine the desired 2D or 3D properties Produce the required shape of the component Verify properties To ensure that the fibres state and orientation Ensure free of defects
56
Procedure, Pros, Cons: Wet Lay-Up
Fibres laid up in open mould, with resin added by brushing or spraying Labour intensive, with challenging quality control Cost effective
57
Procedure, Pros, Cons:
“Pre-pregs” are sheets of fibre reinforcement pre-impregnated with partially cured resin. Safer, cleaner, more consistent, less labor intensive Costly with limited shelf life
58
List all composite manufacturing processes
1. Wet Lay Up 2. Pre-Preg 3. Wrapping 4. Compression Die Moulding 5. Open Die Moulding
59
How must pre-preg materials be stored
Refridgerated
60
Draw a pre-preg manufacturing set-up
Picture
61
Draw an autoclave process graph (Temp/Time)
Picture
62
List the resin moulding techniques, and draw each one
Resin Transfer Moulding Resin Film Infusion Vacuum Assisted RTM
63
Advantages/Disadvantages of Liquid Resin Moulding
Advantages: Can be used for manufacturing complex shapes and parts Materials can be selected to obtain the desired properties Process can be tailored to each individual type of component to maximise efficiency Disadvantages: Tooling is very costly Initial set up time is time consuming and expensive Process is time consuming and laborious High operator skill and experience required Very low through put
64
Explain Filament Winding
Process that enables continuous reinforcement to be laid down at high speed and precision in predefined paths The process involves impregnating continuous fibres with resin and winding them on to a stationary or rotating mandrel.
65
Pros/Cons of filament winding
Advantages: High speed and high precision process Fully automated High fibre volume ratios can be achieved Can be employed to make very large components Disadvantages: Tooling is very costly Initial set up time is time consuming and expensive
66
Explain Pultrusion
Highly automated, continuous linear process for manufacturing of components with constant cross-sectional profiles with fibre reinforced PMCs The process essentially involves impregnating continuous fibres with a thermosetting resin and pulling them through a heated die to shape and cure
67
Pultrusion pros/cons
Advantages: Continuous process Fully automated High throughput Can use inexpensive forms of reinforcement Can be employed to make very long components No lamination or autoclave curing is required No requirement to refrigerate raw materials Disadvantages: Tooling can be costly Initial set up time is time consuming and expensive Process can only be applied to parts with constant cross section
68
Outline the manufacturing process for thermoplastics
- Very viscous, so liquid resin moulding techniques don't work - Requires only heat and pressure over a short period of time - High temp and High Pressure
69
Define: 1. Isotropic 2. Anisotropic 3. Orthotropic 4. Transversely Isotropic
1. Has the same material properties in all directions (infinite number of planes of symmetry) 2. Has different material properties in different directions with no planes of symmetry 3. Has three planes of symmetry for its material properties 4. Material with one plane (at every point) in which the properties are the same in all directions
70
Define the longitudinal and transverse modulus
Longitudinal: Stiffness in fiber direction = E1 Transverse: Stiffness across fiber direction = E2
71
Define the Major and Minor Poisson's Ratio
Major = v12 = -E2/E1 Minor = v21 = -E1/E2
72
Relation between E and v
(V12/E1) = (v21/E2)
73
List the methods used to calculate the mechanical properties of a single lamina from the known properties of the fiber and matrix
1. Mechanics of materials approach 2. Theory of elasticity approach 3. Finite Element Modelling
74
What assumptions are involved in determining elastic constants using Micromechanics:
The fibres are assumed to be homogeneous, linearly elastic, isotropic, regularly spaced, perfectly aligned and of uniform strength The matrix is assumed to be homogeneous, linearly elastic and isotropic The fibre matrix interface is assumed to be perfect with no voids or dis-bonds The lamina is orthotropic along its principal directions The composite is considered to be homogeneous
75
State the Rule of Mixtures Mechanics of Materials Approach Equation
E1 = Ef*Vf + Em * Vm For: - E1 = Longitudinal Modulus - Ef = E of fibres - Vf = Volume fraction of the fibers - Em = E of Matrix - Vm = Volume fraction of matrix (1-Vf)
76
What is G12
In Plane Shear Modulus
77
"Sigma 1 t" notation meaning
Tensile strength in fiber direction (1)
78
Types of glass fibers and their mechanical properties
1. E-Glass: moderate strength and stiffness, low cost, non-structural and semi-structural applications 2. S-Glass: higher strength and higher stiffness than E-Glass, cost comparable to that of Carbon/epoxy, employed for some structural components 3. D-Glass: better dielectric properties than E-glass, protection against lightning strikes
79
Compare the general properties of glass fibres with those of other types of PMCs
Cheaper for non or less load bearing structures Density comparable to that of Boron/epoxy (B), higher than aramid/epoxy (A) and carbon/epoxy (C) Lower specific stiffness than all three (A,B and C) Not employed for weight critical load bearing structures Better dielectric properties than other PMCs
80
Describe the fatigue properties of Glass fiber composites
Poor comparative fatigue performance Particularly vulnerable in hot and wet conditions due to low conductivity and moisture ingress tendencies
81
Outline the properties of GFRP relating to impact strength and environmental degradation
Superior ability to absorb impact energy Degrades significantly in extreme environments
82
Pros and Cons of GFRP
Advantages of GFRP Low cost Superior Impact Resistance Better dielectric Properties Disadvantages of GFRP Lower specific stiffness than all other PMCs Poorer fatigue performance Susceptible to Stress rupture Degradation of Properties due to moisture and other aggressive environments
83
Advantages and Disadvantages of Aramid composites
Advantages: - Low density - Mid-range specific strength and stiffness - Low creep rate - Good tensile properties - High impact resistance Disadvantages: - Poor compressive strength - Poor fiber adhesion - Difficult to machine - High absorption
84
4 Different classifications of CFRP fibers
1. High Strength 2. High Modulus 3. Intermediate Modulus 4. Ultra High Modulus
85
2 different TYPES of CFRP fibres. Pros/Cons to each
1. PAN: Low Cost, higher strain to failure. Less stiff 2. Pitch: More conductive, More stiff. More expensive
86
4 different CFRP Matrix types in order of low-to-high temp ranges
1. Thermoplastics (*?) 2. Epoxy Resins 3. Bismaleimides 4. Polyimides
87
What properties in a CFRP matrix are dependent on the matrix?
1. Strain-to-Failure 2. Compressive Strength 3. Interlaminar Shear
88
Explain what is meant by 'adequate' interfacial bonding.
Carbon fibres are normally surface treated to develop adequate interfacial bonding. Too strong bonding is not desirable as the fibre should be capable of disbonding to alleviate local stress concentrations such as at microcracks
89
Rank composite impact resistance (most to least)
1. GFRP 2. Aramid 3. CFRP (least)
90
What is BVID and what does it affect?
- Barely Visible Impact Damage -Can significantly affect the residual compressive strength and buckling resistance by causing significant reductions in the bending stiffness of the laminate
91
Outline the desirable trend for fibre to matrix stiffness ratio, and why:
Maintain high fibre to matrix stiffness ratio so that the matrix strains are kept low to avoid matrix cracking
92
Discuss the fatigue resistance properties of CFRP:
- Generally, fatigue resistant - At moderate strain levels fatigue resistance of CFRP is strain dependent with fibre bridged matrix cracking and disbonding - Fatigue of CFRP at low strain levels causes only a small amount of matrix cracking which can lead to environmental damage.
93
Fatigue Resistance of GFRP
Glass fibres exhibit degradation of strength under fatigue Low modulus of glass fibres causes high matrix strains leading to matrix cracking, which exacerbates fatigue sensitivity by causing strain concentration and exposing fibres to environment
94
Fatigue Resistance of Aramids
Between GFRP and CFRP
95
Why is combined high matrix toughness and high adhesion bad?
Allows damaged fibres to be isolated from the good fibres by matrix cracking, disbonding and formation of delaminations.
96
97
Three phases of tension fatigue in cross-ply laminates
1. Cracking in the off axis plys accumulate leading to saturation of matrix cracks 2. Crack coupling and delaminations develop which slowly increase the stresses carried by the on-axis ply 3. Zero degree fibres begin to fail under the tensile load leading to final fracture
98
Effects of stress concentrations on composites
Minimal due to formation of microcracking and delamination
99
Effects of loading frequency on GFRP and CFRP
GFRP: Frequencies over 5 Hz can reduce fatigue performance due to accumulation of heat damage due to the poor thermal conductivity of glass fibres CFRP: Minimal
100
Outline the factors involved in compressive strength of composites
Depends on the ability of the matrix to support the fibres to avoid micro buckling which depends on interfacial bond strength and the presence of matrix cracks
101
What negatively effects the compressive strength of a composite
Hot/wet conditions, due to lowering of the Tg and softening of the matrix
102
What type of composite is greatly affected by BVID
CFRP - The BVID delaminations grow marginally under fatigue loading, which leads to a small drop in fatigue strength or fatigue life. - Greater effect on static residual strength
103
What is the mechanism for water absorption into a matrix
hydrogen bonding with polar sites in the polymer molecule
104
What types of matrices are most/least polar
1. Epoxies most 2. Phenolics least
105
What law governs water ingress
Fick's Law
106
Effects of temperature in moisture absorption
1. High Temp: vaporizes leading to matrix cracking 2. Low temp: freezing = expansion 3. Room temp: plasticiser of the resin system and degrades the mechanical properties at room temperature
107
Water affect on Tg - and result
Reduces. Lower high temp performance
108
Water ingress differing effects on matrix and fiber dominated composites
1. Fiber: Compression and buckling 2. Matrix: Tensile strength and stiffnes
109
4 stages of quality assurance
1. Control of raw materials 2. Monitoring of manufacturing 3. QA of finished product 4. In service damage monitoring
110
Mechanical properties tested
longitudinal tensile strength, elastic modulus, elongation, yield, density, twist, creep and sizing content
111
Types of QA tests
1. Mechanical 2. Chemical 3. Xray 4. Pressure 5. Optical 6. Ultrasonic
112
Method of cure monitoring
Measurement of temperature variations and electrical conductivity KNOW GRAPH (slide 13)
113
Types of composite damages
1. Fiber breaks 2. Matrix cracks 3. Delaminations
114
Methods of ultrasonic testing (common in aviation)
1. Pulse-Echo 2. Through transmission
115
Techniques of US testing
A and C scans
116