Things To Know Flashcards
Sae 1st digit
Primary alloying element
Sae last two digits
Percentage of hundredths of a precentor carbon in steel
Sae 2XXX
Nickle
Sae 1020 carbon content
.20%
Low carbon steel
0.03 - 0.3
Medium carbon steel
0.3 - 0.8
High carbon steel
0.8 - 1.4
The lower Critical Point of all Steel
723deg C
0.83 carbon steel when heated the Lower and Upper
Critical points converge and is called
Eutectoid point
After Steel is cold worked, bent, rolled it is
Annealed, Normalised
Hardening causes Steel to be brittle and is reduced by
Tempering
Lowest heat treatment
Tempering
Heat treatment
Annealing-Normalising- Hardening-
Tempering and surface hardening
Steel that is Forged
Normalizing
Heat treatment for Steel
hardening, tempering , normalizing
Heat treatment - Case hardening are
Carburising, Nitriding
Case hardening hard wear
resistant surface over strong core, tough
Nitriding
Case hardening
Carburising
is Case hardening
Heat treatment
age hardening
Young’s Modulus tests
Tensile load
Young’s modulus/ test material resistance
Strain under tensile loads
High longitudinal modulus of elasticity
Young’s modules
CRES what group
Austenitic group
Tensile tests the
Strength of metal
Tensile strength
Stretching material
Hooke’s Law Stress
is directly proportional to Strain
Creep is
When a metal is subject to both Tensile Stress and High Heat over a long period
Fatigue strength test
Repeated Stress Cycles
Fatigue strength test determines
life span of material
Prone to Fatigue
Effects Life Span
What do you measure in the Brinell test
diameter of the impression
Impact resistance test Izod
Toughness
Vickers hardness tester use a
Diamond
To measure Brinell Impression you use
Calibrated Microscope
What point is on Brinell tester
Ball
What point can be on Rockwell hardness tester
Conical Diamond
Aluminium Alloy AA1017 what is the first Digit
Alloy type
AA1017 what is the second Digit
Modification of Alloy
AA1017 Third and Fourth digit.
Percentage of Purity of Aluminium above 99%
AA 5056 Alloy
Magnesium
AA 2024 alloy
copper
AA 3003 alloy
Manganese
7075 Al
Zinc
5052 alloy
Magnesium Can be Welded, High strength, ductile
1100 Pure Aluminium
High electrical conductivity
2117-T3
Solution Heat treatment -cold worked
T6
Solution Heat treatment and Artificial Ageing
2024-T6
Solution heat treated and Precipitation treated
T3
Al solution heat treatment & cold worked
T3
Solution heat treatment and Strain hardening
Slow down Ageing process
Freezing to -20 degree
T4
Solution Heat treatment & Natural ageing
Alclad
Thin layer of pure Al on both sides of 2024-T4
Fuselage skin made from
CLAD 2024-T3
Core material of Alclad 2024-T4
Solution Heat treated Aluminium Alloy/surface pure aluminium
Repeat Annealing will cause
Material to Crack/ less strength
Treatment for non-heat treatable Alloy
Cold working
Skin of Firewall made from
Titanium
Strength of non-heat treatment aluminium increases with.
Strain hardening
Strength of non-heat treatment aluminium increases with
cold Working
In Appearance Titanium is similar to
stainless steel
Aluminium heat treated to specific temperature for a set Time and Quenched is?
Solution Heat Treatment
Pure Aluminium on both surfaces
Process to prevent Corrosion
Failure to Quench Aluminium in time
Impairs Corrosion resistant Qualities
Further name for Precipitation heat treatment.
Artificially aged
Material to Clad Aluminium Alloy
Pure Aluminium
O
Temper Designation for Aluminium Annealed cold
H
Metal cannot be heat treated-Hardened by Cold
working
Another Term for Artificial aging
Precipitation heat treatment
AA numbering system-second digit
Alloy Modification
Where is Cast Aluminium found on
aircraft Gearbox
Fuselage’s are generally made from
2024-T3
Melting point of Aluminium
660 degree
Where is Aluminium used
Fuselage skin
Nickle-chromium-Iron Alloy used for
Temperature sensing bulbs
Silver Solder melting point
460 deg C
Sintering Bronze used in
small oil retaining Bearings
Solder Tin/Lead 60/40 melting point
187 deg C
Heat treatable Aluminium alloy’s
2,6,7,8 Series
Hooke’s law
Strain is proportional to stress
Tensile strength
Max force divided by cross section area
Strength increase non heatable alloy
cold working
Spherical penetrator used by
Brinell
Impact tester
toughness
Creep
Tensile stress & high temp - long time
Advantage of Epoxy resin
Low Shrinkage and High strength to weight ratio
Temperature moisture should be removed at
150 degree F
What direction is honeycomb replaced
ribbon direction
Information about working on Resin
Material Safety data
Chopped strand Mat
Fibres are short
Pattern of Honeycomb
Hex
Shelf Life
Length of Time Resin is Stored
Curing Agent
Epoxy resin
Load carrying property of Fibre
Fibre Length
Carbon Graphite Fibre
is Stiff-High Compression Strength-Corrode
aluminium
Forms of Fibre
Mat-Woven- Strains- Chopped
Glass or Composite Plastic are
Thermosets
Honeycomb Core for Al Nomex Glass – Kevlar
Kevlar
Catalyst in Polyester resin
Aids joining Polyester Modules
Polyester Resin to Cure
Requires Heat
Honeycomb compared to sheet metal Adv.
Rigidity
Micro Balloons added to Epoxy resin
Add Volume-light in weight
Gains of Honeycomb over Soft Metal
Rigidity
Kevlar is strongest
Tension –strength
Dermatitis
Skin contact resin
Honeycomb Core
Nomex
Composites used
Lighter than metal
Increase temperature in cold cure resins
decreases Pot life
Black Composite material
Carbon
Epoxy type
Thermoset
Pot Life
resin Length of time resin remains useable
Nomex honeycomb made from
Resin impregnated synthetic Fibre
Unidirectional weave cloth used when
Strength in one direction
3 properties of Composites
Strength-Stiff- Impact resistance
Chopped strands Mat in woven fabric
Fibres are short
4 types of honeycomb core
Nomex, aluminium, Glassfibre, Kevlar
Water in composite
X Ray
Composite Delamination
Core from Face sheet
Washing Hands
Cold water
Bonding of Composite
Tap test
Damage composite
refer to SRM