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 Non-Ferrous Alloys
Al alloys
Cu alloys
Mg Alloys
Ti and Ni alloys
Limitations of ferrous alloys
Steel and other ferrous alloys are consumed in exceedingly
large quantities because they have such a wide range of
mechanical properties, may be fabricated with relative ease,
and are economical to produce.
However, they have some distinct limitations,
chiefly:
(1)a relatively high density,
(2)a comparatively low electrical conductivity,
(3) an inherent susceptibility to corrosion in some common
environments.
Thus, for many applications it is advantageous or even
necessary to utilize other alloys having more suitable
property combinations.
Aluminum (Al) Alloys
Aluminium alloys can be can be classified
 Wrought alloys
 Cast alloys
Each of these alloys can be further classified
(a) Non heat treatable alloys
(b) Heat treatable alloys
Classification
Alloys that are so brittle that forming or
shaping by appreciable deformation is not
possible ordinarily are cast; these are
classified as cast alloys.
On the other hand, those that
are amenable to mechanical deformation are
termed wrought alloys.
Aluminum and Its Alloys
 Aluminum and its alloys are characterized by a relatively low density
(2.7 g/cm3 as compared to 7.9 g/cm3 for steel)
 High electrical and thermal conductivities, and
 Resistance to corrosion in some common environments, including the
ambient atmosphere.
 Many of these alloys are easily formed by virtue of high ductility; this
is evidenced by the thin aluminum foil sheet into which the relatively pure
material may be rolled.
 Since aluminum has an FCC crystal structure, its ductility is retained
even at very low temperatures.
 The chief limitation of aluminum is its low melting temperature (660 C),
which restricts the maximum temperature at which it can be used.
Mechanical Strength
 The mechanical strength of aluminum may be enhanced by cold
work and by alloying; however, both processes tend to diminish
resistance to corrosion.
 Principal alloying elements include copper, magnesium, silicon,
manganese, and zinc.
 Nonheat-treatable alloys consist of a single phase, for which an
increase in strength is achieved by solid-solution strengthening.
 Others are rendered heat treatable (capable of being precipitation
hardened) as a result of alloying.
 In several of these alloys precipitation hardening is due to the
precipitation of two elements other than aluminum, to form an
intermetallic compound such as MgZn2
Specific strength
 Recent attention has been given to alloys of aluminum
and other low-density metals (e.g., Mg and Ti) as
engineering materials for transportation, to effect
reductions in fuel consumption.
 An important characteristic of these materials is specific
strength, which is quantified by the tensile
strength–specific gravity ratio.
 Even though an alloy of one of these metals may have a
tensile strength that is inferior to a more dense material
(such as steel), on a weight basis it will be able to
sustain a larger load.
Al alloys: Types
Al- Li Alloy
 A generation of new aluminum–lithium alloys have been
developed recently for use by the aircraft and aerospace
industries.
 These materials have relatively low densities (between
about 2.5 and 2.6 g/cm3), high specific moduli (elastic
modulus specific gravity ratios), and excellent fatigue
and low-temperature toughness properties.
 Furthermore, some of them may be precipitation
hardened. However, these materials are more costly to
manufacture than the conventional aluminum alloys
because special processing techniques are required as a
result of lithium’s chemical reactivity
APPLICATIONS
Applications based on above properties are very wide.
 Aluminium alloys are widely used for aeronautical applications because of
high strength weight ratio.
 For automobiles for reducing weight of the vehicle thus reducing fuel
consumption.
 For applications as electrical conductors including overhead transmission
lines.
 For Packaging of food and medicines because of non-toxic nature and good
corrosion resistance.
 House hold and consumer items such as utensils.
 Architectural applications such as windows, doors and railings.
 For surface transport such as fittings in railway coaches and buses.
 For heat exchanger purposes because of the good thermal conductivity.
 Marine applications.
 Used as sacrificial anode.
Applications of pure aluminium however are rather limited.
APPLICATIONS
Application in Specific Sectors
 Transport sector accounts for nearly 18% of the total aluminium
consumption in India.
 Lower density is the prime reason for their preference in this sector
but good thermal conductivity is another major consideration.
 Development of more brazeable and durable aluminium alloys has
lead to total conversion to aluminium alloy heat exchangers.
 Radiators, heater cores and air conditioner evaporators fabricated
from improved brazing sheet products can now be reliably brazed by
vacuum or by non corrosive flux techniques.
 These components have corrosion life expectancies at least two to
three times the life of copper based products.
AA7075 alloy: Grain boundaries
and Precipitates
Non ferrous al alloy

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Non ferrous al alloy

  • 1.  Non-Ferrous Alloys Al alloys Cu alloys Mg Alloys Ti and Ni alloys
  • 2. Limitations of ferrous alloys Steel and other ferrous alloys are consumed in exceedingly large quantities because they have such a wide range of mechanical properties, may be fabricated with relative ease, and are economical to produce. However, they have some distinct limitations, chiefly: (1)a relatively high density, (2)a comparatively low electrical conductivity, (3) an inherent susceptibility to corrosion in some common environments. Thus, for many applications it is advantageous or even necessary to utilize other alloys having more suitable property combinations.
  • 4. Aluminium alloys can be can be classified  Wrought alloys  Cast alloys Each of these alloys can be further classified (a) Non heat treatable alloys (b) Heat treatable alloys Classification
  • 5. Alloys that are so brittle that forming or shaping by appreciable deformation is not possible ordinarily are cast; these are classified as cast alloys. On the other hand, those that are amenable to mechanical deformation are termed wrought alloys.
  • 6. Aluminum and Its Alloys  Aluminum and its alloys are characterized by a relatively low density (2.7 g/cm3 as compared to 7.9 g/cm3 for steel)  High electrical and thermal conductivities, and  Resistance to corrosion in some common environments, including the ambient atmosphere.  Many of these alloys are easily formed by virtue of high ductility; this is evidenced by the thin aluminum foil sheet into which the relatively pure material may be rolled.  Since aluminum has an FCC crystal structure, its ductility is retained even at very low temperatures.  The chief limitation of aluminum is its low melting temperature (660 C), which restricts the maximum temperature at which it can be used.
  • 7. Mechanical Strength  The mechanical strength of aluminum may be enhanced by cold work and by alloying; however, both processes tend to diminish resistance to corrosion.  Principal alloying elements include copper, magnesium, silicon, manganese, and zinc.  Nonheat-treatable alloys consist of a single phase, for which an increase in strength is achieved by solid-solution strengthening.  Others are rendered heat treatable (capable of being precipitation hardened) as a result of alloying.  In several of these alloys precipitation hardening is due to the precipitation of two elements other than aluminum, to form an intermetallic compound such as MgZn2
  • 8. Specific strength  Recent attention has been given to alloys of aluminum and other low-density metals (e.g., Mg and Ti) as engineering materials for transportation, to effect reductions in fuel consumption.  An important characteristic of these materials is specific strength, which is quantified by the tensile strength–specific gravity ratio.  Even though an alloy of one of these metals may have a tensile strength that is inferior to a more dense material (such as steel), on a weight basis it will be able to sustain a larger load.
  • 10. Al- Li Alloy  A generation of new aluminum–lithium alloys have been developed recently for use by the aircraft and aerospace industries.  These materials have relatively low densities (between about 2.5 and 2.6 g/cm3), high specific moduli (elastic modulus specific gravity ratios), and excellent fatigue and low-temperature toughness properties.  Furthermore, some of them may be precipitation hardened. However, these materials are more costly to manufacture than the conventional aluminum alloys because special processing techniques are required as a result of lithium’s chemical reactivity
  • 11. APPLICATIONS Applications based on above properties are very wide.  Aluminium alloys are widely used for aeronautical applications because of high strength weight ratio.  For automobiles for reducing weight of the vehicle thus reducing fuel consumption.  For applications as electrical conductors including overhead transmission lines.  For Packaging of food and medicines because of non-toxic nature and good corrosion resistance.  House hold and consumer items such as utensils.  Architectural applications such as windows, doors and railings.  For surface transport such as fittings in railway coaches and buses.  For heat exchanger purposes because of the good thermal conductivity.  Marine applications.  Used as sacrificial anode. Applications of pure aluminium however are rather limited.
  • 13. Application in Specific Sectors  Transport sector accounts for nearly 18% of the total aluminium consumption in India.  Lower density is the prime reason for their preference in this sector but good thermal conductivity is another major consideration.  Development of more brazeable and durable aluminium alloys has lead to total conversion to aluminium alloy heat exchangers.  Radiators, heater cores and air conditioner evaporators fabricated from improved brazing sheet products can now be reliably brazed by vacuum or by non corrosive flux techniques.  These components have corrosion life expectancies at least two to three times the life of copper based products.
  • 14. AA7075 alloy: Grain boundaries and Precipitates