Common materials used in modern jet engines.
|
Material |
Component Used |
Key Properties |
Purpose |
|
Titanium
alloys |
Fan
blades, compressor |
High
strength-to-weight ratio, corrosion-resistant |
Lightweight
and strong for high-speed rotation |
|
Nickel-based
superalloys |
Turbine
blades, combustion chamber |
High-temperature
resistance, creep-resistant |
Maintains
integrity under extreme heat |
|
Stainless
steel |
Compressor
discs, casings |
High-strength, corrosion-resistant |
Durable
and resistant to environmental factors |
|
Aluminium
alloys |
Low-pressure
fan |
Lightweight,
moderate strength |
Reduces
overall engine weight |
|
Ceramics |
Turbine
coatings |
High
thermal resistance, low thermal conductivity |
Insulates
and protects metal components |
|
Carbon
composites |
Fan
blades, ducts |
Lightweight,
high fatigue resistance |
Reduces
weight while retaining strength |
|
Cobalt-based
superalloys |
Hot
section parts |
Excellent
oxidation and wear resistance |
Enhances
durability in extreme heat |
|
Inconel |
Combustion
chambers |
Corrosion-resistant,
high tensile strength |
Withstands
high temperatures and stresses |
|
Tantalum
alloys |
Combustion
chamber liners |
High
thermal stability |
Enhances
heat resistance |
|
Silicon
carbide (SiC) |
Turbine
components |
High-temperature
and chemical resistance |
Enables
higher operating temperatures |
|
Polymeric
composites |
Fan
casings, nacelles |
Lightweight,
impact-resistant |
Improves
efficiency and safety |
|
Titanium
aluminides |
Low-pressure
turbine blades |
High-temperature
strength, low density |
Improves
efficiency in low-pressure sections |
|
Magnesium
alloys |
Gearbox
components |
Lightweight,
moderate strength |
Reduces
weight in less critical areas |
|
Molybdenum
alloys |
Structural
components |
High-temperature
strength, wear-resistant |
Adds
strength in critical structural areas |
|
Glass-reinforced
composites |
Radomes,
fairings |
Transparent
to radar, lightweight |
Optimizes
aerodynamics and radar visibility |
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