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Presented by:
Kanchha Lama (0991904)
Parth Patel (0989754)
Pramith Varikoti (0988868)
 Introduction : What is composite?
 Why composite in Aerospace industry?
 Applications of composite in aerospace
 Future involvement of composite
 Conclusion
o Composite is material consisting of two or more
materials, which have different physical and chemical
properties, combined together in a proper content and
fashion to produce a new material properties that are
different from the properties of those individual
materials.
 The main aim of the aerospace/aircraft industries is to
reduce weight keeping the same or more strength
than the regular metals have.
 This criteria leads to use composite.
 Light weight
 High heat resistance
 High strength to weight ratio
 Low density
 Corrosion resistance
 High stiffness
 Fatigue resistance
Application of composite materials in aerospace industry (1)
 Fiber glass
 CFRP
 QFRP
 GFRP
 GLARE
Fuselage (Bulkhead)
Wing flaps
Rudder
Elevators
Radome
Spoilers
Floor beams and panels
Helicopter main and tail rotor blades
Space vehicles: Satellites, Missiles, Rockets etc.
Commercial :
o Boeing 777
o Boeing 787 Dreamliner
o Airbus A380
Military:
o B-2 Bomber
o LCA Tejas (HAL)
 Components that uses composite
structure are:
 Horizontal Stabilizer
 Vertical Fin
 Radom
 Wing fairings
 Passenger floor beams
 Wing Box
 Engine Cowlings
 Engine fairings
 Reduction in weight is over
5800 pounds.
 Components that uses composite structure are:
 Almost full fuselage
 Upper and lower wing skin
 Radom
 Wing flaps, elevators, ailerons
 Vertical Fin and Horizontal Stabilizer
 Use of composite is 80% by volume and 50% by weight.
 Components that uses composite
structure are:
 Horizontal Stabilizer
 Vertical Fin
 Radom
 Wing Fairings
 Wing Box
 Belly Fairings
 Engine Cowlings
 Engine fairings
 Wing box, made of CFRP, has reduced
weight up to one and a half tones.
 B-2 Bomber is mostly made of
carbon/epoxy materials.
 The reduction in weight was
about 40000 to 50000 pounds.
 Design material was specially
designed to absorb radar
waves.
 LCA stands for Light Combat Aircraft which is basically use of composite
materials in its structure.
 Components which are made of composite material are:
 Nose
 Wing upper surface and leading edge
 Exit Nozzle
 Weight is reduced by 21%
 Used to manufacture Rocket and Missiles motor cases.
Materials for this are carbon, aramid and glass.
 Composites like carbon-carbon are used to manufacture
re-entry nose tips and heat shields.
 Use of composite is more challenging to design.
 NDT test for composite material is much more difficult as
compared to metals.
 Delamination of layers.
 High cost
 Damage tolerance.
 Need specialized repair techniques.
Honeycomb Structure
 Honeycomb Structure
 Hybrid composite materials
 Advanced Designs through
Simulation
 Investigations into damage
tolerance of bonded repairs
by test and simulation.
 Since the invention of composite materials, aerospace industry
has shown significant use of it in building different parts first
to almost most of the structural parts and use of it is rapidly
growing.
 The main aspect we need to keep in mind that strength and
stiffness are major considerations for aircrafts whereas
stiffness and low coefficient of thermal expansion are major
considerations for space applications.
 Composite Materials. Retrieved from http://www.aviation-
history.com/theory/composite.htm.
 Creating a Titan. Retrieved from
 http://www.flightglobal.com/news/articles/creating-a-titan-199071.
 Daniel, I. M., Ishai, O.(2005). Engineering mechanics of composite materials.
Oxford, New York, 2, 3-4.
 Holly, R.H. (2013). The great metal tube in the sky. Retrieved from
 https://arch5541.wordpress.com/2013/01/08/the-great-metal-tube-in-the-sky.
 Honeycomb structure. Retrieved from
http://en.wikipedia.org/wiki/Honeycomb_structure.
 Hybrid material. Retrieved from http://en.wikipedia.org/wiki/Hybrid_material.
 LCA Tejas Technology. Retrieved from
 http://www.tejas.gov.in/technology/composite_materials.html.
 National Aeronautics and Space Administration. Composites. Retrieved from
 http://www.aeronautics.nasa.gov/pdf/composites_k-12.pdf.
 Northrop Grumman B-2 Spirit. Retrieved from http://www.military-
today.com/aircraft/b2_spirit.htm.
Thank You

More Related Content

Application of composite materials in aerospace industry (1)

  • 1. Presented by: Kanchha Lama (0991904) Parth Patel (0989754) Pramith Varikoti (0988868)
  • 2. Introduction : What is composite? Why composite in Aerospace industry? Applications of composite in aerospace Future involvement of composite Conclusion
  • 3. o Composite is material consisting of two or more materials, which have different physical and chemical properties, combined together in a proper content and fashion to produce a new material properties that are different from the properties of those individual materials.
  • 4. The main aim of the aerospace/aircraft industries is to reduce weight keeping the same or more strength than the regular metals have. This criteria leads to use composite.
  • 5. Light weight High heat resistance High strength to weight ratio Low density Corrosion resistance High stiffness Fatigue resistance
  • 7. Fiber glass CFRP QFRP GFRP GLARE
  • 8. Fuselage (Bulkhead) Wing flaps Rudder Elevators Radome Spoilers Floor beams and panels Helicopter main and tail rotor blades Space vehicles: Satellites, Missiles, Rockets etc.
  • 9. Commercial : o Boeing 777 o Boeing 787 Dreamliner o Airbus A380 Military: o B-2 Bomber o LCA Tejas (HAL)
  • 10. Components that uses composite structure are: Horizontal Stabilizer Vertical Fin Radom Wing fairings Passenger floor beams Wing Box Engine Cowlings Engine fairings Reduction in weight is over 5800 pounds.
  • 11. Components that uses composite structure are: Almost full fuselage Upper and lower wing skin Radom Wing flaps, elevators, ailerons Vertical Fin and Horizontal Stabilizer Use of composite is 80% by volume and 50% by weight.
  • 12. Components that uses composite structure are: Horizontal Stabilizer Vertical Fin Radom Wing Fairings Wing Box Belly Fairings Engine Cowlings Engine fairings Wing box, made of CFRP, has reduced weight up to one and a half tones.
  • 13. B-2 Bomber is mostly made of carbon/epoxy materials. The reduction in weight was about 40000 to 50000 pounds. Design material was specially designed to absorb radar waves.
  • 14. LCA stands for Light Combat Aircraft which is basically use of composite materials in its structure. Components which are made of composite material are: Nose Wing upper surface and leading edge Exit Nozzle Weight is reduced by 21%
  • 15. Used to manufacture Rocket and Missiles motor cases. Materials for this are carbon, aramid and glass. Composites like carbon-carbon are used to manufacture re-entry nose tips and heat shields.
  • 16. Use of composite is more challenging to design. NDT test for composite material is much more difficult as compared to metals. Delamination of layers. High cost Damage tolerance. Need specialized repair techniques.
  • 17. Honeycomb Structure Honeycomb Structure Hybrid composite materials Advanced Designs through Simulation Investigations into damage tolerance of bonded repairs by test and simulation.
  • 18. Since the invention of composite materials, aerospace industry has shown significant use of it in building different parts first to almost most of the structural parts and use of it is rapidly growing. The main aspect we need to keep in mind that strength and stiffness are major considerations for aircrafts whereas stiffness and low coefficient of thermal expansion are major considerations for space applications.
  • 19. Composite Materials. Retrieved from http://www.aviation- history.com/theory/composite.htm. Creating a Titan. Retrieved from http://www.flightglobal.com/news/articles/creating-a-titan-199071. Daniel, I. M., Ishai, O.(2005). Engineering mechanics of composite materials. Oxford, New York, 2, 3-4. Holly, R.H. (2013). The great metal tube in the sky. Retrieved from https://arch5541.wordpress.com/2013/01/08/the-great-metal-tube-in-the-sky. Honeycomb structure. Retrieved from http://en.wikipedia.org/wiki/Honeycomb_structure. Hybrid material. Retrieved from http://en.wikipedia.org/wiki/Hybrid_material. LCA Tejas Technology. Retrieved from http://www.tejas.gov.in/technology/composite_materials.html. National Aeronautics and Space Administration. Composites. Retrieved from http://www.aeronautics.nasa.gov/pdf/composites_k-12.pdf. Northrop Grumman B-2 Spirit. Retrieved from http://www.military- today.com/aircraft/b2_spirit.htm.