Aeronautical Engineering

NSWEngineering StudiesSyllabus dot point

Engineering materials: How are composite materials used in modern aircraft like the Boeing 787 and Airbus A350, and what advantages do they provide over aluminium?

Describe the structure, properties and manufacturing of carbon fibre reinforced polymer used in modern airframes, identify advantages over aluminium, and apply this knowledge to the Boeing 787 and Qantas operations

A focused answer to the HSC Engineering Studies Aeronautical Engineering dot point on aircraft composites. CFRP construction, autoclave manufacturing, Boeing 787 Dreamliner half-composite airframe, fatigue and corrosion advantages, Qantas Project Sunrise, and worked HSC-style past exam questions.

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What this dot point is asking

NESA wants you to describe carbon fibre reinforced polymer (CFRP) as used in modern aircraft, identify the manufacturing process, compare CFRP with aluminium on a property-by-property basis, and apply this to the Boeing 787 Dreamliner and Qantas long-haul operations.

The answer

What CFRP is

CFRP combines high-strength carbon fibres (typically 7 micron diameter) in an epoxy resin matrix. Fibres carry the tensile and compressive load; the matrix transmits load between fibres and protects them from environment. The fibres are oriented based on the load direction at each point in the structure (laminated layups with plies at 0°, 90°, +45° and -45° to give multi-directional strength).

Manufacturing

Modern aerospace CFRP is made by pre-preg autoclave processing:

  1. Pre-impregnated fabric. Woven or unidirectional carbon fibre tape impregnated with B-stage epoxy resin at the factory and stored frozen.
  2. Layup. The pre-preg is laid into a mould by hand or by automated tape laying machines, building up the laminate orientation according to the design.
  3. Vacuum bagging. The laminate is covered with release film, breather cloth and a vacuum bag; the bag is evacuated to consolidate the plies.
  4. Autoclave cure. The whole mould goes into an autoclave at about 180 degrees C and 7 bar for 2 to 6 hours. Heat cures the resin; pressure consolidates the plies and crushes voids.
  5. Demould and trim. The part is removed from the mould, trimmed and inspected by ultrasonic non-destructive testing for delamination.

Larger structures (787 fuselage barrels) use automated fibre placement machines that lay narrow tows of pre-preg over a rotating mandrel, building the barrel as a single piece. This eliminates the longitudinal seam that aluminium fuselages need.

Property comparison

Property Aluminium 2024-T3 CFRP (quasi-isotropic)
Density (kg/m^3) 2780 1600
Tensile strength (MPa) 485 600 to 800
Specific strength (MPa per kg/m^3) 0.174 0.38 to 0.50
Modulus (GPa) 73 70 (quasi-isotropic)
Fatigue endurance (MPa) 138 350+
Corrosion Galvanic, requires cladding None
Recycling High value scrap Pyrolysis, emerging
Cost per kg A5A5 | A50

Specific strength: CFRP is roughly twice as strong per unit mass as aerospace aluminium. The factor doubles in fatigue-limited applications because CFRP has a much higher fatigue threshold.

Where CFRP is used in modern airliners

The Boeing 787 uses composites for:

  • Fuselage barrels (one-piece, no longitudinal seams)
  • Wings (upper and lower skins, spars)
  • Empennage (horizontal and vertical stabilisers)
  • Doors, fairings, control surfaces

Total composite content by mass: about 50 percent on the 787, 53 percent on the Airbus A350, and about 35 percent on the A380.

Limits and trade-offs

CFRP wins on mass, fatigue and corrosion but loses on cost, repairability and impact tolerance. Specific issues:

  • Lightning strike protection requires a copper or aluminium mesh in the outer ply.
  • Impact damage can produce barely-visible delaminations that need ultrasonic inspection.
  • Repair of composites is more complex than aluminium patches; bonded scarf repairs require trained technicians and sometimes a return to a maintenance base.
  • Disposal at end-of-life is difficult; thermoset epoxies cannot be remelted, although pyrolysis recovery of carbon fibre is an emerging industry.

Qantas and the long-haul market

Qantas Airlines operates the Boeing 787-9 on routes including Perth-London (14{,}500 km, 17 hours) and Sydney-San Francisco. Project Sunrise (formally announced in 2022, first flights expected 2026-2027) will use the Airbus A350-1000 for Sydney-London non-stop. Both aircraft rely on the CFRP airframe for the fuel economy and cabin environment that make ultra-long-haul economically viable.

Past exam questions, worked

Real questions from past NESA papers on this dot point, with our answer explainer.

2023 HSC style5 marksThe Boeing 787 Dreamliner uses carbon fibre reinforced polymer for 50 percent of its airframe by mass. Discuss the advantages of CFRP over aluminium alloys for a long-haul airliner, with reference to one Qantas operational advantage.
Show worked answer →

Carbon fibre reinforced polymer (CFRP) has roughly the same yield strength as aerospace aluminium but at 60 percent the density. The Boeing 787 uses CFRP for the fuselage barrels, wings, empennage and most secondary structure. The 50 percent composite content delivers three engineering advantages over the previous-generation Boeing 767.

Mass reduction
A composite airframe is 20 percent lighter than an equivalent aluminium structure. Less mass means less lift required, which means less induced drag, which means less fuel burn per kilometre. The 787 is about 20 percent more fuel efficient per passenger-kilometre than the 767 it replaces.
Higher cabin pressure and humidity
Aluminium fuselage skins suffer corrosion and fatigue cracking under high humidity and pressurisation cycles. CFRP is immune to corrosion and has better fatigue tolerance under cyclic loading, so the 787 can pressurise the cabin to 6000 ft altitude equivalent (versus 8000 ft for aluminium aircraft) and run the cabin at 15 percent relative humidity. Passenger fatigue and dehydration on long-haul flights are reduced.
Lower maintenance and longer life
No skin corrosion to inspect, no zinc-chromate primer to maintain. Composite damage is less common from typical impact events. Boeing claims 30 percent lower scheduled maintenance hours per flight cycle than for the 767.
Qantas operational advantage
Qantas operates a fleet of Boeing 787-9 aircraft on the Perth to London direct route (17 hours, 14{,}500 km). The 20 percent fuel reduction and the larger cabin make this ultra-long-haul route economically viable. Qantas Project Sunrise (Sydney to London non-stop) plans to use the Airbus A350-1000, which has even higher composite content.

Markers reward (1) the mass reduction and fuel-efficiency link, (2) the corrosion and fatigue advantage, (3) at least one specific cabin-environment advantage, and (4) a named Qantas operation or route.

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