FAA Aviation Mechanic Powerplant (AMP)Turbine EnginesMedium

A technician compares materials used in a turbofan engine's compressor and turbine sections. Which statement correctly describes typical material selection?

  1. AFront compressor stages use nickel-based superalloys for high strength at low weight, while turbine discs use aluminum for heat resistance
  2. BFront compressor stages use ceramic matrix composites exclusively, while turbine sections use titanium alloys
  3. CBoth compressor and turbine sections use the same aluminum alloys throughout for weight savings
  4. DFront compressor stages commonly use titanium alloys for their strength-to-weight ratio, while turbine discs and blades use nickel-based superalloys for high-temperature strength
Show answer & explanation

Correct answer: D. Front compressor stages commonly use titanium alloys for their strength-to-weight ratio, while turbine discs and blades use nickel-based superalloys for high-temperature strength

Front compressor stages operate at relatively lower temperatures, so lightweight, strong titanium alloys are commonly used. Turbine discs and blades face extreme temperatures and stresses, requiring nickel-based superalloys (and sometimes single-crystal castings) for high-temperature strength and creep resistance.

Why the other options are wrong

  • A. Aluminum cannot withstand turbine section temperatures.
  • B. Ceramic matrix composites are used selectively, not exclusively, and titanium is unsuitable for turbine hot sections.
  • C. Aluminum is unsuitable for turbine hot-section temperatures.

Turbine Engine Material Selection

Titanium alloys are typically used in cooler front compressor stages for strength-to-weight benefits, while nickel-based superalloys are used in the hot turbine section for high-temperature strength and creep resistance.

  • Titanium: front compressor, moderate temps
  • Nickel superalloys: turbine discs/blades, high temps
  • Some turbine blades use single-crystal casting
  • Ceramic matrix composites emerging in hot sections

Memory trick: Cool front = titanium, hot back = nickel superalloy

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