C-17 Globemaster III

PRIME CONTRACTOR:
Boeing

ENGINE CONTRACTOR:
Pratt & Whitney F117-PW-100 (PW 2041 derivative)

 

C-17 Globemaster III
Nacelle/Propulsion System

Triumph Aerostructures Responsibility
Triumph Aerostructures-Produced Integrated Aerostructures

C-17 Globemaster III Nacelle/Propulsion SystemNacelle systems include:

  • Inlet
  • Fan Cowl Door
  • Fan Reverser
  • Core Reverser

Responsibility


Triumph Aerostructures completes the following:

  • Engine Build-Up
  • Podding
  • Fabrication
  • Assembly
  • Systems Testing


Triumph Aerostructures delivers four nacelles per shipset.

Key Product Features

  • Multiple Materials
    • Composites
    • High-temperature Composites
    • Aluminum
    • Titanium
    • Inconel
  • Spray-on Insulation and Blankets
  • In-flight Reversing
  • Targeted Full-reverse Thrust
  • Reverse Ground Running Operable

Feature

Enables Aircraft To

Fully reversible thrust in flight

Perform tactical descent.

On-ground continuous operations

Perform engine running operations (ERO).

Both fan and core air reversed

Perform unimpeded ramp loading.

More than 10,000 pounds thrust per engine

Back up a 2-percent grade, fully loaded; land in less than 3,000 feet; and do a three-point turn.

All air directed up and forward

Operate with no ground disturbance.

No engine reingestion of reverse air

Perform continuous operations without engine problems.

Meeting FAA Stage 3 noise requirements

Operate out of commercial airports.