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Rolls Royce AE 2100

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Rolls-Royce AE 2100

The Rolls-Royce AE 2100 is a turboprop developed by Allison Engine Company, now part of Rolls-Royce North America. A derivative of the Allison AE 1107C-Liberty (Rolls-Royce T406) turboshaft engine, the AE 2100 shares the same high-pressure core as that engine, as does the Rolls-Royce AE 3007 turbofan. The engine is a two-shaft design, and was the first to use dual FADECs (full authority digital engine control) to control both engine and propeller. There are two versions of the engine: the civil AE2100A, and the AE2100D3 military variant.

Contents

The engine uses new six-bladed Dowty propellers for use on the 50-seat Saab 2000 and the Lockheed Martin C-130J Super Hercules military transport. Each engine develops 4,591 shaft horsepower.

Applications

AE2100A
  • Saab 2000
  • Indonesian Aerospace N-250 - Prototype only
  • AE2100D2A
  • Alenia C-27J Spartan
  • AE2100J
  • ShinMaywa US-2
  • AE2100D3
  • Lockheed Martin C-130J Super Hercules
  • Lockheed P-3 Orion (test-bed)
  • Specifications (AE 2100D2)

    Data from Rolls-Royce product data sheet.

    General characteristics

  • Type: Turboprop
  • Length: 118 in (3.0 m)
  • Diameter: 28.7 in (0.73 m)
  • Dry weight: 1,727 lb (783 kg)
  • Components

  • Compressor: 14-stage axial
  • Turbine: 2-stage HP, 2-stage PT
  • Performance

  • Maximum power output: 4,637 shp (3,458 kW)
  • Overall pressure ratio: 16.6:1
  • Power-to-weight ratio: 2.7 shp/lb (4.53 kW/kg)
  • References

    Rolls-Royce AE 2100 Wikipedia


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