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Rolls Royce AE 3007

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Rolls-Royce AE 3007

The Rolls-Royce AE 3007 is a high-bypass turbofan engine produced by Rolls-Royce. In military service it is designated as F137.

Contents

Design and development

The engine was initially developed by the Allison Engine Company for use on the Cessna Citation X. The engine provides up to 9,440 lbf (42 kN) of thrust. It consists of a fan, 14-stage high-pressure compressor, 2-stage high-pressure turbine and 3-stage low-pressure turbine. It shares a common core with the AE 1107C-Liberty and AE 2100.

Variants

AE 3007C, C1, C2 for the Cessna Citation X
AE 3007H (F137) for the Northrop Grumman GlobalHawk and Triton
AE 3007A, A1, A1/1, A1/3, A3, A1P, A1E, A2 for the Embraer ERJ Family of Jets

Applications

  • Cessna Citation X
  • Embraer ERJ 145 family
  • Embraer Legacy 600
  • Embraer R-99 series
  • RQ-4 Global Hawk
  • Northrop Grumman MQ-4C Triton

    • Specifications (AE 3007)

    Data from

    General characteristics

  • Type: Turbofan
  • Length: 106.5 in (2,705 mm)
  • Diameter: 38.5 in (978 mm)
  • Dry weight: 1,585 lb (719 kg)

    • Components

  • Compressor: 14-stage high pressure axial compressor and single-stage fan
  • Turbine: 2-stage high pressure and 3-stage low pressure

    • Performance

  • Maximum thrust: 6,495–9,440 lbf (28.9–42.0 kN)
  • Overall pressure ratio: 18–20:1
  • Bypass ratio: 5.1
  • Air mass flow: 240–280 lb/s (109–127 kg/s)
  • Turbine inlet temperature: 994℃
  • Thrust-to-weight ratio: : 4.1–5.6

    • References

    Rolls-Royce AE 3007 Wikipedia
    (Text) CC BY-SA


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