Rolls-Royce AE 3007

From Wikipedia, the free encyclopedia
Jump to: navigation, search
AE 3007
Brussels airport bmi RJXC 01.JPG
A Rolls-Royce AE 3007 installed on an Embraer ERJ 145
Type Turbofan
National origin United States
Manufacturer Allison Engine Company
Rolls-Royce North America
First run 1990s
Major applications Cessna Citation X
Embraer ERJ 145 family
RQ-4 Global Hawk

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

Design and development[edit]

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[edit]

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[edit]

Specifications (AE 3007)[edit]

Data from[citation needed]

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

See also[edit]

Related development
Related lists

References[edit]

  • Leyes II, Richard A.; William A. Fleming (1999). The History of North American Small Gas Turbine Aircraft Engines. Washington, DC: Smithsonian Institution. ISBN 1-56347-332-1. 

External links[edit]