Rolls-Royce AE 3007
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| AE 3007 | |
|---|---|
| 300px | |
| AE 3007 mounted on a Cessna Citation X | |
| 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 MQ-4C Triton |
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
File:AE 3007engine2.JPG
Rolls-Royce AE 3007 installed on a Cessna Citation X undergoing maintenance
File:Brussels airport bmi RJXC 01.JPG
A Rolls-Royce AE 3007 installed on an Embraer ERJ 145
- 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[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
- Maximum thrust: 6,495–9,440 lbf (28.9–42.0 kN)
- Overall pressure ratio: 18–20:1
- Air mass flow: 240–280 lb/s (109–127 kg/s)
- Turbine inlet temperature: 994℃
- Thrust-to-weight ratio: : 4.1–5.6
See also
- Related development
- Related lists
References
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External links
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