Rolls-Royce AE 3007: Difference between revisions
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|length=106.5 in (2,705 mm)001001 |
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|weight=1,585 lb (719 kg) |
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Revision as of 11:40, 20 January 2017
 | This article includes a list of references, related reading, or external links, but its sources remain unclear because it lacks inline citations. (September 2009) |
| AE 3007 | |
|---|---|
| |
| AE 3007 mounted on a Cessna Citation X | |
| Type | Turbofan |
| National origin | United States |
| Manufacturer | Allison Engine Company Rolls-Royce North America |
| First run | 1991[1] |
| 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.
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 [citation needed]
General characteristics
- Type: Turbofan
- Length: 106.5 in (2,705 mm)001001
- 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 [2]
- 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
Comparable engines
- General Electric CF34
- Honeywell ALF 502/Honeywell LF 507
- Honeywell HTF7000
- Pratt & Whitney Canada PW300
Related lists
References
- ^ "Baby big fan". Flight Global. 10 April 1996.
- ^ https://www.flightglobal.com/news/articles/baby-big-fan-17332/
- 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
Wikimedia Commons has media related to Rolls-Royce AE 3007.