|The Rolls-Royce AE 2100 D2A of a C-27J|
|National origin||United States|
|Manufacturer||Allison Engine Company
|Major applications||Lockheed Martin C-130J Hercules
Alenia C-27J Spartan
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. 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.
Specifications (AE 2100D2)
Data from Rolls-Royce product data sheet.
- Type: Turboprop
- Length: 118 in (3.0 m)
- Diameter: 28.7 in (0.73 m)
- Dry weight: 1,727 lb (783 kg)
- Compressor: 14-stage axial
- Turbine: 2-stage HP, 2-stage PT
- 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)
- Related development
- Related lists
- 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.
|Wikimedia Commons has media related to Rolls-Royce AE 2100.|
- AE 2100 product page at rolls-royce.com
- Lockheed Martin C-130J specification booklet
- Canadian C-130J site