Rolls-Royce AE 2100
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| AE 2100 | |
|---|---|
| Type | Turboprop |
| National origin | United States |
| Manufacturer | Allison Engine Company Rolls-Royce plc |
| Major applications | C-130J Hercules C-27J Spartan ShinMaywa US-2 |
The Rolls-Royce AE 2100 is a turboprop. Developed by Allison Engine Company, now part of Rolls-Royce North America, derivative of the Allison T406 (Rolls-Royce AE 1107C-Liberty) turboshaft engine, and shares the same high-pressure core as the engine, as does the Rolls-Royce AE 3007. The engine is a two-shaft design and is 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 defence variant the AE2100D3.
The engine uses new six-bladed Dowty propellers for use on the 50-seat Saab 2000 and the Lockheed C-130J Hercules military transport. According to Lockheed each engine develops 4,591 shaft horsepower, an increase of about 300 over the engines in the 'H' model C-130.
Contents |
[edit] Applications
- AE2100A
- AE2100D3
[edit] See also
[edit] References
- Rolls-Royce - http://www.rolls-royce.com/defence_aerospace/downloads/transport/ae2100.pdf
- Lockheed Martin C-130J specification booklet - http://www.c-130j.ca/document/Spec_Book.pdf
- Canadian C-130J site - http://www.c-130j.ca/index.php?page=capabilities&lang_id=1&page_id=33
[edit] External links
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