翻訳と辞書 |
Rolls-Royce AE 2100 : ウィキペディア英語版 | Rolls-Royce AE 2100
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. The engine uses new six-bladed Dowty propellers for use on the 50-seat Saab 2000 and the Lockheed Martin C-130J Super Hercules military transport. Each engine develops 4,591 shaft horsepower. ==Applications==
;AE2100A * Saab 2000 * Indonesian Aerospace N-250 - Prototype only ;AE2100D2A * Alenia C-27J Spartan ;AE2100J * ShinMaywa US-2 ;AE2100D3 * Lockheed Martin C-130J Super Hercules * Lockheed P-3 Orion (test-bed)〔(AE 2100 Description )〕
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Rolls-Royce AE 2100」の詳細全文を読む
スポンサード リンク
翻訳と辞書 : 翻訳のためのインターネットリソース |
Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.
|
|