| タイトル | Ultra-efficient Engine Diameter Study |
| 本文（外部サイト） | http://hdl.handle.net/2060/20030061085 |
| 著者（英） | Brown, Stephen T.; Kawai, Ron T.; Daggett, David L. |
| 著者所属（英） | Boeing Commercial Airplane Group |
| 発行日 | 2003-05-01 |
| 言語 | eng |
| 内容記述 | Engine fan diameter and Bypass Ratio (BPR) optimization studies have been conducted since the beginning of the turbofan age with the recognition that reducing the engine core jet velocity and increasing fan mass flow rate generally increases propulsive efficiency. However, performance tradeoffs limit the amount of fan flow achievable without reducing airplane efficiency. This study identifies the optimum engine fan diameter and BPR, given the advanced Ultra-Efficient Engine Technology (UEET) powerplant efficiencies, for use on an advanced subsonic airframe. Engine diameter studies have historically focused on specific engine size options, and were limited by existing technology and transportation infrastructure (e.g., ability to fit bare engines through aircraft doors and into cargo holds). This study is unique in defining the optimum fan diameter and drivers for future 2015 (UEET) powerplants while not limiting engine fan diameter by external constraints. This report follows on to a study identifying the system integration issues of UEET engines. This Engine Diameter study was managed by Boeing Phantom Works, Seattle, Washington through the NASA Glenn Revolutionary Aero Space Engine Research (RASER) contract under task order 10. Boeing Phantom Works, Huntington Beach, completed the engine/airplane sizing optimization, while the Boeing Commercial Airplane group (BCA) provided design oversight. A separate subcontract to support the overall project was issued to Tuskegee University. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | NASA/CR-2003-212309
NAS 1.26:212309
E-13893 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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