Characteristics of a single-rotation drive system for an advanced turboprop engine are described. The gearbox is designed for a 10.000 shp three-spool, free-turbine engine and is installed in a wing-mounted nacelle. An offset gearbox from an earlier APET study provided the background for the preliminary design and benefit analysis for a 1990s advanced technology versus 1980s state-of-the-art gearbox. High efficiencies were achieved for both designs with inherently high life goals. Increases in design allowables for gears, bearings, and lubricants resulted in improvements for the 1990s design.
Advanced propfan drive system characteristics and technology needs
Eigenschaften und technologische Anforderungen an moderne Turbopropantriebssysteme
AIAA-Papers ; 1-8
1984
8 Seiten, 14 Bilder, 3 Tabellen, 7 Quellen
Aufsatz (Konferenz)
Englisch
Advanced single-rotation propfan drive system
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