Skip to main content
U.S. Department of Energy
Office of Scientific and Technical Information

The Rolls Royce Allison RB580 turbofan - Matching the market requirement for regional transport

Conference ·
OSTI ID:5577437

The RB580 high bypass turbofan engine has a thrust growth capability to 10,000 lb and has been optimized for efficient operation in regional markets involving 50-70 seat airliners with higher-than-turboprop cruise speeds. The two-spool engine configuration achieves an overall pressure ratio of 24 and features a single-stage wide-chord fan for high efficiency/low noise operation. The highly modular design of the configuration facilitates maintenance and repair; a dual-redundant full-authority digital electronic control system is incorporated. An SFC reduction of the order of 10 percent at cruise thrust is achieved, relative to current engines of comparable thrust class.

OSTI ID:
5577437
Report Number(s):
AIAA-Paper--89-2488; CONF-8907118--
Country of Publication:
United States
Language:
English

Similar Records

Advanced turbofan blade refurbishment technique
Journal Article · Sun Oct 01 00:00:00 EDT 1995 · Journal of Turbomachinery · OSTI ID:136527

Aircraft turbofans: new economic and environmental benefits
Journal Article · Sun Sep 01 00:00:00 EDT 1985 · Mech. Eng.; (United States) · OSTI ID:6201669

Turbofan engine cycle design selection - Year 2000
Conference · Tue Dec 31 23:00:00 EST 1985 · OSTI ID:6812643