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Rolls-Royce Trent The clear market choice for the Airbus A380 Entry into service 2007 Technical Data Configuration: Three-shaft turbofan Bypass Ratio: 7:7-8:5 Overall Pressure Ratio: 39:1 Fan: 24 blades, 116” diameter Intermediate Pressure Compressor: 8 stages High Pressure Compressor: 6 stages Noise: QC 2 departures/ QC 0.5 arrivals High Pressure Turbine: Single stage Intermediate Pressure Turbine: Single stage Low Pressure Turbine: 5 stages
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