Trent 900 - Rolls-Royce Holdings · 900Trent © 2016 Rolls-Royce plc Vcom16983/4 Technical Data...
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Trent 900 www.rolls-royce.com © 2016 Rolls-Royce plc Vcom16983/4 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 Entry into service 2007 Thrust 70,000–72,000 lbf Airbus A380–800 The clear market choice for the Airbus A380
Transcript of Trent 900 - Rolls-Royce Holdings · 900Trent © 2016 Rolls-Royce plc Vcom16983/4 Technical Data...
Trent
900www.rolls-royce.com © 2016 Rolls-Royce plc Vcom16983/4
Technical DataConfiguration: 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
Entry into service 2007Thrust 70,000–72,000 lbfAirbus A380–800
The clear market choice for the Airbus A380