trent xwb - rolls-royce holdings · pdf technical data configuration: three-shaft turbofan...

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www.rolls-royce.com Technical Data Conﬁguration: Three-shaft turbofan Bypass Ratio: 9.6:1 Overall Pressure Ratio: 50:1 Fan: 22 blades, 118” diameter Intermediate Pressure Compressor: 8 stages High Pressure Compressor: 6 stages Noise: QC 0.5 departures/ QC 0.5 arrivals High Pressure Turbine: Single stage Intermediate Pressure Turbine: Dual stage Low Pressure Turbine: 6 stages Entry into service 2014 Thrust 84,000–97,000 lbf Airbus A350–900 Airbus A350–1000 The world’s most eﬃcient large aero engine Trent © 2015 Rolls-Royce plc Vcom16983/4 XWB

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Page 1: Trent XWB - Rolls-Royce Holdings · PDF Technical Data Configuration: Three-shaft turbofan Bypass Ratio: 9.6:1 Overall Pressure Ratio: 50:1 Fan: 22 blades, 118” diameter

www.rolls-royce.com

Technical DataConfiguration: Three-shaft turbofan

Bypass Ratio: 9.6:1

Overall Pressure Ratio: 50:1

Fan: 22 blades, 118” diameter

Intermediate Pressure Compressor: 8 stages

High Pressure Compressor: 6 stages

Noise: QC 0.5 departures/ QC 0.5 arrivals

High Pressure Turbine: Single stage

Intermediate Pressure Turbine: Dual stage

Low Pressure Turbine: 6 stages

Entry into service 2014Thrust 84,000–97,000 lbfAirbus A350–900 Airbus A350–1000

The world’s most efficient large aero engine

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© 2015 Rolls-Royce plc Vcom16983/4

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