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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Rolls-Royce_Trent_XWB-97
|
|
gptkbp:aircraft_operated
|
gptkb:Airbus_A350-900
gptkb:Airbus_A350-1000
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:bypass_ratio
|
9:1
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|
gptkbp:certification
|
gptkb:EASA
|
|
gptkbp:competitors
|
General Electric G Enx
|
|
gptkbp:controls
|
gptkb:Full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:design
|
Advanced aerodynamics
|
|
gptkbp:developer
|
Derived from Trent 1000
|
|
gptkbp:diameter
|
118 in
2.68 m
|
|
gptkbp:emissions_standard
|
Lower C O2 emissions
|
|
gptkbp:engine
|
gptkb:Trent_family
Advanced materials
High reliability
Modular design
High thrust-to-weight ratio
Low maintenance requirements
Composite fan blades
Advanced cooling techniques
Twin-engine
3 D-printed components
Optimized for long-haul flights
Digital engine monitoring
Efficient combustion system
Noise-reducing features
Robust performance in various conditions
Sustainable aviation fuel compatibility
|
|
gptkbp:engine_type
|
gptkb:6
gptkb:Trent_XWB-97
gptkb:Trent_XWB-75
2
High bypass turbofan
|
|
gptkbp:first_flight
|
gptkb:2013
|
|
gptkbp:fuel_capacity
|
High fuel efficiency
Lightweight design
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Trent XWB-84
|
|
gptkbp:introduced
|
gptkb:2012
|
|
gptkbp:is_tested_for
|
gptkb:aircraft
gptkb:Boeing_747-400
|
|
gptkbp:length
|
3.46 m
|
|
gptkbp:maintenance
|
Longer intervals than predecessors
|
|
gptkbp:manufacturer
|
gptkb:film_production_company
|
|
gptkbp:market
|
gptkb:Commercial_aviation
|
|
gptkbp:noise_level
|
Quieter than previous models
|
|
gptkbp:notable_feature
|
High bypass ratio
|
|
gptkbp:operational_area
|
Lower operating costs
|
|
gptkbp:order
|
Over 1,600 engines
|
|
gptkbp:propulsion
|
84,000 lbf
|
|
gptkbp:services
|
gptkb:2014
|
|
gptkbp:setting
|
twin-spool
|
|
gptkbp:weight
|
7,200 lb
|