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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:Airbus
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gptkbp:armament
|
gptkb:26
composite
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gptkbp:bypass_ratio
|
9.0
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|
gptkbp:cancellation_reason
|
yes
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gptkbp:certification
|
EASA and FAA certified
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gptkbp:compressor_type
|
axial compressor
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gptkbp:configuration
|
twin-spool
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gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
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air-cooled
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gptkbp:diameter
|
2.7 m
118 in
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gptkbp:elevation
|
43,000 ft
|
|
gptkbp:emissions_standard
|
CAEP/6
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gptkbp:engine
|
gptkb:Trent_family
advanced materials
state-of-the-art technology
global support network
bleed air start
developed for Airbus A350 XWB
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|
gptkbp:engine_availability
|
high availability
|
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gptkbp:engine_power
|
high reliability
optimized for long-haul flights
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
Trent XWB-84, Trent XWB-97
|
|
gptkbp:fuel_capacity
|
2.7 m
3.1 m
1,500 kg
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:has_historical_building
|
Trent 900
|
|
gptkbp:high_pressure_compressor
|
9 stages
|
|
gptkbp:high_pressure_turbine
|
2 stages
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Trent XWB engine
|
|
gptkbp:length
|
3.1 m
|
|
gptkbp:low_pressure_compressor
|
3 stages
|
|
gptkbp:low_pressure_turbine
|
2 stages
|
|
gptkbp:maintenance
|
6,000 hours
on-wing maintenance possible
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
-54 to 50 ° C
|
|
gptkbp:original_run
|
gptkb:2011
|
|
gptkbp:propulsion
|
84,000 lbf
|
|
gptkbp:service_entry
|
gptkb:2014
|
|
gptkbp:total_deliveries
|
gptkb:1,000
|
|
gptkbp:total_orders
|
1,600
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Group_plc
gptkb:Rolls-Royce_Defence
|
|
gptkbp:bfsLayer
|
5
|