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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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commercial aviation
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|
gptkbp:armament
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gptkb:textiles
|
|
gptkbp:cancellation_reason
|
advanced noise reduction technology
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|
gptkbp:certification
|
CAEP/6
EASA and FAA certified
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gptkbp:competitors
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gptkb:General_Electric_GEnx
gptkb:Pratt_&_Whitney_PW1000_G
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gptkbp:compressor_type
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gptkb:10
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gptkbp:control_system
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gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
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gptkbp:cooling_system
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air-cooled
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gptkbp:design
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gptkb:Rolls-Royce
|
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gptkbp:development
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gptkb:Rolls-Royce_Trent_900
|
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gptkbp:diameter
|
2.68 m
|
|
gptkbp:engine
|
gptkb:Boeing_787-9
gptkb:Boeing_787-8
gptkb:Trent_family
gptkb:Boeing_787-10
|
|
gptkbp:engine_configuration
|
twin-spool
high bypass ratio
up to 74,000 lbf
|
|
gptkbp:engine_type
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gptkb:Trent_1000-Engine_Alliance
gptkb:Trent_1000-TEN
turbofan
|
|
gptkbp:first_flight
|
gptkb:2011
|
|
gptkbp:fuel_capacity
|
4,000 kg
3.4 m
2.68 m
|
|
gptkbp:fuel_economy
|
high fuel efficiency
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Trent 1000
|
|
gptkbp:is_used_in
|
gptkb:Boeing_787
|
|
gptkbp:length
|
3.4 m
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Ford_Motor_Company
|
|
gptkbp:noise_level
|
Chapter 4
|
|
gptkbp:operational_cost
|
lower than previous models
|
|
gptkbp:propulsion
|
240,000 lbf
up to 74,000 lbf
|
|
gptkbp:service_entry
|
gptkb:2011
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:used_in
|
gptkb:Boeing_787_Dreamliner
|
|
gptkbp:variant
|
gptkb:Trent_1000-Engine_Alliance
gptkb:Trent_1000-TEN
|
|
gptkbp:weight
|
4,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Boeing_787_Dreamliner
|
|
gptkbp:bfsLayer
|
4
|