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gptkbp:instance_of
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gptkb:engine
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|
gptkbp:bfsLayer
|
4
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|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Trent_800
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|
gptkbp:aircraft_operated
|
wide-body aircraft
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:armament
|
composite
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|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:certification
|
EASA and FAA certified
|
|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
2.9 m
2.7 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:Trent_family
advanced aerodynamics
twin-spool
high bypass ratio
global support network
bleed air start
available for older models
pylon-mounted
2 per aircraft
proven track record
noise reduction technology
optimized for long-haul flights
up to 20,000 hours
|
|
gptkbp:engine_type
|
gptkb:Trent_800
turbofan
axial
high-pressure and low-pressure
nickel alloy
compatible with Boeing 777-200 and 777-300.
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_capacity
|
2.7 m
3.5 m
4,000 kg
0.5 lb/hp/hr
improved over previous models
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Trent 800 R
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
modular design
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:material
|
titanium
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:number_of_stages
|
gptkb:6
|
|
gptkbp:operational_area
|
high
|
|
gptkbp:produced_by
|
over 1,000 engines
|
|
gptkbp:propulsion
|
gptkb:battle
up to 85,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
gptkb:1995
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
4,000 kg
|