gptkbp:instance_of
|
gptkb:engine
|
gptkbp:bfsLayer
|
4
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Trent_800
|
gptkbp:aircraft_operated
|
wide-body aircraft
|
gptkbp:armament
|
composite materials
|
gptkbp:average_temperature
|
1,600 ° C
|
gptkbp:certification
|
EASA and FAA certified
|
gptkbp:compression_ratio
|
up to 30:1
|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
gptkbp:cooling_system
|
advanced cooling technology
|
gptkbp:customer_support
|
gptkb:British_Airways
global support network
|
gptkbp:diameter
|
2.5 m
2.7 m
|
gptkbp:emissions_standard
|
CAEP/6 compliant
|
gptkbp:engine
|
gptkb:Trent_family
modular design
quiet operation
twin-spool
real-time performance monitoring
high reliability rating
up to 10,000 hours
long-haul routes
optimized for efficiency
up to 70,000 lbf
up to 20,000 hours
available for existing engines
|
gptkbp:engine_type
|
gptkb:Trent_800
gptkb:3
2
turbofan
|
gptkbp:environmental_impact
|
low emissions
|
gptkbp:features
|
advanced aerodynamics
|
gptkbp:first_flight
|
gptkb:1992
1992-08-15
|
gptkbp:fuel_capacity
|
2.7 m
3.5 m
high
4,000 kg
0.5 lb/lbf/hr
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
advanced fuel system technology
|
gptkbp:has_programs
|
Trent engine program
|
https://www.w3.org/2000/01/rdf-schema#label
|
Trent 800 V
|
gptkbp:is_tested_for
|
extensive ground testing
|
gptkbp:length
|
3.5 m
|
gptkbp:maintenance
|
6,000 hours
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
gptkbp:market_segment
|
wide-body aircraft market
|
gptkbp:noise_level
|
Chapter 4 compliant
state-of-the-art noise reduction technology
|
gptkbp:operational_area
|
commercial aviation
|
gptkbp:operational_range
|
long-haul flights
|
gptkbp:produced_by
|
over 1,000 engines
|
gptkbp:propulsion
|
high thrust-to-weight ratio
up to 70,000 lbf
|
gptkbp:reliability
|
high
|
gptkbp:service_ceiling
|
40,000 ft
|
gptkbp:successor
|
gptkb:Trent_1000
|
gptkbp:type
|
high-bypass turbofan
|
gptkbp:used_in
|
gptkb:aircraft
|
gptkbp:weight
|
4,000 kg
|