|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:certification
|
CAEP/6
|
|
gptkbp:combustor_type
|
annular
annular combustor
|
|
gptkbp:competitors
|
gptkb:Rolls-Royce_Trent_900
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
General Electric and Pratt & Whitney
|
|
gptkbp:design_purpose
|
high reliability
|
|
gptkbp:development
|
General Electric and Pratt & Whitney
|
|
gptkbp:diameter
|
2.9 m
118 inches
|
|
gptkbp:emissions_standard
|
compliant with CAEP/6 standards
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Trent_900
|
|
gptkbp:engine_configuration
|
high bypass ratio
high bypass turbofan
|
|
gptkbp:first_flight
|
gptkb:2007
|
|
gptkbp:fuel_economy
|
lower than previous models
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Engine Alliance GP7200
|
|
gptkbp:is_used_in
|
gptkb:Airbus_A380-800_F
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
6,000 hours
longer than previous engines
|
|
gptkbp:manufacturer
|
gptkb:Engine_Alliance
|
|
gptkbp:noise_level
|
gptkb:Stage_4
meets Stage 4 noise regulations
|
|
gptkbp:number_of_engines
|
over 1,000
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:operational_range
|
long-haul flights
|
|
gptkbp:operational_use
|
commercial aviation
|
|
gptkbp:produced_by
|
gptkb:Engine_Alliance
|
|
gptkbp:produces
|
over 1,000
|
|
gptkbp:propulsion
|
70,000 to 115,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Airbus_A380-800
|
|
gptkbp:service_entry
|
gptkb:2008
|
|
gptkbp:type
|
gptkb:turbofan_engine
twin-spool
twin-spool engine
|
|
gptkbp:used_by
|
gptkb:Airbus
|
|
gptkbp:weight
|
4,000 kg
approximately 8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Airbus
|
|
gptkbp:bfsLayer
|
4
|