|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:aircraft_type
|
wide-body aircraft
|
|
gptkbp:application
|
gptkb:Boeing_707
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:9
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
gptkb:British_Airways
|
|
gptkbp:diameter
|
123 inches
3.1 ft
|
|
gptkbp:engine
|
gptkb:Evendale,_Ohio
advanced materials
bleed air start
|
|
gptkbp:engine_configuration
|
twin-engine
2 per aircraft
|
|
gptkbp:engine_power
|
high reliability
high efficiency
|
|
gptkbp:engine_type
|
gptkb:Boeing_777-200_LR
gptkb:Boeing_777_F
gptkb:Boeing_777_X
gptkb:Boeing_777-300_ER
turbofan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-115 B6
|
|
gptkbp:introduced
|
gptkb:2002
|
|
gptkbp:is_tested_for
|
gptkb:Peebles,_Ohio
|
|
gptkbp:length
|
12.5 ft
|
|
gptkbp:maintenance
|
10,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 4 compliant
advanced design
|
|
gptkbp:notable_feature
|
largest fan diameter of any commercial jet engine
|
|
gptkbp:number_of_engines
|
over 1,600
|
|
gptkbp:operational_range
|
up to 8,000 nautical miles
|
|
gptkbp:propulsion
|
115,300 lbf
|
|
gptkbp:successor
|
gptkb:GE9_X
|
|
gptkbp:turbine_type
|
gptkb:3
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:GE90_engine
|
|
gptkbp:bfsLayer
|
4
|