|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Boeing_707
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
gptkb:British_Airways
|
|
gptkbp:diameter
|
123 inches
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:Evendale,_Ohio
gptkb:GE90
gptkb:GE90_family
advanced materials
state-of-the-art
bleed air
|
|
gptkbp:engine_configuration
|
gptkb:GE90-115_B4_T
|
|
gptkbp:engine_power
|
high
excellent
|
|
gptkbp:engine_technology_leader
|
gptkb:General_Electric
|
|
gptkbp:engine_type
|
gptkb:Boeing_777-200_LR
turbofan
|
|
gptkbp:engine_weight_to_thrust_ratio
|
0.069 lb/lbf
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
11.5 ft
3.5 ft
|
|
gptkbp:fuel_economy
|
high
0.8 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-115 B4 T
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:impact
|
global aviation
|
|
gptkbp:is_tested_for
|
gptkb:Peebles,_Ohio
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:number_of_stages
|
gptkb:9
|
|
gptkbp:propulsion
|
115,300 lbf
|
|
gptkbp:turbine_type
|
axial
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:GE90-115_B4
|
|
gptkbp:bfsLayer
|
5
|