|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Boeing_707
|
|
gptkbp:armament
|
22 blades
|
|
gptkbp:average_temperature
|
high temperature
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:certification
|
gptkb:FAA
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
123 inches
3.1 ft
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
advanced materials
state-of-the-art technology
modular
air start
|
|
gptkbp:engine_configuration
|
high efficiency
wing-mounted
two per aircraft
|
|
gptkbp:engine_power
|
high performance
high reliability
|
|
gptkbp:engine_type
|
gptkb:Boeing_777-200_LR
gptkb:Boeing_777_F
gptkb:Boeing_777-300_ER
turbofan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
3.5 m
3,600 kg
0.79 m
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-5 B
|
|
gptkbp:introduced
|
gptkb:1995
|
|
gptkbp:length
|
11.5 ft
|
|
gptkbp:maintenance
|
scheduled maintenance
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:maximum_power
|
115,300 lbf
|
|
gptkbp:noise_level
|
Stage 4 compliant
advanced design
|
|
gptkbp:number_of_stages
|
gptkb:9
|
|
gptkbp:number_of_turbine_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
long-haul
|
|
gptkbp:propulsion
|
115,300 lbf
14.4:1
|
|
gptkbp:related_aircraft
|
gptkb:Boeing_777_family
|
|
gptkbp:successor
|
gptkb:GE90-115_B
|
|
gptkbp:turbine_type
|
axial
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:GE90
|
|
gptkbp:bfsLayer
|
5
|