|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Boeing_707
|
|
gptkbp:armament
|
gptkb:22
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:certification
|
gptkb:EASA
gptkb:FAA
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
2.9 m
3.25 m
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:civil_aviation
gptkb:GE90_family
advanced materials
state-of-the-art technology
ongoing development
bleed air
|
|
gptkbp:engine_configuration
|
gptkb:1
wing-mounted
|
|
gptkbp:engine_legacy_system
|
gptkb:GE90_series
|
|
gptkbp:engine_power
|
high performance
high reliability
|
|
gptkbp:engine_technology_investment
|
significant investment
|
|
gptkbp:engine_type
|
gptkb:Boeing_777-200_LR
gptkb:GE90-115_B
high-bypass turbofan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
3.5 m
8,000 lb
3.25 m
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-2 B16
|
|
gptkbp:impact
|
fuel savings
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
scheduled maintenance
10,000 hours
low maintenance cost
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_operating_temperature
|
1,500 ° C
|
|
gptkbp:noise_level
|
low
advanced design
|
|
gptkbp:operational_range
|
long-haul
|
|
gptkbp:propulsion
|
115,300 lbf
14.4:1
|
|
gptkbp:revenue_service
|
gptkb:1996
|
|
gptkbp:service_entry
|
gptkb:1995
|
|
gptkbp:turbine_type
|
high-pressure and low-pressure
|
|
gptkbp:weight
|
8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:GE90-2_B
|
|
gptkbp:bfsLayer
|
6
|