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gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Boeing_707
|
|
gptkbp:armament
|
composite
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
gptkb:United_Airlines
|
|
gptkbp:diameter
|
2.9 m
3.25 m
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:Evendale,_Ohio
gptkb:GE90_family
next-generation engine technology
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_nozzle_type
|
variable area nozzle
|
|
gptkbp:engine_power
|
high
efficient
20,000 hours
|
|
gptkbp:engine_testbed
|
gptkb:Boeing
|
|
gptkbp:engine_type
|
gptkb:Boeing_777-200_LR
gptkb:GE90-115_B
high-bypass turbofan
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
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
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-40 B
|
|
gptkbp:innovation
|
advanced materials
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
low
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:maximum_power_output
|
40,000 lbf
|
|
gptkbp:noise_level
|
gptkb:Stage_4
advanced design
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:operational_range
|
long-haul
|
|
gptkbp:produces
|
over 1,500 engines
|
|
gptkbp:propulsion
|
5:1
40,000 lbf
|
|
gptkbp:service_entry
|
gptkb:1995
|
|
gptkbp:turbine_type
|
gptkb:Super_GT
high-pressure turbine
|
|
gptkbp:weight
|
8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:GE90
|
|
gptkbp:bfsLayer
|
5
|