|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Boeing_707
|
|
gptkbp:armament
|
gptkb:22
|
|
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:design
|
30,000 hours
|
|
gptkbp:development_cost
|
high
|
|
gptkbp:diameter
|
2.9 m
3.25 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:GE90
gptkb:GE90_series
yes
advanced materials
modular
air start
|
|
gptkbp:engine_configuration
|
gptkb:1
minimal
wing-mounted
|
|
gptkbp:engine_legacy_systems
|
compatible
|
|
gptkbp:engine_power
|
optimized
|
|
gptkbp:engine_repair_time
|
short
|
|
gptkbp:engine_type
|
gptkb:GE90-130_B1_B
gptkb:Boeing_777-200_LR
high-bypass turbofan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
integrated
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-130 B1
|
|
gptkbp:impact
|
fuel savings
|
|
gptkbp:is_tested_for
|
gptkb:Peebles,_Ohio
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
low
long
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market_share
|
dominant
|
|
gptkbp:max_operating_temperature
|
1,500 ° C
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_use
|
commercial aviation
|
|
gptkbp:propulsion
|
no
130,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:1995
|
|
gptkbp:successor
|
gptkb:GE90-115_B
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:weight
|
lightweight
8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:GE90-115_B1
gptkb:GE90-130_B
|
|
gptkbp:bfsLayer
|
5
|