|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Boeing_707
|
|
gptkbp:armament
|
gptkb:22
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
123 in
3.3 ft
|
|
gptkbp:elevation
|
43,000 ft
|
|
gptkbp:engine
|
gptkb:Evendale,_Ohio
advanced materials
high bypass ratio
bleed air
part of GE90 family
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_customer_base
|
global airlines
|
|
gptkbp:engine_design_innovation
|
state-of-the-art design
|
|
gptkbp:engine_fan_blade_material
|
composite
|
|
gptkbp:engine_fan_type
|
wide chord fan
|
|
gptkbp:engine_gearbox_type
|
reduction gearbox
|
|
gptkbp:engine_market_share
|
dominant market share
|
|
gptkbp:engine_power
|
high reliability
20,000 hours
high thrust output
|
|
gptkbp:engine_support_network
|
extensive support network
|
|
gptkbp:engine_technology_leadership
|
industry leader
|
|
gptkbp:engine_thermal_efficiency
|
high thermal efficiency
|
|
gptkbp:engine_turbine_blade_material
|
single crystal superalloy
|
|
gptkbp:engine_type
|
gptkb:Boeing_777-200_LR
gptkb:GE90-110_B
turbofan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
3.5 m
1.0 m
3,600 kg
high fuel capacity
|
|
gptkbp:fuel_economy
|
high efficiency
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-110 B4
|
|
gptkbp:is_tested_for
|
gptkb:Peebles,_Ohio
|
|
gptkbp:length
|
11.5 ft
|
|
gptkbp:maintenance
|
6,000 hours
low maintenance cost
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 4 compliant
advanced design
|
|
gptkbp:number_of_engines
|
over 1,600
|
|
gptkbp:propulsion
|
110,000 lbf
29.4:1
|
|
gptkbp:service_entry
|
gptkb:1995
|
|
gptkbp:successor
|
gptkb:GE90-115_B
|
|
gptkbp:turbine_type
|
high bypass turbofan
|
|
gptkbp:weight
|
8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:GE90-110_B
|
|
gptkbp:bfsLayer
|
6
|