GE90-100 B1

GPTKB entity

Statements (58)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:Boeing_707
gptkbp:armament gptkb:textiles
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:customer_support gptkb:British_Airways
gptkbp:diameter 3.0 m
3.3 ft
gptkbp:emissions_standard CAEP/6
gptkbp:engine gptkb:Evendale,_Ohio
advanced aerodynamics
state-of-the-art technology
bleed air start
widely used in aviation.
gptkbp:engine_configuration wing-mounted
gptkbp:engine_control_software advanced control algorithms
gptkbp:engine_cooling_technology advanced cooling techniques
gptkbp:engine_development_time 10 years
gptkbp:engine_fan_blade_count gptkb:22
gptkbp:engine_fan_design wide chord fan blades
gptkbp:engine_power high reliability
excellent performance
gptkbp:engine_research_investment over $1 billion
gptkbp:engine_test_flights extensive test flights
gptkbp:engine_turbine_blades single crystal alloy
gptkbp:engine_turbine_design high-efficiency turbine
gptkbp:engine_type gptkb:Boeing_777-200_LR
gptkb:GE90-115_B
high-thrust turbofan
gptkbp:engine_variant_count multiple variants
gptkbp:first_flight gptkb:1995
gptkbp:fuel_economy high efficiency
0.5 lb/lbf/hr
gptkbp:fuel_type gptkb:Jet_A-1
dual-channel fuel system
gptkbp:gearbox reduction gearbox
https://www.w3.org/2000/01/rdf-schema#label GE90-100 B1
gptkbp:ignition_system dual ignition system
gptkbp:is_tested_for gptkb:Peebles,_Ohio
gptkbp:length 11.5 ft
gptkbp:maintenance 10,000 hours
low maintenance cost
gptkbp:manufacturer gptkb:General_Electric
gptkbp:max_takeoff_weight 775,000 lb
gptkbp:noise_level Stage 4 compliant
gptkbp:number_of_engines over 1,600
gptkbp:number_of_stages gptkb:10
gptkbp:propulsion 115,300 lbf
gptkbp:service_entry gptkb:1995
gptkbp:turbine_type high bypass turbofan
gptkbp:weight 8,000 lb
gptkbp:bfsParent gptkb:GE90-115_B1
gptkb:GE90-115_B13
gptkb:GE90-115_B4
gptkbp:bfsLayer 5