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gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Boeing_707
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
bypass air
|
|
gptkbp:diameter
|
123 inches
3.25 ft
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:Evendale,_Ohio
modular design
advanced materials
state-of-the-art technology
air start
widely used in long-haul flights
|
|
gptkbp:engine_dimensions
|
3.25 ft diameter, 12.5 ft length
|
|
gptkbp:engine_maintenance_provider
|
gptkb:GE_Aviation
|
|
gptkbp:engine_power
|
high performance
high reliability
30,000 hours
|
|
gptkbp:engine_repair_facility
|
gptkb:Singapore
|
|
gptkbp:engine_test_date
|
gptkb:1995
|
|
gptkbp:engine_type
|
gptkb:Boeing_777-200_LR
gptkb:GE90-110_B1
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
3,600 kg
|
|
gptkbp:fuel_economy
|
high efficiency
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-115 B14
|
|
gptkbp:is_tested_for
|
gptkb:Peebles,_Ohio
|
|
gptkbp:length
|
12.5 ft
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 0.84
|
|
gptkbp:noise_level
|
gptkb:advanced_technology
Stage 4 compliant
|
|
gptkbp:number_of_stages
|
10 stages
|
|
gptkbp:propulsion
|
115,300 lbf
14.4:1
|
|
gptkbp:service_entry
|
gptkb:1995
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:GE90_engine
|
|
gptkbp:bfsLayer
|
4
|