|
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
|
gptkb:FAA
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
gptkb:British_Airways
|
|
gptkbp:diameter
|
123 in
98 in
|
|
gptkbp:engine
|
low emissions
advanced aerodynamics
high durability
modular design
real-time data analysis
advanced materials
computer-aided design
noise reduction technologies
environmentally friendly design
advanced cooling techniques
high bypass ratio
high thrust-to-weight ratio
advanced testing methods
composite fan blades
fuel efficiency improvements
digital engine control
bleed air
engine monitoring systems
state-of-the-art manufacturing
high performance materials
|
|
gptkbp:engine_configuration
|
gptkb:GE90-110_B1_B-1
twin-engine
pylon-mounted
|
|
gptkbp:engine_power
|
high reliability
high efficiency
|
|
gptkbp:engine_type
|
gptkb:Boeing_777-200_LR
gptkb:Boeing_777_F
gptkb:GE90-110_B1
gptkb:Boeing_777_X
gptkb:Boeing_777-300_ER
high-thrust turbofan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-110 B1 B
|
|
gptkbp:length
|
102 in
|
|
gptkbp:maintenance
|
10,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 4 compliant
advanced design
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:propulsion
|
110,000 lbf
|
|
gptkbp:turbine_type
|
high bypass
|
|
gptkbp:weight
|
8,000 lb
|
|
gptkbp:bfsParent
|
gptkb:GE90-115_B13
|
|
gptkbp:bfsLayer
|
5
|