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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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gptkb:Boeing_707
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gptkbp:certification
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FAA certified
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gptkbp:compressor_type
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axial compressor
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gptkbp:control_system
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gptkb:FADEC
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gptkbp:cooling_system
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air-cooled
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gptkbp:diameter
|
3.0 ft
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gptkbp:emissions_standard
|
CAEP/6
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gptkbp:engine
|
modular design
advanced materials
bleed air start
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gptkbp:engine_configuration
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twin-spool
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gptkbp:engine_inlet
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nacelle-mounted
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gptkbp:engine_power
|
high thrust-to-weight ratio
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gptkbp:engine_type
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gptkb:GE90-110_B1
gptkb:GE90-115_B
gptkb:GE90-94_B
gptkb:GE90-100_B1
gptkb:GE90-130_B1
gptkb:GE90-140_B1
gptkb:GE90-150_B1
gptkb:GE90-160_B1
gptkb:GE90-170_B1
gptkb:GE90-180_B1
gptkb:GE90-190_B1
gptkb:GE90-200_B1
gptkb:GE90-210_B1
gptkb:GE90-220_B1
gptkb:GE90-230_B1
gptkb:GE90-240_B1
gptkb:GE90-250_B1
gptkb:GE90-260_B1
gptkb:GE90-120_B1
turbofan
GE90-270 B1
GE90-280 B1
GE90-290 B1
GE90-300 B1
GE90-310 B1
GE90-320 B1
GE90-330 B1
GE90-340 B1
GE90-350 B1
GE90-360 B1
GE90-370 B1
GE90-380 B1
GE90-390 B1
GE90-400 B1
GE90-410 B1
GE90-420 B1
GE90-430 B1
GE90-440 B1
GE90-450 B1
GE90-460 B1
GE90-470 B1
GE90-480 B1
GE90-490 B1
GE90-500 B1
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|
gptkbp:exhaust_system
|
convergent nozzle
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
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gptkbp:fuel_type
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gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE90-1110 B1
|
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gptkbp:is_tested_for
|
static test
|
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gptkbp:length
|
11.5 ft
|
|
gptkbp:maintenance
|
on-wing maintenance
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gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
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gptkbp:number_of_stages
|
gptkb:10
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|
gptkbp:operational_range
|
0 to 40,000 ft
|
|
gptkbp:original_run
|
gptkb:1995
|
|
gptkbp:propulsion
|
110,000 lbf
|
|
gptkbp:successor
|
gptkb:GE90-115_B
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|
gptkbp:turbine_type
|
high-pressure turbine
|
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gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
8,000 lb
|
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gptkbp:bfsParent
|
gptkb:GE90-115_B1
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gptkbp:bfsLayer
|
5
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