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gptkbp:instanceOf
|
turbofan engine
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gptkbp:application
|
commercial aviation
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gptkbp:certifications
|
gptkb:FAA
|
|
gptkbp:compressionRatio
|
5.5:1
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|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
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gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
20,000 hours
|
|
gptkbp:diameter
|
1.73 m
68 in
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
CAEP/6
|
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gptkbp:engine
|
1.73 m
modular
3.94 m
|
|
gptkbp:engineConfiguration
|
dual spool
|
|
gptkbp:engineType
|
gptkb:CF6-80C2B1F10
gptkb:CF6-80C2B1F4
gptkb:CF6-80C2A1
gptkb:CF6-80C2B1F3
gptkb:CF6-80C2B1F6
gptkb:CF6-80C2B1F1
gptkb:CF6-80C2B1F5
gptkb:CF6-80C2B1F8
turbofan
axial
1,600 °F
CF6-80C2B1F2
CF6-80C2B1F7
CF6-80C2B1F9
|
|
gptkbp:fanEvents
|
composite
superalloy
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
gptkbp:hasArea
|
static and flight testing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80C2B1F26
|
|
gptkbp:length
|
155 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Chapter_4
|
|
gptkbp:notableUsers
|
gptkb:Airbus_A330
gptkb:Boeing_767
McDonnell Douglas MD-11
|
|
gptkbp:number_of_stages
|
compressor: 10
fan: 3
turbine: 2
|
|
gptkbp:propulsion
|
18,500 lbf
4.63
|
|
gptkbp:related_engine
|
CF6
|
|
gptkbp:serviceType
|
1982
|
|
gptkbp:weight
|
4,000 lb
|