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gptkbp:instanceOf
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turbofan engine
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gptkbp:application
|
commercial aviation
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gptkbp:certifications
|
gptkb:FAA
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gptkbp:climate
|
1,600 °F
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gptkbp:compressionRatio
|
5.5:1
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gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
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gptkbp:customerService
|
gptkb:United_Airlines
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gptkbp:diameter
|
68 in
60 in
|
|
gptkbp:emissionsStandard
|
NOx compliant
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gptkbp:engineConfiguration
|
twin_spool
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gptkbp:engineType
|
gptkb:CF6-80C2B1F27
gptkb:CF6-80C2B1F28
gptkb:CF6-80C2B1F24
gptkb:CF6-80C2B1F29
gptkb:CF6-80C2B1F
gptkb:CF6-80C2B1F32
gptkb:CF6-80C2B1F34
gptkb:CF6-80E1
gptkb:CF6-80C2
gptkb:CF6-80C2B1F35
gptkb:CF6-80C2B1F40
gptkb:CF6-80C2B1F25
gptkb:CF6-80C2B1F26
gptkb:CF6-80C2B1F33
gptkb:CF6-80C2B1F37
axial
high bypass
dual rotor
CF6-80C2B1F22
CF6-80C2B1F30
CF6-80C2B1F31
CF6-80C2B1F36
CF6-80C2B1F38
CF6-80C2B1F39
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
|
|
gptkbp:fuelType
|
Jet A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80C2B1F23
|
|
gptkbp:length
|
156 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notableUsers
|
gptkb:Airbus_A330
gptkb:Boeing_767
|
|
gptkbp:number_of_stages
|
2 stages
6 stages
9 stages
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:propulsion
|
18,500 lbf
20,000 lbf
|
|
gptkbp:related_engine
|
gptkb:CF6_family
|
|
gptkbp:serviceType
|
1982
|
|
gptkbp:weight
|
4,000 lb
|