|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
gptkb:Boeing_767
gptkb:Airbus_A300
McDonnell Douglas MD-11
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:climate
|
1,500 °F
|
|
gptkbp:compressionRatio
|
5.5:1
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:criticalReception
|
40 psi
|
|
gptkbp:design
|
20,000 hours
|
|
gptkbp:diameter
|
3.0 ft
2.9 ft
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
CAEP/6
|
|
gptkbp:engine
|
2
|
|
gptkbp:engineConfiguration
|
twin_spool
|
|
gptkbp:engineType
|
gptkb:CF6-80C2B1F10
gptkb:CF6-80C2B1F4
gptkb:CF6-80C2B1F16
gptkb:CF6-80C2B1F13
gptkb:CF6-80C2B1F12
gptkb:CF6-80C2B1F3
gptkb:CF6-80C2B1F14
gptkb:CF6-80C2B1F18
gptkb:CF6-80C2B1F6
gptkb:CF6-80C2B1F1
gptkb:CF6-80C2B1F5
gptkb:CF6-80C2B1F8
axial
high bypass ratio
CF6-80C2B1F11
CF6-80C2B1F15
CF6-80C2B1F17
CF6-80C2B1F2
CF6-80C2B1F7
CF6-80C2B1F9
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
1,200 lb/hr
|
|
gptkbp:fuelType
|
Jet A
dual ignition
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80C2B1F19
|
|
gptkbp:launched
|
air starter
|
|
gptkbp:length
|
11.5 ft
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Chapter_4
|
|
gptkbp:number_of_stages
|
9
|
|
gptkbp:propulsion
|
18,500 lbf
4.6:1
|
|
gptkbp:related_engine
|
gptkb:CF6_family
|
|
gptkbp:serviceType
|
1982
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
4,000 lb
|