|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:customerService
|
gptkb:United_Airlines
|
|
gptkbp:developer
|
gptkb:CF6_family
|
|
gptkbp:diameter
|
68 in
112 in
|
|
gptkbp:emissionsStandard
|
NOx certification
|
|
gptkbp:engine
|
modular design
|
|
gptkbp:engineConfiguration
|
twin_spool
|
|
gptkbp:engineType
|
gptkb:CF6-80C2B1F10
gptkb:CF6-80C2B1F4
gptkb:CF6-80A1
gptkb:CF6-80A2
gptkb:CF6-80C2B1F
gptkb:CF6-80C2B1F3
gptkb:CF6-80E1
gptkb:CF6-80C2
gptkb:CF6-80C2B1F6
gptkb:CF6-80C2B1F1
gptkb:CF6-80C2B1F5
gptkb:CF6-80C2B1F8
2
9
axial
high bypass ratio
1,600 °F
CF6-80C2B1F2
CF6-80C2B1F7
CF6-80C2B1F9
high pressure turbine
|
|
gptkbp:fanEvents
|
composite
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
30:1
|
|
gptkbp:fuelType
|
Jet A
|
|
gptkbp:hasArea
|
static test
flight test
EASA_certified
FAA_certified
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80A3
|
|
gptkbp:length
|
150 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notableUsers
|
gptkb:Airbus_A330
gptkb:Boeing_747
McDonnell Douglas MD-11
|
|
gptkbp:operationalRange
|
-40 to 50 °C
|
|
gptkbp:propulsion
|
60,000 lbf
cascade
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:CF6-80C2
|
|
gptkbp:weight
|
4,000 lb
|