Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:regional_airliner
|
| gptkbp:bypassRatio |
5.0:1
|
| gptkbp:compressor_stages |
1 fan, 4 axial, 1 centrifugal
|
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:family |
gptkb:General_Electric_CF34
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:introduced |
1999
|
| gptkbp:length |
2.5 m
|
| gptkbp:mainRotorDiameter |
132 cm
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:thrust |
13,790 lbf
|
| gptkbp:turbine_stages |
2 low-pressure, 1 high-pressure
|
| gptkbp:usedInAircraft |
gptkb:Bombardier_CRJ700
gptkb:Bombardier_CRJ900 |
| gptkbp:weight |
1,544 lb
|
| gptkbp:bfsParent |
gptkb:Bombardier_CRJ1000
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CF34-8C5A1
|