General Electric CF34-10E turbofan
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
regional airliner
|
| gptkbp:bypassRatio |
5.4:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressor_type |
axial/centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:family |
gptkb:General_Electric_CF34
|
| gptkbp:firstRun |
2000s
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CF34-10E turbofan
|
| gptkbp:length |
120 inches
|
| gptkbp:mainRotorDiameter |
52 inches
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:number_of_fan_blades |
24
|
| gptkbp:number_of_stages_(high-pressure_turbine) |
2
|
| gptkbp:number_of_stages_(low-pressure_turbine) |
4
|
| gptkbp:thrust |
18,500 lbf
|
| gptkbp:usedInAircraft |
gptkb:Embraer_E195
gptkb:Embraer_E190 |
| gptkbp:weight |
2,627 lb
|
| gptkbp:bfsParent |
gptkb:E190
gptkb:Embraer_ERJ_190 |
| gptkbp:bfsLayer |
7
|