Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional jets
|
| gptkbp:compressor_type |
axial
axial compressor |
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:design |
high bypass ratio
|
| gptkbp:diameter |
2.5 ft
|
| gptkbp:fan_art |
wide-chord fan
|
| gptkbp:first_flight |
gptkb:1997
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
gptkb:Jet_A |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce AE 3007
|
| gptkbp:length |
3.5 ft
4.5 ft |
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notable_users |
gptkb:Bombardier_CRJ-900
gptkb:Embraer_ERJ-190 gptkb:Bombardier_Q400 gptkb:Embraer_ERJ_145 gptkb:Cessna_Citation_X |
| gptkbp:propulsion |
15,000 lbf
|
| gptkbp:turbine_type |
high-pressure turbine
single-stage high-pressure turbine |
| gptkbp:weight |
1,200 lb
1,500 lb |
| gptkbp:bfsParent |
gptkb:Northrop_Grumman_Global_Hawk
|
| gptkbp:bfsLayer |
4
|