Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional jets
Airbus A318, A319, A320 |
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:design |
high bypass ratio
|
| gptkbp:diameter |
68 inches
|
| gptkbp:first_flight |
gptkb:1996
gptkb:2000 |
| gptkbp:fuel_economy |
high
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW6000
|
| gptkbp:maintenance |
5,000 hours
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:noise_level |
low
compliant with Stage 4 regulations |
| gptkbp:notable_users |
gptkb:Embraer_E-Jet_family
gptkb:Bombardier_CRJ-700 gptkb:Bombardier_CRJ-900 |
| gptkbp:propulsion |
15,000 to 20,000 lbf
20,000 to 30,000 lbf |
| gptkbp:successor |
PW6100
|
| gptkbp:turbine_type |
high-pressure turbine
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:weight |
approximately 3,000 lb
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_engines
|
| gptkbp:bfsLayer |
7
|