Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional jets
|
| gptkbp:average_temperature |
high
|
| gptkbp:bypass_ratio |
8:1
|
| gptkbp:cancellation_reason |
yes
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
gptkb:6
|
| gptkbp:configuration |
twin-spool
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:development |
gptkb:GTF_engine_family
|
| gptkbp:diameter |
1,600 mm
1,500 mm |
| gptkbp:emissions_standard |
CAEP/6
|
| gptkbp:first_flight |
gptkb:2013
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| gptkbp:gearbox |
reduction gearbox
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW1200 G-11
|
| gptkbp:length |
1,800 mm
|
| gptkbp:maintenance |
5,000 hours
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:propulsion |
18,000 lbf
|
| gptkbp:service_entry |
gptkb:2016
|
| gptkbp:turbine_type |
2
|
| gptkbp:type |
geared turbofan
|
| gptkbp:used_in |
gptkb:Bombardier_CSeries
|
| gptkbp:weight |
3,600 lb
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_PW1200_G
|
| gptkbp:bfsLayer |
6
|