Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
commercial aviation |
| gptkbp:bypassRatio |
8.5:1
|
| gptkbp:certification |
2018
|
| gptkbp:contrastsWith |
gptkb:Pratt_&_Whitney_PW1000G
gptkb:CFM_International_LEAP |
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:developedBy |
gptkb:Aviadvigatel
|
| gptkbp:family |
Aviadvigatel PD family
|
| gptkbp:firstFlight |
2015
|
| gptkbp:fuelType |
15% better than PS-90A
|
| gptkbp:hasConcept |
new core design
|
| https://www.w3.org/2000/01/rdf-schema#label |
PD-14
|
| gptkbp:intendedAircraft |
gptkb:Irkut_MC-21
|
| gptkbp:length |
4.9 m
|
| gptkbp:mainRotorDiameter |
1.9 m
|
| gptkbp:manufacturer |
gptkb:United_Engine_Corporation
|
| gptkbp:notableFeature |
first all-new Russian civil turbofan since Soviet era
|
| gptkbp:status |
in production
|
| gptkbp:thrust |
14000 kgf
|
| gptkbp:variant |
PD-14A
PD-14M PD-14P |
| gptkbp:weight |
2850 kg
|
| gptkbp:bfsParent |
gptkb:Aviadvigatel_PS-90A_turbofan
|
| gptkbp:bfsLayer |
6
|