Statements (27)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:application |
commercial aviation
|
gptkbp:bypassRatio |
8.5:1
|
gptkbp:certification |
gptkb:Russian_Federal_Air_Transport_Agency
2018 |
gptkbp:countryOfOrigin |
gptkb:Russia
|
gptkbp:developedBy |
gptkb:United_Engine_Corporation
|
gptkbp:diameter |
1.9 m
|
gptkbp:family |
gptkb:PD-14_engine_family
|
gptkbp:firstFlight |
2015
|
gptkbp:firstRun |
2012
|
gptkbp:fuelType |
aviation kerosene
|
gptkbp:hasConcept |
two-spool
|
https://www.w3.org/2000/01/rdf-schema#label |
Aviadvigatel PD-14
|
gptkbp:intendedAircraft |
gptkb:Irkut_MC-21
|
gptkbp:length |
4.9 m
|
gptkbp:mainRotorDiameter |
1.9 m
|
gptkbp:manufacturer |
gptkb:Aviadvigatel
|
gptkbp:marketedAs |
narrow-body airliners
|
gptkbp:notableFeature |
first all-new Russian commercial turbofan since Soviet era
|
gptkbp:numberOfStages |
8
|
gptkbp:status |
in production
|
gptkbp:successor |
gptkb:PS-90A
|
gptkbp:thrust |
14000 kgf
|
gptkbp:usedOn |
gptkb:Irkut_MC-21
|
gptkbp:bfsParent |
gptkb:Irkut_MC-21
|
gptkbp:bfsLayer |
5
|