Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
8.5:1
|
| gptkbp:certification |
Russian certification in 2018
|
| gptkbp:constructionStartYear |
2008
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:emissionStandard |
gptkb:ICAO_CAEP/6
|
| gptkbp:exportedTo |
gptkb:Africa
gptkb:Asia gptkb:Middle_East |
| gptkbp:fanBlades |
18
|
| gptkbp:firstFlight |
2015
|
| gptkbp:fuelType |
15% better than PS-90A
|
| gptkbp:hasConcept |
high-bypass turbofan
|
| https://www.w3.org/2000/01/rdf-schema#label |
PD-14 engine
|
| gptkbp:intendedAircraft |
gptkb:Irkut_MC-21
|
| gptkbp:length |
4.9 m
|
| gptkbp:mainRotorDiameter |
1.9 m
|
| gptkbp:manufacturer |
gptkb:United_Engine_Corporation
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfStages |
2
8 |
| gptkbp:relatedTo |
gptkb:PD-10
gptkb:PD-35 PD-12V |
| gptkbp:testLocation |
gptkb:Perm,_Russia
|
| gptkbp:thrust |
14000 kgf
|
| gptkbp:usedOn |
gptkb:MC-21-300
gptkb:MC-21-310 |
| gptkbp:volume |
compliant with ICAO Chapter 4
|
| gptkbp:weight |
2850 kg
|
| gptkbp:bfsParent |
gptkb:Rostec
|
| gptkbp:bfsLayer |
5
|