Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
0.59
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.905 m
|
| gptkbp:firstFlight |
1976
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
AL-31 turbofan
|
| gptkbp:length |
4.95 m
|
| gptkbp:manufacturer |
gptkb:NPO_Saturn
gptkb:Lyulka |
| gptkbp:notableVariant |
gptkb:AL-31F
gptkb:AL-31FM2 gptkb:AL-31FN AL-31FP AL-31FM1 AL-31FM3 |
| gptkbp:numberOfStages |
1-stage high-pressure, 1-stage low-pressure
4-stage low-pressure, 9-stage high-pressure |
| gptkbp:originatedIn |
engine for Su-27
|
| gptkbp:relatedTo |
gptkb:WS-10
AL-41F |
| gptkbp:status |
in production
|
| gptkbp:thrust |
122.6 kN with afterburner
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Chengdu_J-10
gptkb:Sukhoi_Su-27 gptkb:Sukhoi_Su-30 gptkb:Sukhoi_Su-35 gptkb:Sukhoi_Su-34 |
| gptkbp:weight |
1520 kg
|
| gptkbp:bfsParent |
gptkb:Lyulka_design_bureau
|
| gptkbp:bfsLayer |
7
|