Statements (34)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
9.0:1 to 10.5:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:competitor |
gptkb:Rolls-Royce_Trent_1000
gptkb:Rolls-Royce_Trent_XWB |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:family |
gptkb:GE90_family
|
| gptkbp:features |
reduced emissions
composite fan blades twin-annular pre-swirl combustor lower fuel consumption |
| gptkbp:firstRun |
2006
|
| gptkbp:hasConcept |
dual-spool
|
| https://www.w3.org/2000/01/rdf-schema#label |
GEnx
|
| gptkbp:mainRotorDiameter |
111 in (2.82 m)
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableOperation |
gptkb:Air_India
gptkb:Japan_Airlines gptkb:Korean_Air gptkb:Lufthansa gptkb:Qatar_Airways gptkb:United_Airlines gptkb:Ethiopian_Airlines gptkb:Nippon_Cargo_Airlines |
| gptkbp:numberOfStages |
10
2 (high-pressure), 6 (low-pressure) |
| gptkbp:successor |
gptkb:CF6
|
| gptkbp:thrust |
53,000 to 75,000 lbf
|
| gptkbp:usedIn |
gptkb:aircraft
gptkb:Boeing_747-8 |
| gptkbp:bfsParent |
gptkb:GE90-115B
gptkb:GEnx-2B67 |
| gptkbp:bfsLayer |
5
|