Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
business jet
|
| gptkbp:bypassRatio |
5.6:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:combustorType |
single annular combustor
|
| gptkbp:compressionRatio |
10-stage high-pressure axial compressor
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:fanBlades |
18 composite blades
|
| gptkbp:firstRun |
2013
|
| gptkbp:fuelType |
improved over previous generation engines
|
| https://www.w3.org/2000/01/rdf-schema#label |
GE Passport
|
| gptkbp:length |
86 inches
|
| gptkbp:mainRotorDiameter |
52 inches
|
| gptkbp:manufacturer |
gptkb:GE_Aviation
|
| gptkbp:marketEntry |
2018
|
| gptkbp:noiseCompliance |
Stage 4 ICAO
|
| gptkbp:technology |
derived from GE90/CF34/LEAP
|
| gptkbp:thrust |
16,500 lbf
|
| gptkbp:turbineType |
2-stage high-pressure turbine
4-stage low-pressure turbine |
| gptkbp:usedIn |
gptkb:Bombardier_Global_7500
|
| gptkbp:weight |
2,920 lb
|
| gptkbp:bfsParent |
gptkb:Global_7500
gptkb:Global_8000 |
| gptkbp:bfsLayer |
7
|