Honeywell TFE731-40BR turbofan
GPTKB entity
Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_50EX
|
| gptkbp:bypassRatio |
2.8:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
two-spool
|
| gptkbp:diameter |
34.2 in
|
| gptkbp:family |
gptkb:TFE731
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasTower |
two-stage low pressure, one-stage high pressure
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell TFE731-40BR turbofan
|
| gptkbp:introducedIn |
1995
|
| gptkbp:length |
72.6 in
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
|
| gptkbp:market |
business jet
|
| gptkbp:thrust |
4200 lbf
|
| gptkbp:weight |
950 lb
|
| gptkbp:bfsParent |
gptkb:Bombardier_Learjet_75
|
| gptkbp:bfsLayer |
7
|