Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter_tail_rotor
|
| gptkbp:advantage |
reduced noise
improved anti-torque efficiency increased safety reduced risk of damage |
| gptkbp:alsoKnownAs |
fan-in-fin
|
| gptkbp:category |
aeronautical engineering
helicopter technology |
| gptkbp:feature |
multiple blades
enclosed tail rotor integrated into vertical fin |
| gptkbp:firstFlight |
1968
|
| gptkbp:introducedIn |
gptkb:Gazelle_helicopter
|
| gptkbp:inventedBy |
gptkb:Sud_Aviation
|
| gptkbp:usedIn |
gptkb:Eurocopter_EC135
gptkb:Eurocopter_EC145 gptkb:Eurocopter_AS365_Dauphin gptkb:Harbin_Z-9 gptkb:Eurocopter_AS565_Panther gptkb:Eurocopter_EC175 gptkb:Eurocopter_EC155 gptkb:Eurocopter_AS350_B3 gptkb:Eurocopter_H160 gptkb:Kamov_Ka-60 gptkb:Eurocopter_EC120_Colibri |
| gptkbp:bfsParent |
gptkb:Eurocopter_AS365_Dauphin
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Fenestron
|