Anzani 25 hp 3-cylinder engine
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
105 mm
|
| gptkbp:configuration |
3-cylinder
fan-type radial |
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:designer |
gptkb:Alessandro_Anzani
|
| gptkbp:displacement |
3.0 L
|
| gptkbp:firstFlight |
1909
|
| gptkbp:fuelType |
petrol
|
| gptkbp:ignition |
magneto
|
| gptkbp:manufacturer |
gptkb:Anzani
|
| gptkbp:notableEvent |
used in first flight across the English Channel
|
| gptkbp:notableFor |
gptkb:Blériot_XI
|
| gptkbp:powerOutput |
25 hp
|
| gptkbp:stroke |
120 mm
|
| gptkbp:usedIn |
early aviation
|
| gptkbp:weight |
approximately 65 kg
|
| gptkbp:bfsParent |
gptkb:Sikorsky_S-5
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Anzani 25 hp 3-cylinder engine
|