Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5.0 in
|
| gptkbp:compressionRatio |
7.0:1
|
| gptkbp:configuration |
horizontally opposed
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
470 cubic inches
|
| gptkbp:engineType |
piston engine
|
| gptkbp:family |
gptkb:Continental_O-470_series
|
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental O-470-L
|
| gptkbp:ignition |
dual magneto
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:numberOfEngines |
6
|
| gptkbp:powerOutput |
230 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:stroke |
4.0 in
|
| gptkbp:usedInAircraft |
gptkb:Cessna_182
gptkb:Cessna_180 |
| gptkbp:valvetrain |
overhead valve
|
| gptkbp:weight |
393 lb
|
| gptkbp:bfsParent |
gptkb:Cessna_182
|
| gptkbp:bfsLayer |
6
|