Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
military and civilian aircraft
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:configuration |
V engine
|
| gptkbp:cooling_system |
liquid-cooled
water-cooled |
| gptkbp:displacement |
27.0 liters
|
| gptkbp:engine |
no
|
| gptkbp:engine_configuration |
gptkb:V12
longitudinal |
| gptkbp:engine_type |
reciprocating engine
|
| gptkbp:first_introduced |
1920s
|
| gptkbp:fuel_capacity |
wet sump
|
| gptkbp:fuel_type |
gptkb:carburetor
aviation gasoline |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 230 HP
|
| gptkbp:ignition_system |
magneto ignition
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notable_users |
gptkb:Avro_504_K
|
| gptkbp:powers |
230 horsepower
|
| gptkbp:production_years |
1920s to 1930s
|
| gptkbp:successor |
gptkb:Rolls-Royce_Kestrel
|
| gptkbp:type |
gptkb:V8_engine
|
| gptkbp:used_in |
various aircraft
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
approximately 300 kg
|
| gptkbp:bfsParent |
gptkb:Sir_Henry_Royce
|
| gptkbp:bfsLayer |
5
|