Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:Sir_Henry_Royce
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compression_ratio |
5.5:1
|
| gptkbp:cooling_system |
liquid-cooled
|
| gptkbp:displacement |
19.7 liters
|
| gptkbp:engine |
inline engine
|
| gptkbp:first_introduced |
1915
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 120 HP
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notable_users |
gptkb:Royal_Flying_Corps
|
| gptkbp:powers |
120 horsepower
|
| gptkbp:production_years |
1915-1920
|
| gptkbp:replaced_by |
gptkb:Rolls-Royce_Eagle_engine
|
| gptkbp:setting |
gptkb:V12
|
| gptkbp:successor |
gptkb:Rolls-Royce_Eagle
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:aircraft
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
approximately 300 kg
|