Rolls-Royce Eagle VIII engine
GPTKB entity
Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
7
|
| gptkbp:bfsParent |
gptkb:Supermarine_Seagull_V
|
| gptkbp:aircraft_operated |
gptkb:aircraft
|
| gptkbp:compression_ratio |
5.5:1
|
| gptkbp:cooling_system |
liquid cooling
|
| gptkbp:displacement |
27.0 L
|
| gptkbp:engine |
gptkb:V12
gptkb:Rolls-Royce_Eagle four-stroke liquid-cooled |
| gptkbp:first_flight |
1919
|
| gptkbp:fuel_type |
gptkb:product
petrol |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Eagle VIII engine
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notable_for |
Transatlantic flight
|
| gptkbp:power_output |
360 hp
|
| gptkbp:production_years |
1915-1925
|
| gptkbp:propulsion |
two-bladed propeller
|
| gptkbp:setting |
V engine
|
| gptkbp:successor |
gptkb:Rolls-Royce_Kestrel
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:Vickers_Vimy
|
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:weight |
300 kg
|