Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bore |
5.5 inches
|
| gptkbp:compression_ratio |
6:1
|
| gptkbp:controls |
mechanical
|
| gptkbp:cooling_system |
liquid-cooled
water-cooled |
| gptkbp:displacement |
27 liters
|
| gptkbp:engine |
gptkb:battle
aluminum commercial aviation V engine high reliability high power-to-weight ratio naturally aspirated longitudinal popular among collectors detailed specifications available advanced engineering for its time limited production run available in vintage markets renowned for performance technical manuals available enthusiast community active influenced future aircraft engines used in WWII aircraft classic British design |
| gptkbp:engine_type |
reciprocating engine
multiple variants produced |
| gptkbp:first_introduced |
1930s
|
| gptkbp:fuel_type |
aviation gasoline
carbureted |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce R V12
|
| gptkbp:ignition_system |
magneto
|
| gptkbp:is_tested_for |
extensively tested before production
|
| gptkbp:maintenance |
regular maintenance required
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:noise_level |
distinctive sound
|
| gptkbp:power_output |
approximately 1,000 hp
|
| gptkbp:production_years |
1930-1940s
|
| gptkbp:setting |
gptkb:V12
|
| gptkbp:stroke |
6.0 inches
|
| gptkbp:successor |
gptkb:Rolls-Royce_R_V12_B
|
| gptkbp:torque |
wet sump
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:aircraft
|
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:variant |
gptkb:Rolls-Royce_R_V12_C
|
| gptkbp:weight |
approximately 1,200 lbs
|
| gptkbp:bfsParent |
gptkb:Supermarine_S.6_B
|
| gptkbp:bfsLayer |
3
|