|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
liquid-cooled
water-cooled
|
|
gptkbp:displacement
|
27 liters
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:Birmingham,_England
gptkb:Rolls-Royce
gptkb:battle
high reliability
high power-to-weight ratio
naturally aspirated
front-mounted
influenced future aircraft engines
used in WWII aircraft
|
|
gptkbp:engine_type
|
gptkb:R_V12_C-7
reciprocating engine
R V12 C-1
R V12 C-10
R V12 C-2
R V12 C-3
R V12 C-4
R V12 C-5
R V12 C-6
R V12 C-8
R V12 C-9
|
|
gptkbp:first_introduced
|
gptkb:World_War_II
|
|
gptkbp:fuel_capacity
|
1,000 mm
1,200 mm
1,800 mm
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce R V12 C
|
|
gptkbp:ignition_system
|
magneto
|
|
gptkbp:maintenance
|
moderate maintenance requirements
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:notable_users
|
gptkb:Hawker_Hurricane
gptkb:noble_title
gptkb:starship
|
|
gptkbp:power_output
|
1,600 hp
|
|
gptkbp:production_years
|
1940s
|
|
gptkbp:setting
|
gptkb:V12
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Griffon
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:valve_configuration
|
DOHC
|
|
gptkbp:weight
|
approximately 1,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_R_V12
|
|
gptkbp:bfsLayer
|
4
|