gptkbp:instance_of
|
gptkb:engine
|
gptkbp:application
|
gptkb:aircraft
|
gptkbp:compression_ratio
|
6.5:1
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gptkbp:controls
|
mechanical
|
gptkbp:cooling_system
|
liquid-cooled
water-cooled
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gptkbp:displacement
|
27 liters
|
gptkbp:engine
|
gptkb:battle
gptkb:Rolls-Royce_V12_series
high reliability
high power-to-weight ratio
longitudinal
influential in aviation history
R-1
V-type engine
inline engine design
detailed specifications available
used in various aircraft models
excellent performance
limited production run
3,000 RPM
various modifications made
historically significant engine
V12 engine configuration
1,200 k W
|
gptkbp:engine_type
|
reciprocating engine
multiple variants produced
|
gptkbp:first_introduced
|
gptkb:World_War_II
|
gptkbp:fuel_capacity
|
800 mm
1,200 mm
600 mm
550 kg
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce R V12 B
|
gptkbp:ignition_system
|
dual ignition
|
gptkbp:is_tested_for
|
extensively tested
|
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_R_V12_C
|
gptkbp:torque
|
1,500 Nm
|
gptkbp:type
|
gptkb:engine
|
gptkbp:used_in
|
gptkb:aircraft
|
gptkbp:valve_configuration
|
overhead valve
|
gptkbp:weight
|
approximately 1,200 lbs
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_R_V12
|
gptkbp:bfsLayer
|
4
|