|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_210_HP
gptkb:Rolls-Royce_290_HP
|
|
gptkbp:bore
|
5.5 in
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
liquid-cooled
water-cooled
|
|
gptkbp:displacement
|
36.7 L
|
|
gptkbp:engine
|
aluminum alloy
modular design
high reliability
2000 hp
advanced for its time
inline engine
influenced future designs
excellent performance
developed in the 1920s
nose-mounted
2500 rpm
used in WWII aircraft
|
|
gptkbp:engine_type
|
reciprocating engine
compatible with various aircraft
K, K1, K2
|
|
gptkbp:first_flight
|
gptkb:1930
|
|
gptkbp:fuel_capacity
|
2.5 m
1.2 m
1.0 m
|
|
gptkbp:fuel_type
|
gptkb:product
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce K series
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:impact
|
significant impact on aviation
|
|
gptkbp:maintenance
|
periodic inspections
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:power_output
|
2000 hp
|
|
gptkbp:production_years
|
1930-1940
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:setting
|
gptkb:V12
|
|
gptkbp:stroke
|
6.0 in
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Merlin
|
|
gptkbp:torque
|
2000 lb-ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Handley_Page_Hastings
gptkb:Avro_York
Avro Lancastrian
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:weight
|
450 kg
|