|
gptkbp:instanceOf
|
gptkb:piston_engine
|
|
gptkbp:bore
|
5.5 in (140 mm)
|
|
gptkbp:configuration
|
V-12
|
|
gptkbp:coolingSystem
|
liquid-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:displacement
|
1710 cubic inches
|
|
gptkbp:firstFlight
|
1931
|
|
gptkbp:fuelType
|
aviation gasoline
|
|
gptkbp:length
|
77.3 in (1,964 mm)
|
|
gptkbp:manufacturer
|
gptkb:Allison_Engine_Company
|
|
gptkbp:notableFeature
|
widely used in WWII American fighters
|
|
gptkbp:numberBuilt
|
over 69,000
|
|
gptkbp:powerOutput
|
1,000–1,600 hp
|
|
gptkbp:productionStartYear
|
1931–1956
|
|
gptkbp:stroke
|
6 in (152 mm)
|
|
gptkbp:supercharger
|
single-stage
|
|
gptkbp:usedInAircraft
|
gptkb:Bell_P-63_Kingcobra
gptkb:Douglas_XB-19
gptkb:P-38_Lightning
gptkb:P-39_Airacobra
gptkb:P-40_Warhawk
gptkb:Convair_XP-81
gptkb:P-51A_Mustang
gptkb:Fisher_P-75_Eagle
gptkb:Lockheed_XP-49
gptkb:North_American_XB-21
gptkb:Curtiss_XP-55_Ascender
|
|
gptkbp:valvetrain
|
DOHC, 4 valves per cylinder
|
|
gptkbp:weight
|
1,335 lb (606 kg) dry
|
|
gptkbp:bfsParent
|
gptkb:Miss_Pepsi_hydroplane
|
|
gptkbp:bfsLayer
|
7
|
|
http://www.w3.org/2000/01/rdf-schema#label
|
Allison V-1710 engines
|