|
gptkbp:instanceOf
|
aircraft engine
|
|
gptkbp:application
|
gptkb:De_Haviland_DH-4
gptkb:Boeing_MB-1
gptkb:Handley_Page_O/400
gptkb:Martin_MB-1
Vickers Vimy
Sopwith Camel
|
|
gptkbp:bore
|
5.5 in
|
|
gptkbp:compressionRatio
|
5.2:1
|
|
gptkbp:coolingSystem
|
liquid-cooled
water-cooled
|
|
gptkbp:cylinderCount
|
16
|
|
gptkbp:displacement
|
27.0 L
|
|
gptkbp:drivetrain
|
overhead valve
|
|
gptkbp:emissionsStandard
|
exhaust manifold
|
|
gptkbp:engine
|
54 in
intake manifold
30 in
low vibration
front-mounted
1800 rpm
influenced future aircraft engines
|
|
gptkbp:engineConfiguration
|
V engine
|
|
gptkbp:engineType
|
electric starter
|
|
gptkbp:firstFlight
|
1917
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
|
|
gptkbp:fuelType
|
spark ignition
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Liberty L-16 engine
|
|
gptkbp:is_used_in
|
gptkb:World_War_I_aircraft
|
|
gptkbp:manufacturer
|
gptkb:Liberty_Engine_Company
|
|
gptkbp:noise_level
|
moderate noise level
|
|
gptkbp:performances
|
high reliability
naturally aspirated
periodic maintenance required
|
|
gptkbp:powerOutput
|
400 hp
|
|
gptkbp:productionYears
|
1917-1920
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:stroke
|
6.0 in
|
|
gptkbp:successor
|
gptkb:Liberty_L-12_engine
|
|
gptkbp:torque
|
600 lb-ft
pressure lubrication
|
|
gptkbp:type
|
gptkb:V-12_engine
|
|
gptkbp:weight
|
400 lb
|