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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
4
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gptkbp:bfsParent
|
gptkb:Sir_Henry_Royce
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:bore
|
120 mm
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:compression_ratio
|
5.5:1
|
|
gptkbp:cooling_system
|
liquid cooling
water-cooled
|
|
gptkbp:displacement
|
1,800 cc
|
|
gptkbp:emissions_standard
|
single exhaust
|
|
gptkbp:engine
|
gptkb:V12
high reliability
historical significance in aviation
manual start
1,800 rpm
110 horsepower
|
|
gptkbp:engine_type
|
various aircraft types
|
|
gptkbp:fuel_capacity
|
800 mm
1,200 mm
600 mm
40 L/h
10 L
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce 110 HP
|
|
gptkbp:ignition_system
|
magneto ignition
|
|
gptkbp:involved_units
|
approximately 1,000
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:noise_level
|
low noise
low vibration
|
|
gptkbp:original_run
|
1915
|
|
gptkbp:power_output
|
110 hp
|
|
gptkbp:production_years
|
1915-1920
|
|
gptkbp:propulsion
|
fixed-pitch propeller
|
|
gptkbp:setting
|
V engine
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Eagle
|
|
gptkbp:torque
|
200 Nm
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Royal_Aircraft_Factory_S._E.5
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:weight
|
200 kg
|