|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:compression_ratio
|
5.5:1
|
|
gptkbp:cooling_system
|
liquid cooling
liquid-cooled
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:displacement
|
27.0 L
|
|
gptkbp:engine
|
gptkb:military_aircraft
limited production
advanced for its time
supercharged
manual start
influenced future aircraft engines
|
|
gptkbp:engine_bore
|
140 mm
|
|
gptkbp:engine_configuration
|
V engine
designed for reliability and performance
|
|
gptkbp:engine_displacement
|
27,000 cc
|
|
gptkbp:engine_oil_system
|
wet sump
|
|
gptkbp:engine_power
|
high reliability
1,000 hours
360 hp at 1,800 rpm
|
|
gptkbp:engine_stroke
|
150 mm
|
|
gptkbp:engine_type
|
compatible with various aircraft types
Eagle VIII
|
|
gptkbp:exhaust_system
|
single exhaust
|
|
gptkbp:first_flight
|
1915
|
|
gptkbp:fuel_capacity
|
800 mm
1,200 mm
|
|
gptkbp:fuel_type
|
gptkb:carburetor
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Eagle engine
|
|
gptkbp:ignition_system
|
magneto ignition
|
|
gptkbp:impact
|
significant impact on aviation history
|
|
gptkbp:maintenance
|
periodic maintenance required
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:noise_level
|
low vibration
moderate noise level
|
|
gptkbp:number_of_engines
|
gptkb:12
|
|
gptkbp:power_output
|
360 hp
|
|
gptkbp:production_years
|
1915-1925
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Kestrel
|
|
gptkbp:torque
|
1,000 Nm
|
|
gptkbp:type
|
gptkb:V8_engine
|
|
gptkbp:used_in
|
gptkb:Avro_504_K
gptkb:Bristol_F.2_Fighter
gptkb:Handley_Page_V/1500
|
|
gptkbp:valve_configuration
|
overhead camshaft
|
|
gptkbp:weight
|
300 kg
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_100_HP
gptkb:Rolls-Royce_120_HP
gptkb:Rolls-Royce_130_HP
gptkb:Rolls-Royce_140_HP
gptkb:Rolls-Royce_300_HP
|
|
gptkbp:bfsLayer
|
6
|