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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
5
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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
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|
gptkbp:bore
|
140 mm
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:compression_ratio
|
5.5:1
|
|
gptkbp:cooling_system
|
liquid cooling
liquid-cooled
|
|
gptkbp:displacement
|
27.0 L
27,000 cc
|
|
gptkbp:emissions_standard
|
single exhaust
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:12
limited production
V engine
high reliability
advanced for its time
1,000 hours
supercharged
wet sump
manual start
influenced future aircraft engines
designed for reliability and performance
360 hp at 1,800 rpm
|
|
gptkbp:engine_type
|
compatible with various aircraft types
Eagle VIII
|
|
gptkbp:first_flight
|
1915
|
|
gptkbp:fuel_capacity
|
800 mm
1,200 mm
|
|
gptkbp:fuel_type
|
gptkb:product
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:origin
|
gptkb:United_Kingdom
|
|
gptkbp:power_output
|
360 hp
|
|
gptkbp:production_years
|
1915-1925
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:stroke
|
150 mm
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Kestrel
|
|
gptkbp:torque
|
1,000 Nm
|
|
gptkbp:type
|
gptkb: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
|