gptkbp:instance_of
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gptkb:engine
|
gptkbp:application
|
gptkb:aircraft
civil aircraft
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gptkbp:compression_ratio
|
6.5:1
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gptkbp:cooling_system
|
air-cooled
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gptkbp:diameter
|
3.5 ft
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gptkbp:displacement
|
27.0 L
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gptkbp:engine
|
gptkb:aircraft
gptkb:14-cylinder_radial_engine
gptkb:14
gptkb:Bristol_Aeroplane_Company
gptkb:Bristol_Proteus
four-stroke
civil aircraft
2,500 hp
horizontally opposed
radial layout
2,800 rpm
Bristol Centaurus family
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gptkbp:engine_type
|
gptkb:engine
piston engine
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gptkbp:fuel_capacity
|
1,200 lb
3.5 ft
4.5 ft
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gptkbp:fuel_type
|
gptkb:product
aviation gasoline
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Centaurus 800
|
gptkbp:ignition_system
|
dual ignition
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gptkbp:length
|
4.5 ft
|
gptkbp:manufacturer
|
gptkb:Bristol_Aeroplane_Company
|
gptkbp:original_run
|
1947
|
gptkbp:power_output
|
2,500 hp
|
gptkbp:production_years
|
1947-1960
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gptkbp:propulsion
|
variable-pitch propeller
|
gptkbp:setting
|
14-cylinder
|
gptkbp:successor
|
gptkb:Bristol_Proteus
|
gptkbp:torque
|
2,200 lb-ft
|
gptkbp:type
|
gptkb:engine
|
gptkbp:used_in
|
gptkb:Bristol_Britannia
gptkb:Bristol_Beaufighter
gptkb:Avro_Shackleton
|
gptkbp:valve_configuration
|
overhead valves
|
gptkbp:weight
|
1,200 lb
|
gptkbp:bfsParent
|
gptkb:Bristol_Type_142_B
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gptkbp:bfsLayer
|
5
|