gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:bore
|
5.125 inches
|
gptkbp:ceo
|
1800 hours
|
gptkbp:compression_ratio
|
8.5:1
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gptkbp:configuration
|
six-cylinder
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gptkbp:control_system
|
throttle control
|
gptkbp:cooling_system
|
air-cooled
finned cylinders
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gptkbp:displacement
|
540 cubic inches
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gptkbp:engine
|
gptkb:Twix
gptkb:gasoline
gptkb:electric_vehicles
magnetos
tachometer
starter motor
oil temperature gauge
fuel pressure gauge
engine monitor system
manifold pressure gauge
prop governor
widely used in light aircraft
cylinder head temperature gauge
engine analyzer
|
gptkbp:engine_configuration
|
inline engine
engine mount system
|
gptkbp:engine_power
|
high reliability
|
gptkbp:engine_type
|
IO-550 engine
horizontally opposed engine
roller camshaft
|
gptkbp:exhaust_system
|
dual intake manifold
exhaust stacks
|
gptkbp:first_introduced
|
1950s
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gptkbp:fuel_capacity
|
8 quarts
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
optional fuel injection
|
https://www.w3.org/2000/01/rdf-schema#label
|
IO-540 engine
|
gptkbp:ignition_system
|
gptkb:Champion_REM40_E
dual ignition
|
gptkbp:maintenance
|
100 hours
|
gptkbp:manufacturer
|
gptkb:Teledyne_Continental_Motors
|
gptkbp:max_speed
|
2700 RPM
|
gptkbp:notable_applications
|
gptkb:Piper_PA-32
gptkb:Beechcraft_Bonanza
gptkb:Cessna_182
|
gptkbp:number_of_engines
|
aluminum alloy
|
gptkbp:power_output
|
300 horsepower
|
gptkbp:propeller
|
constant speed propeller
|
gptkbp:stroke
|
4.0 inches
|
gptkbp:type
|
reciprocating engine
|
gptkbp:used_in
|
general aviation aircraft
|
gptkbp:valve_configuration
|
overhead valve
|
gptkbp:weight
|
approximately 360 lbs
|
gptkbp:bfsParent
|
gptkb:Lycoming
gptkb:Lycoming_Engines
|
gptkbp:bfsLayer
|
6
|