|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:ceo
|
1,700 hours
|
|
gptkbp:compression_ratio
|
8.5:1
|
|
gptkbp:configuration
|
six-cylinder
|
|
gptkbp:control_system
|
constant speed
electronic engine control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:displacement
|
550 cubic inches
|
|
gptkbp:emissions_standard
|
FAA regulations
|
|
gptkbp:engine
|
gptkb:gasoline
gptkb:electric_vehicles
gptkb:exhaust_system
temperature sensors
control unit
pressure sensors
fuel injectors
magnetos
oil cooler
cooling fan
starter motor
engine mounts
major overhaul required at TBO
|
|
gptkbp:engine_configuration
|
front-mounted
|
|
gptkbp:engine_displacement
|
9.0 liters
|
|
gptkbp:engine_power
|
up to 2,000 hours
|
|
gptkbp:engine_type
|
reciprocating engine
|
|
gptkbp:first_introduced
|
1990s
|
|
gptkbp:fuel_capacity
|
12 quarts
|
|
gptkbp:fuel_type
|
fuel injection
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TSIO-550 engines
|
|
gptkbp:ignition_system
|
dual ignition
fine wire
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
gptkb:Teledyne_Continental_Motors
|
|
gptkbp:max_speed
|
2700 RPM
|
|
gptkbp:notable_feature
|
turbocharging
|
|
gptkbp:number_of_engines
|
horizontally opposed
|
|
gptkbp:power_output
|
300 horsepower
|
|
gptkbp:propeller
|
variable pitch
|
|
gptkbp:rating
|
TSIO-550-U
TSIO-550-K
|
|
gptkbp:type
|
turbocharged engine
|
|
gptkbp:used_in
|
gptkb:Boeing_707
gptkb:Piper_Aerostar
gptkb:Mooney_M20_V
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:water_requirement
|
20-30 gallons per hour
|
|
gptkbp:weight
|
approximately 400 pounds
|
|
gptkbp:bfsParent
|
gptkb:Continental_Motors
|
|
gptkbp:bfsLayer
|
7
|