|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:Boeing_B-17_Flying_Fortress
gptkb:C-54_Skymaster
gptkb:C-46_Commando
gptkb:P-47_Thunderbolt
gptkb:B-24_Liberator
|
|
gptkbp:bore
|
5.5 inches
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:control_system
|
mechanical throttle
|
|
gptkbp:cooling_system
|
air-cooled
air cooling
direct air cooling
|
|
gptkbp:displacement
|
975 cubic inches
|
|
gptkbp:engine
|
gptkb:military_aircraft
gptkb:series
gptkb:advanced_technology
gptkb:Continental_R-975
commercial aviation
historically significant
multiple cylinders
|
|
gptkbp:engine_configuration
|
robust design
horizontally opposed
powerful engine
radial layout
detailed specifications
cradle mount
R975 C1
|
|
gptkbp:engine_power
|
high performance
high reliability
long lifespan
performance metrics available
maximum 2800 RPM
|
|
gptkbp:engine_type
|
reciprocating engine
R975 C1 variants
|
|
gptkbp:first_introduced
|
1940s
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Continental R975 C1
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:maintenance
|
moderate maintenance
|
|
gptkbp:manufacturer
|
gptkb:Continental_Motors
|
|
gptkbp:number_of_engines
|
9 cylinders
|
|
gptkbp:power_output
|
400 horsepower
|
|
gptkbp:production_years
|
1940s to 1950s
|
|
gptkbp:propeller
|
variable pitch
|
|
gptkbp:stroke
|
6.0 inches
|
|
gptkbp:successor
|
Continental R-670
|
|
gptkbp:torque
|
high torque
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:military_aircraft
|
|
gptkbp:valve_configuration
|
pushrod
|
|
gptkbp:weight
|
approximately 600 pounds
|
|
gptkbp:bfsParent
|
gptkb:M4_Sherman_tank
gptkb:M4_Sherman_Tank
gptkb:M3_Lee_tank
gptkb:M4_Sherman
|
|
gptkbp:bfsLayer
|
5
|