Statements (48)
Predicate | Object |
---|---|
gptkbp:instanceOf |
aircraft engine
|
gptkbp:application |
military aircraft
civil aircraft |
gptkbp:compressionRatio |
6.5:1
|
gptkbp:coolingSystem |
air-cooled
|
gptkbp:displacement |
2,600 cubic inches
|
gptkbp:drivetrain |
pushrod actuated
|
gptkbp:engine |
horizontally opposed
supercharged moderate vibration technological advancements in design. used_in_many_WWII_aircraft |
gptkbp:engineConfiguration |
over 10,000 units produced
double-row radial |
gptkbp:engineType |
notable design features
multiple variants produced |
gptkbp:firstFlight |
1940
|
gptkbp:fuelType |
aviation gasoline
dual ignition |
gptkbp:hasArea |
extensively tested
FAA_certified |
https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney R-2600
|
gptkbp:is_used_in |
gptkb:Boeing_B-17_Flying_Fortress
gptkb:Grumman_F6F_Hellcat Douglas A-20 Havoc Lockheed PV-1 Ventura |
gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
gptkbp:noise_level |
loud operation
|
gptkbp:notable_feature |
R-2600-14
R-2600-8 R-2600-3 |
gptkbp:operationalHistory |
important in aviation history
|
gptkbp:performances |
high reliability
high power-to-weight ratio detailed specifications available good fuel efficiency moderate maintenance requirements long operational lifespan |
gptkbp:powerOutput |
1,600 horsepower
|
gptkbp:productionYears |
1940-1950
|
gptkbp:propulsion |
variable-pitch propeller
high thrust output |
gptkbp:related_engine |
gptkb:Pratt_&_Whitney_R-2000_family
|
gptkbp:setting |
14-cylinder
|
gptkbp:successor |
gptkb:Pratt_&_Whitney_R-2800
|
gptkbp:torque |
high torque output
|
gptkbp:type |
radial engine
|
gptkbp:weight |
1,800 pounds
|