Statements (54)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
civil aircraft |
| gptkbp:bore |
5.5 inches
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:configuration |
14-cylinder
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:displacement |
2,600 cubic inches
|
| gptkbp:engine |
gptkb:R-2000_family
smooth operation easy installation low vibration levels versatile applications dual ignition system high altitude performance proven track record retractable landing gear good fuel efficiency two-speed supercharger adaptable to various airframes variable pitch propeller widely used in aviation history over 10,000 units produced low speed performance used in various aircraft during WWII |
| gptkbp:engine_configuration |
robust design
horizontally opposed double-row radial engine design |
| gptkbp:engine_power |
high reliability
high power-to-weight ratio |
| gptkbp:engine_type |
supercharged
|
| gptkbp:first_flight |
1941
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney R-2600
|
| gptkbp:maintenance |
moderate maintenance requirements
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:power_output |
1,600 horsepower
|
| gptkbp:production_years |
1941-1951
|
| gptkbp:stroke |
6.0 inches
|
| gptkbp:successor |
gptkb:Pratt_&_Whitney_R-2800
|
| gptkbp:type |
gptkb:radial_engine
|
| gptkbp:used_in |
gptkb:Lockheed_PV-1_Ventura
gptkb:Grumman_F6_F_Hellcat gptkb:Boeing_B-17_Flying_Fortress gptkb:Douglas_A-20_Havoc |
| gptkbp:valve_configuration |
pushrod actuated
|
| gptkbp:variant |
R-2600-14
R-2600-20 R-2600-8 |
| gptkbp:weight |
1,800 pounds
|
| gptkbp:bfsParent |
gptkb:North_American_B-25_Mitchell
gptkb:B-25_Mitchell |
| gptkbp:bfsLayer |
4
|